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+Internet Engineering Task Force (IETF) N. Mäurer, Ed.
+Request for Comments: 9372 T. Gräupl, Ed.
+Category: Informational German Aerospace Center (DLR)
+ISSN: 2070-1721 C. Schmitt, Ed.
+ Research Institute CODE, UniBwM
+ March 2023
+
+
+ L-Band Digital Aeronautical Communications System (LDACS)
+
+Abstract
+
+ This document gives an overview of the L-band Digital Aeronautical
+ Communications System (LDACS) architecture, which provides a secure,
+ scalable, and spectrum-efficient terrestrial data link for civil
+ aviation. LDACS is a scheduled and reliable multi-application
+ cellular broadband system with support for IPv6. It is part of a
+ larger shift of flight guidance communication moving to IP-based
+ communication. High reliability and availability of IP connectivity
+ over LDACS, as well as security, are therefore essential. The intent
+ of this document is to introduce LDACS to the IETF community, raise
+ awareness on related activities inside and outside of the IETF, and
+ to seek expertise in shaping the shift of aeronautics to IP.
+
+Status of This Memo
+
+ This document is not an Internet Standards Track specification; it is
+ published for informational purposes.
+
+ This document is a product of the Internet Engineering Task Force
+ (IETF). It represents the consensus of the IETF community. It has
+ received public review and has been approved for publication by the
+ Internet Engineering Steering Group (IESG). Not all documents
+ approved by the IESG are candidates for any level of Internet
+ Standard; see Section 2 of RFC 7841.
+
+ Information about the current status of this document, any errata,
+ and how to provide feedback on it may be obtained at
+ https://www.rfc-editor.org/info/rfc9372.
+
+Copyright Notice
+
+ Copyright (c) 2023 IETF Trust and the persons identified as the
+ document authors. All rights reserved.
+
+ This document is subject to BCP 78 and the IETF Trust's Legal
+ Provisions Relating to IETF Documents
+ (https://trustee.ietf.org/license-info) in effect on the date of
+ publication of this document. Please review these documents
+ carefully, as they describe your rights and restrictions with respect
+ to this document. Code Components extracted from this document must
+ include Revised BSD License text as described in Section 4.e of the
+ Trust Legal Provisions and are provided without warranty as described
+ in the Revised BSD License.
+
+Table of Contents
+
+ 1. Introduction
+ 2. Acronyms
+ 3. Motivation and Use Cases
+ 3.1. Voice Communications Today
+ 3.2. Data Communications Today
+ 4. Provenance and Documents
+ 5. Applicability
+ 5.1. Advances beyond the State of the Art
+ 5.1.1. Priorities
+ 5.1.2. Security
+ 5.1.3. High Data Rates
+ 5.2. Application
+ 5.2.1. Air/Ground Multilink
+ 5.2.2. Air/Air Extension for LDACS
+ 5.2.3. Flight Guidance
+ 5.2.4. Business Communications of Airlines
+ 5.2.5. LDACS-Based Navigation
+ 6. Requirements
+ 7. Characteristics
+ 7.1. LDACS Access Network
+ 7.2. Topology
+ 7.3. LDACS Protocol Stack
+ 7.3.1. LDACS Physical Layer
+ 7.3.2. LDACS Data Link Layer
+ 7.3.3. LDACS Subnetwork Layer and Protocol Services
+ 7.4. LDACS Mobility
+ 7.5. LDACS Management Interfaces and Protocols
+ 8. Reliability and Availability
+ 8.1. Below Layer 1
+ 8.2. Layers 1 and 2
+ 8.3. Beyond Layer 2
+ 9. Security Considerations
+ 9.1. Security in Wireless Digital Aeronautical Communications
+ 9.2. Security in Depth
+ 9.3. LDACS Security Requirements
+ 9.4. LDACS Security Objectives
+ 9.5. LDACS Security Functions
+ 9.6. LDACS Security Architecture
+ 9.6.1. Entities
+ 9.6.2. Entity Identification
+ 9.6.3. Entity Authentication and Key Establishment
+ 9.6.4. Message-In-Transit Confidentiality, Integrity, and
+ Authenticity
+ 9.7. Considerations on LDACS Security Impact on IPv6 Operational
+ Security
+ 10. IANA Considerations
+ 11. Informative References
+ Appendix A. Selected Information from DO-350A
+ Acknowledgements
+ Authors' Addresses
+
+1. Introduction
+
+ One of the main pillars of the modern Air Traffic Management (ATM)
+ system is the existence of a communications infrastructure that
+ enables efficient aircraft control and safe aircraft separation in
+ all phases of flight. Current systems are technically mature, but
+ they are suffering from the Very High Frequency (VHF) band's
+ increasing saturation in high-density areas and the limitations posed
+ by analog radio communications. Therefore, aviation strives for a
+ sustainable modernization of the aeronautical communications
+ infrastructure on the basis of IP.
+
+ This modernization is realized in two steps: (1) the transition of
+ communications data links from analog to digital technologies and (2)
+ the introduction of IPv6-based networking protocols [RFC8200] in
+ aeronautical networks [ICAO2015].
+
+ Step (1) is realized via ATM communications transitioning from analog
+ VHF voice [KAMA2010] to more spectrum-efficient digital data
+ communication. For terrestrial communications, the Global Air
+ Navigation Plan (GANP) created by the International Civil Aviation
+ Organization (ICAO) foresees this transition to be realized by the
+ development of the L-band Digital Aeronautical Communications System
+ (LDACS). Since Central Europe has been identified as the area of the
+ world that suffers the most from increased saturation of the VHF
+ band, the initial rollout of LDACS will likely start there and
+ continue to other increasingly saturated zones such as the East and
+ West Coast of the US and parts of Asia [ICAO2018].
+
+ Technically, LDACS enables IPv6-based Air/Ground (A/G) communication
+ related to aviation safety and regularity of flight [ICAO2015].
+ Passenger communication and similar services are not supported since
+ only communications related to "safety and regularity of flight" are
+ permitted in protected aviation frequency bands. The particular
+ challenge is that no additional frequencies can be made available for
+ terrestrial aeronautical communication; thus, it was necessary to
+ develop coexistence mechanisms and procedures to enable the
+ interference-free operation of LDACS in parallel with other
+ aeronautical services and systems in the protected frequency band.
+ Since LDACS will be used for aircraft guidance, high reliability and
+ availability for IP connectivity over LDACS are essential.
+
+ LDACS is standardized in ICAO and the European Organization for Civil
+ Aviation Equipment (EUROCAE).
+
+ This document provides information to the IETF community about the
+ aviation industry transition of flight guidance systems from analog
+ to digital, provides context for LDACS relative to related IETF
+ activities [LISP-GB-ATN], and seeks expertise on realizing reliable
+ IPv6 over LDACS for step (1). This document does not intend to
+ advance LDACS as an IETF Standards Track document.
+
+ Step (2) is a strategy for the worldwide rollout of IPv6-capable
+ digital aeronautical internetworking. This is called the
+ Aeronautical Telecommunications Network (ATN) / Internet Protocol
+ Suite (IPS) (hence, ATN/IPS). It is specified in the ICAO document
+ Doc 9896 [ICAO2015], the Radio Technical Commission for Aeronautics
+ (RTCA) document DO-379 [RTCA2019], the EUROCAE document ED-262
+ [EURO2019], and the Aeronautical Radio Incorporated (ARINC) document
+ 858 [ARI2021]. LDACS is subject to these regulations since it
+ provides an "access network" (link-layer data link) to the ATN/IPS.
+
+ ICAO has chosen IPv6 as a basis for the ATN/IPS mostly for historical
+ reasons since a previous architecture based on ISO/OSI protocols (the
+ ATN/OSI) failed in the marketplace.
+
+ In the context of safety-related communications, LDACS will play a
+ major role in future ATM. ATN/IPS data links will provide
+ diversified terrestrial and space-based connectivity in a multilink
+ concept called the Future Communications Infrastructure (FCI)
+ [VIR2021]. From a technical point of view, the FCI will realize
+ airborne and multihomed IPv6 networks connected to a global ground
+ network via at least two independent communication technologies.
+ This is considered in more detail in related documents [LISP-GB-ATN]
+ [RTGWG-ATN-BGP]. As such, ICAO has actively sought out the support
+ of IETF to define a mobility solution for step (2), which is
+ currently the Locator/ID Separation Protocol (LISP).
+
+ In the context of the Reliable and Available Wireless (RAW) Working
+ Group, developing options, such as intelligent switching between data
+ links, for reliably delivering content from and to endpoints is
+ foreseen. As LDACS is part of such a concept, the work of RAW is
+ immediately applicable. In general, with the aeronautical
+ communications system transitioning to ATN/IPS and data being
+ transported via IPv6, closer cooperation and collaboration between
+ the aeronautical and IETF community is desirable.
+
+ LDACS standardization within the framework of ICAO started in
+ December 2016. As of 2022, the ICAO standardization group has
+ produced the final Standards and Recommended Practices (SARPS)
+ document [ICAO2022] that defines the general characteristics of
+ LDACS. By the end of 2023, the ICAO standardization group plans to
+ have developed an ICAO technical manual, which is the ICAO equivalent
+ to a technical standard. The LDACS standardization is not finished
+ yet; therefore, this document is a snapshot of the current status.
+ The physical characteristics of an LDACS installation (form, fit, and
+ function) will be standardized by EUROCAE. Generally, the group is
+ open to input from all sources and encourages cooperation between the
+ aeronautical and IETF communities.
+
+2. Acronyms
+
+ The following terms are used in the context of RAW in this document:
+
+ A/A: Air/Air
+ A/G: Air/Ground
+ A2G: Air-to-Ground
+ ACARS: Aircraft Communications Addressing and Reporting System
+ AC-R: Access Router
+ ADS-B: Automatic Dependent Surveillance - Broadcast
+ ADS-C: Automatic Dependent Surveillance - Contract
+ AeroMACS: Aeronautical Mobile Airport Communications System
+ ANSP: Air Traffic Network Service Provider
+ AOC: Aeronautical Operational Control
+ ARINC: Aeronautical Radio Incorporated
+ ARQ: Automatic Repeat reQuest
+ AS: Aircraft Station
+ ATC: Air Traffic Control
+ ATM: Air Traffic Management
+ ATN: Aeronautical Telecommunications Network
+ ATS: Air Traffic Service
+ BCCH: Broadcast Channel
+ CCCH: Common Control Channel
+ CM: Context Management
+ CNS: Communication Navigation Surveillance
+ COTS: Commercial Off-The-Shelf
+ CPDLC: Controller-Pilot Data Link Communications
+ CSP: Communications Service Provider
+ DCCH: Dedicated Control Channel
+ DCH: Data Channel
+ Diffserv: Differentiated Services
+ DLL: Data Link Layer
+ DLS: Data Link Service
+ DME: Distance Measuring Equipment
+ DSB-AM: Double Side-Band Amplitude Modulation
+ DTLS: Datagram Transport Layer Security
+ EUROCAE: European Organization for Civil Aviation Equipment
+ FAA: Federal Aviation Administration
+ FCI: Future Communications Infrastructure
+ FDD: Frequency Division Duplex
+ FL: Forward Link
+ GANP: Global Air Navigation Plan
+ GBAS: Ground-Based Augmentation System
+ GNSS: Global Navigation Satellite System
+ GS: Ground-Station
+ G2A: Ground-to-Air
+ HF: High Frequency
+ ICAO: International Civil Aviation Organization
+ IP: Internet Protocol
+ IPS: Internet Protocol Suite
+ kbit/s: kilobit per second
+ LDACS: L-band Digital Aeronautical Communications System
+ LISP: Locator/ID Separation Protocol
+ LLC: Logical Link Control
+ LME: LDACS Management Entity
+ MAC: Medium Access Control
+ MF: Multiframe
+ NETCONF: Network Configuration Protocol
+ OFDM: Orthogonal Frequency Division Multiplexing
+ OFDMA: Orthogonal Frequency Division Multiplexing Access
+ OSI: Open Systems Interconnection
+ PHY: Physical Layer
+ QPSK: Quadrature Phase-Shift Keying
+ RACH: Random-Access Channel
+ RL: Reverse Link
+ RTCA: Radio Technical Commission for Aeronautics
+ SARPS: Standards and Recommended Practices
+ SDR: Software-Defined Radio
+ SESAR: Single European Sky ATM Research
+ SF: Super-Frame
+ SNMP: Simple Network Management Protocol
+ SNP: Subnetwork Protocol
+ VDLm2: VHF Data Link mode 2
+ VHF: Very High Frequency
+ VI: Voice Interface
+
+
+3. Motivation and Use Cases
+
+ Aircraft are currently connected to Air Traffic Control (ATC) and
+ Aeronautical Operational Control (AOC) services via voice and data
+ communications systems through all phases of flight. ATC refers to
+ communication for flight guidance. AOC is a generic term referring
+ to the business communication of airlines and refers to the mostly
+ proprietary exchange of data between the aircraft of the airline and
+ the airline's operation centers and service partners. The ARINC
+ document 633 was developed and first released in 2007 [ARI2019] with
+ the goal to standardize these messages for interoperability, e.g.,
+ messages between the airline and fueling or de-icing companies.
+ Within the airport and terminal area, connectivity is focused on high
+ bandwidth communications. However, in the en route domain, high
+ reliability, robustness, and range are the main foci. Voice
+ communications may use the same or different equipment as data
+ communications systems. In the following, the main differences
+ between voice and data communications capabilities are summarized.
+ The assumed list of use cases for LDACS complements the list of use
+ cases stated in [RAW-USE-CASES] and the list of reliable and
+ available wireless technologies presented in [RAW-TECHNOS].
+
+3.1. Voice Communications Today
+
+ Voice links are used for Air/Ground (A/G) and Air/Air (A/A)
+ communications. The communications equipment can be installed on
+ ground or in the aircraft, in which cases the High Frequency (HF) or
+ VHF frequency band is used. For remote domains, voice communications
+ can also be satellite-based. All VHF and HF voice communications are
+ operated via open Broadcast Channels (BCCHs) without authentication,
+ encryption, or other protective measures. The use of well-proven
+ communications procedures via BCCHs, such as phraseology or read-
+ backs, requiring well-trained personnel help to enhance the safety of
+ communications but does not replace necessary cryptographical
+ security mechanisms. The main voice communications media is still
+ the analog VHF Double Side-Band Amplitude Modulation (DSB-AM)
+ communications technique supplemented by HF single side-band
+ amplitude modulation and satellite communications for remote and
+ oceanic regions. DSB-AM has been in use since 1948, works reliably
+ and safely, and uses low-cost communication equipment. These are the
+ main reasons why VHF DSB-AM communications are still in use, and it
+ is likely that this technology will remain in service for many more
+ years. However, this results in current operational limitations and
+ impediments in deploying new ATM applications, such as flight-centric
+ operation with point-to-point communications between pilots and ATC
+ officers [BOE2019].
+
+3.2. Data Communications Today
+
+ Like for voice communications, data communications into the cockpit
+ are currently provided by ground-based equipment operating either on
+ HF or VHF radio bands or by legacy satellite systems. All these
+ communication systems use narrowband radio channels with a data
+ throughput capacity in the order of kbit/s. Additional
+ communications systems are available while the aircraft is on the
+ ground, such as the Aeronautical Mobile Airport Communications System
+ (AeroMACS) or public cellular networks, that operate in the Airport
+ (APT) domain and are able to deliver broadband communications
+ capability [BOE2019].
+
+ For regulatory reasons, the data communications networks used for the
+ transmission of data relating to the safety and regularity of flight
+ must be strictly isolated from those providing entertainment services
+ to passengers. This leads to a situation where the flight crews are
+ supported by narrowband services during flight while passengers have
+ access to in-flight broadband services. The current HF and VHF data
+ links cannot provide broadband services now or in the future due to
+ the lack of available spectrum. This technical shortcoming is
+ becoming a limitation to enhanced ATM operations, such as trajectory-
+ based operations and 4D trajectory negotiations [BOE2019].
+
+ Satellite-based communications are currently under investigation, and
+ enhanced capabilities that will be able to provide in-flight
+ broadband services and communications supporting the safety and
+ regularity of flight are under development. In parallel, the ground-
+ based broadband data link technology LDACS is being standardized by
+ ICAO and has recently shown its maturity during flight tests
+ [MAE20211] [BEL2021]. The LDACS technology is scalable, secure, and
+ spectrum-efficient, and it provides significant advantages to the
+ users and service providers. It is expected that both satellite
+ systems and LDACS will be deployed to support the future aeronautical
+ communication needs as envisaged by the ICAO GANP [BOE2019].
+
+4. Provenance and Documents
+
+ The development of LDACS has already made substantial progress in the
+ Single European Sky ATM Research (SESAR) framework and is currently
+ being continued in the follow-up program SESAR2020 [RIH2018]. A key
+ objective of these activities is to develop, implement, and validate
+ a modern aeronautical data link that is able to evolve with aviation
+ needs over the long term. To this end, an LDACS specification has
+ been produced [GRA2020] and is continuously updated. Transmitter
+ demonstrators were developed to test the spectrum compatibility of
+ LDACS with legacy systems operating in the L-band [SAJ2014], and the
+ overall system performance was analyzed by computer simulations,
+ indicating that LDACS can fulfill the identified requirements
+ [GRA2011].
+
+ Up to now, LDACS standardization has been focused on the development
+ of the Physical Layer (PHY) and the Data Link Layer (DLL). Only
+ recently have higher layers come into the focus of the LDACS
+ development activities. Currently no "IPv6 over LDACS" specification
+ is defined; however, SESAR2020 has started experimenting with
+ IPv6-based LDACS and ICAO plans to seek guidance from IETF to develop
+ IPv6 over LDACS. As of May 2022, LDACS defines 1536-byte user data
+ packets [GRA2020] in which IPv6 traffic shall be encapsulated.
+ Additionally, Robust Header Compression (ROHC) [RFC5795] is
+ considered on the LDACS Subnetwork Protocol (SNP) layer
+ (cf. Section 7.3.3).
+
+ The IPv6 architecture for the aeronautical telecommunication network
+ is called the ATN/IPS. Link-layer technologies within the ATN/IPS
+ encompass LDACS [GRA2020], AeroMACS [KAMA2018], and several SatCOM
+ candidates; combined with the ATN/IPS, these are called the "FCI".
+ The FCI will support quality of service, link diversity, and mobility
+ under the umbrella of the "multilink concept". The "multilink
+ concept" describes the idea that depending on link quality,
+ communication can be switched seamlessly from one data link
+ technology to another. This work is led by the ICAO Communication
+ Panel Working Group (WG-I).
+
+ In addition to standardization activities, several industrial LDACS
+ prototypes have been built. One set of LDACS prototypes has been
+ evaluated in flight trials confirming the theoretical results
+ predicting the system performance [GRA2018] [MAE20211] [BEL2021].
+
+5. Applicability
+
+ LDACS is a multi-application cellular broadband system capable of
+ simultaneously providing various kinds of Air Traffic Services (ATSs)
+ including ATS-B3 and AOC communications services from deployed
+ Ground-Stations (GSs). The physical layer and data link layer of
+ LDACS are optimized for Controller-Pilot Data Link Communications
+ (CPDLC), but the system also supports digital A/G voice
+ communications.
+
+ LDACS supports communications in all airspaces (airport, terminal
+ maneuvering area, and en route) and on the airport surface. The
+ physical LDACS cell coverage is effectively decoupled from the
+ operational coverage required for a particular service. This is new
+ in aeronautical communications. Services requiring wide-area
+ coverage can be installed at several adjacent LDACS cells. The
+ handover between the involved LDACS cells is seamless, automatic, and
+ transparent to the user. Therefore, the LDACS communications concept
+ enables the aeronautical communication infrastructure to support
+ future dynamic airspace management concepts.
+
+5.1. Advances beyond the State of the Art
+
+ LDACS will offer several capabilities that are not yet provided in
+ contemporarily deployed aeronautical communications systems. These
+ capabilities were already tested and confirmed in lab or flight
+ trials with available LDACS prototype hardware [BEL2021] [MAE20211].
+
+5.1.1. Priorities
+
+ LDACS is able to manage service priorities, which is an important
+ feature that is not available in some of the current data link
+ deployments. Thus, LDACS guarantees bandwidth availability, low
+ latency, and high continuity of service for safety-critical ATS
+ applications while simultaneously accommodating less safety-critical
+ AOC services.
+
+5.1.2. Security
+
+ LDACS is a secure data link with built-in security mechanisms. It
+ enables secure data communications for ATS and AOC services,
+ including secured private communications for aircraft operators and
+ Air Traffic Network Service Providers (ANSPs). This includes
+ concepts for key and trust management, Mutual Authentication and Key
+ Establishment (MAKE) protocols, key derivation measures, user and
+ control message-in-transit protection, secure logging, and
+ availability and robustness measures [MAE20182] [MAE2021].
+
+5.1.3. High Data Rates
+
+ The user data rate of LDACS is 315 kbit/s to 1428 kbit/s on the
+ Forward Link (FL) for the Ground-to-Air (G2A) connection, and 294
+ kbit/s to 1390 kbit/s on the Reverse Link (RL) for the Air-to-Ground
+ (A2G) connection, depending on coding and modulation. This is up to
+ two orders of magnitude greater than what current terrestrial digital
+ aeronautical communications systems, such as the VHF Data Link mode 2
+ (VDLm2), provide; see [ICAO2019] [GRA2020].
+
+5.2. Application
+
+ LDACS will be used by several aeronautical applications ranging from
+ enhanced communications protocol stacks (multihomed mobile IPv6
+ networks in the aircraft and potentially ad-hoc networks between
+ aircraft) to broadcast communication applications (Global Navigation
+ Satellite System (GNSS) correction data) and integration with other
+ service domains (using the communications signal for navigation)
+ [MAE20211]. Also, a digital voice service offering better quality
+ and service than current HF and VHF systems is foreseen.
+
+5.2.1. Air/Ground Multilink
+
+ It is expected that LDACS, together with upgraded satellite-based
+ communications systems, will be deployed within the FCI and
+ constitute one of the main components of the multilink concept within
+ the FCI.
+
+ Both technologies, LDACS and satellite systems, have their specific
+ benefits and technical capabilities that complement each other.
+ Satellite systems are especially well-suited for large coverage areas
+ with less dense air traffic, e.g., oceanic regions. LDACS is well-
+ suited for dense air traffic areas, e.g., continental areas or
+ hotspots around airports and terminal airspace. In addition, both
+ technologies offer comparable data link capacity; thus, both are
+ well-suited for redundancy, mutual back-up, or load balancing.
+
+ Technically, the FCI multilink concept will be realized by multihomed
+ mobile IPv6 networks in the aircraft. The related protocol stack is
+ currently under development by ICAO, within SESAR, and the IETF.
+ Currently, two layers of mobility are foreseen. Local mobility
+ within the LDACS access network is realized through Proxy Mobile IPv6
+ (PMIPv6), and global mobility between "multilink" access networks
+ (which need not be LDACS) is implemented on top of LISP [LISP-GB-ATN]
+ [RFC9300] [RFC9301].
+
+5.2.2. Air/Air Extension for LDACS
+
+ A potential extension of the multilink concept is its extension to
+ the integration of ad-hoc networks between aircraft.
+
+ Direct A/A communication between aircraft in terms of ad-hoc data
+ networks is currently considered a research topic since there is no
+ immediate operational need for it, although several possible use
+ cases are discussed (Automatic Dependent Surveillance - Broadcast
+ (ADS-B), digital voice, wake vortex warnings, and trajectory
+ negotiation) [BEL2019]. It should also be noted that currently
+ deployed analog VHF voice radios support direct voice communication
+ between aircraft, making a similar use case for digital voice
+ plausible.
+
+ LDACS A/A is currently not a part of the standardization process and
+ will not be covered within this document. However, it is planned
+ that LDACS A/A will be rolled out after the initial deployment of
+ LDACS A/G and seamlessly integrated in the existing LDACS ground-
+ based system.
+
+5.2.3. Flight Guidance
+
+ The FCI (and therefore LDACS) is used to provide flight guidance.
+ This is realized using three applications:
+
+ 1. Context Management (CM): The CM application manages the automatic
+ logical connection to the ATC center currently responsible to
+ guide the aircraft. Currently, this is done by the air crew
+ manually changing VHF voice frequencies according to the progress
+ of the flight. The CM application automatically sets up
+ equivalent sessions.
+ 2. Controller-Pilot Data Link Communications (CPDLC): The CPDLC
+ application provides the air crew with the ability to exchange
+ data messages similar to text messages with the currently
+ responsible ATC center. The CPDLC application takes over most of
+ the communication currently performed over VHF voice and enables
+ new services that do not lend themselves to voice communication
+ (i.e., trajectory negotiation).
+ 3. Automatic Dependent Surveillance - Contract (ADS-C): ADS-C
+ reports the position of the aircraft to the currently active ATC
+ center. Reporting is bound to "contracts", i.e., pre-defined
+ events related to the progress of the flight (i.e., the
+ trajectory). ADS-C and CPDLC are the primary applications used
+ for implementing in-flight trajectory management.
+
+ CM, CPDLC, and ADS-C are available on legacy data links but are not
+ widely deployed and with limited functionality.
+
+ Further ATC applications may be ported to use the FCI or LDACS as
+ well. A notable application is the Ground-Based Augmentation System
+ (GBAS) for secure, automated landings. The GNSS-based GBAS is used
+ to improve the accuracy of GNSS to allow GNSS-based instrument
+ landings. This is realized by sending GNSS correction data (e.g.,
+ compensating ionospheric errors in the GNSS signal) to the aircraft's
+ GNSS receiver via a separate data link. Currently, the VHF Data
+ Broadcast (VDB) data link is used. VDB is a narrowband one-way,
+ single-purpose data link without advanced security and is only used
+ to transmit GBAS correction data. These shortcomings show a clear
+ need to replace VDB. A natural candidate to replace it is LDACS,
+ because it is a bidirectional data link, also operates in non-line-of
+ sight scenarios, offers strong integrated link-layer security, and
+ has a considerably larger operational range than VDB [MAE20211].
+
+5.2.4. Business Communications of Airlines
+
+ In addition to ATSs, AOC services are transmitted over LDACS. AOC is
+ a generic term referring to the business communication of airlines
+ between the airlines and service partners on the ground and their own
+ aircraft in the air. Regulatory-wise, this is considered related to
+ safety and regularity of flight; therefore, it may be transmitted
+ over LDACS. AOC communication is considered the main business case
+ for LDACS communications service providers since modern aircraft
+ generate significant amounts of data (e.g., engine maintenance data).
+
+5.2.5. LDACS-Based Navigation
+
+ Beyond communications, radio signals can always be used for
+ navigation as well. This fact is used for the LDACS navigation
+ concept.
+
+ For future aeronautical navigation, ICAO recommends the further
+ development of GNSS-based technologies as primary means for
+ navigation. However, due to the large separation between
+ navigational satellites and aircraft, the power of the GNSS signals
+ received by the aircraft is very low. As a result, GNSS disruptions
+ might occasionally occur due to unintentional interference or
+ intentional jamming. Yet, the navigation services must be available
+ with sufficient performance for all phases of flight. Therefore,
+ during GNSS outages or blockages, an alternative solution is needed.
+ This is commonly referred to as Alternative Positioning, Navigation,
+ and Timing (APNT).
+
+ One such APNT solution is based on exploiting the built-in navigation
+ capabilities of LDACS operation. That is, the normal operation of
+ LDACS for ATC and AOC communications would also directly enable the
+ aircraft to navigate and obtain a reliable timing reference from the
+ LDACS GSs. Current cell planning for Europe shows 84 LDACS cells to
+ be sufficient [MOST2018] to cover the continent at a sufficient
+ service level. If more than three GSs are visible by the aircraft,
+ via knowing the exact positions of these and having a good channel
+ estimation (which LDACS does due to numerous works mapping the L-band
+ channel characteristics [SCHN2018]), it is possible to calculate the
+ position of the aircraft via measuring signal propagation times to
+ each GS. In flight trials in 2019 with one aircraft (and airborne
+ radio inside it) and just four GSs, navigation feasibility was
+ demonstrated within the footprint of all four GSs with a 95th
+ percentile position-domain error of 171.1m [OSE2019] [BEL2021]
+ [MAE20211]. As such, LDACS can be used independently of GNSS as a
+ navigation alternative. Positioning errors will decrease markedly as
+ more GSs are deployed [OSE2019] [BEL2021] [MAE20211].
+
+ LDACS navigation has already been demonstrated in practice in two
+ flight measurement campaigns [SHU2013] [BEL2021] [MAE20211].
+
+6. Requirements
+
+ The requirements for LDACS are mostly defined by its application
+ area: communications related to safety and regularity of flight.
+
+ A particularity of the current aeronautical communication landscape
+ is that it is heavily regulated. Aeronautical data links (for
+ applications related to safety and regularity of flight) may only use
+ spectrum licensed to aviation and data links endorsed by ICAO.
+ Nation states can change this locally; however, due to the global
+ scale of the air transportation system, adherence to these practices
+ is to be expected.
+
+ Aeronautical data links for the ATN are therefore expected to remain
+ in service for decades. The VDLm2 data link currently used for
+ digital terrestrial internetworking was developed in the 1990s (the
+ use of the Open Systems Interconnection (OSI) stack indicates that as
+ well). VDLm2 is expected to be used at least for several decades to
+ come. In this respect, aeronautical communications for applications
+ related to safety and regularity of flight is more comparable to
+ industrial applications than to the open Internet.
+
+ Internetwork technology is already installed in current aircraft.
+ Current ATS applications use either the Aircraft Communications
+ Addressing and Reporting System (ACARS) or the OSI stack. The
+ objective of the development effort of LDACS, as part of the FCI, is
+ to replace legacy OSI stack and proprietary ACARS internetwork
+ technologies with industry standard IP technology. It is anticipated
+ that the use of Commercial Off-The-Shelf (COTS) IP technology mostly
+ applies to the ground network. The avionics networks on the aircraft
+ will likely be heavily modified versions of Ethernet or proprietary.
+
+ Currently, AOC applications mostly use the same stack (although some
+ applications, like the graphical weather service, may use the
+ commercial passenger network). This creates capacity problems
+ (resulting in excessive amounts of timeouts) since the underlying
+ terrestrial data links do not provide sufficient bandwidth (i.e.,
+ with VDLm2 currently in the order of 10 kbit/s). The use of non-
+ aviation-specific data links is considered a security problem.
+ Ideally, the aeronautical IP internetwork (hence the ATN over which
+ only communications related to safety and regularity of flight is
+ handled) and the Internet should be completely separated at Layer 3.
+
+ The objective of LDACS is to provide a next-generation terrestrial
+ data link designed to support IP addressing and provide much higher
+ bandwidth to avoid the operational problems that are currently
+ experienced.
+
+ The requirement for LDACS is therefore to provide a terrestrial high-
+ throughput data link for IP internetworking in the aircraft.
+
+ In order to fulfill the above requirement, LDACS needs to be
+ interoperable with IP (and IP-based services like Voice-over-IP) at
+ the gateway connecting the LDACS network to other aeronautical ground
+ networks (i.e., the ATN). On the avionics side, in the aircraft,
+ aviation-specific solutions are to be expected.
+
+ In addition to these functional requirements, LDACS and its IP stack
+ need to fulfill the requirements defined in RTCA DO-350A/EUROCAE ED-
+ 228A [DO350A]. This document defines continuity, availability, and
+ integrity requirements at different scopes for each ATM application
+ (CPDLC, CM, and ADS-C). The scope most relevant to IP over LDACS is
+ the Communications Service Provider (CSP) scope.
+
+ Continuity, availability, and integrity requirements are defined in
+ Volume 1 of [DO350A] in Tables 5-14 and 6-13. Appendix A presents
+ the required information.
+
+ In a similar vein, requirements to fault management are defined in
+ the same tables.
+
+7. Characteristics
+
+ LDACS will become one of several wireless access networks connecting
+ aircraft to the ATN implemented by the FCI.
+
+ The current LDACS design is focused on the specification of Layers 1
+ and 2. However, for the purpose of this work, only Layer 2 details
+ are discussed here.
+
+ Achieving the stringent continuity, availability, and integrity
+ requirements defined in [DO350A] will require the specification of
+ Layer 3 and above mechanisms (e.g., reliable crossover at the IP
+ layer). Fault management mechanisms are similarly unspecified as of
+ November 2022. Current regulatory documents do not fully specify the
+ above mechanism yet. However, a short overview of the current state
+ shall be given throughout each section here.
+
+7.1. LDACS Access Network
+
+ An LDACS access network contains an Access Router (AC-R) and several
+ GSs, each of them providing one LDACS radio cell.
+
+ User-plane interconnection to the ATN is facilitated by the AC-R
+ peering with an A/G Router connected to the ATN.
+
+ The internal control plane of an LDACS access network interconnects
+ the GSs. An LDACS access network is illustrated in Figure 1. Dashes
+ denote the user plane and points denote the control plane.
+
+ wireless user
+ link plane
+ AS-------------GS---------------AC-R---A/G-----ATN
+ .............. | Router
+ control . |
+ plane . |
+ . |
+ GS----------------|
+ . |
+ . |
+ GS----------------+
+
+ Figure 1: LDACS Access Network with Three GSs and One AS
+
+7.2. Topology
+
+ LDACS is a cellular point-to-multipoint system. It assumes a star
+ topology in each cell where Aircraft Stations (ASs) belonging to
+ aircraft within a certain volume of space (the LDACS cell) are
+ connected to the controlling GS. The LDACS GS is a centralized
+ instance that controls LDACS A/G communications within its cell. The
+ LDACS GS can simultaneously support multiple bidirectional
+ communications to the ASs under its control. LDACS's GSs themselves
+ are connected to each other and the AC-R.
+
+ Prior to utilizing the system, an aircraft has to register with the
+ controlling GS to establish dedicated logical channels for user and
+ control data. Control channels have statically allocated resources
+ while user channels have dynamically assigned resources according to
+ the current demand. Logical channels exist only between the GS and
+ the AS.
+
+7.3. LDACS Protocol Stack
+
+ The protocol stack of LDACS is implemented in the AS and GS. It
+ consists of the PHY with five major functional blocks above it. Four
+ are placed in the DLL of the AS and GS: Medium Access Control (MAC)
+ layer, Voice Interface (VI), Data Link Service (DLS), and LDACS
+ Management Entity (LME). The fifth entity, the SNP, resides within
+ the subnetwork layer. The LDACS radio is externally connected to a
+ voice unit and radio control unit via the AC-R to the ATN network.
+
+ LDACS is considered an ATN/IPS radio access technology from the view
+ of ICAO's regulatory framework. Hence, the interface between ATN and
+ LDACS must be IPv6-based, as regulatory documents such as ICAO Doc
+ 9896 [ICAO2015] and DO-379 [RTCA2019] clearly foresee that. The
+ translation between the IPv6 layer and SNP layer is currently the
+ subject of ongoing standardization efforts and not finished yet at
+ the time of writing.
+
+ Figure 2 shows the protocol stack of LDACS as implemented in the AS
+ and GS. Acronyms used here are introduced throughout the upcoming
+ sections.
+
+ IPv6 Network Layer
+ |
+ Airborne Voice |
+ Interface (AVI) / | Radio Control Unit (RCU)
+ Voice Unit (VU) |
+ | |
+ | +------------------+ +----+
+ | | SNP |--| | Subnetwork
+ | | | | | Layer
+ | +------------------+ | |
+ | | | LME|
+ +-----+ +------------------+ | |
+ | VI | | DLS | | | LLC Layer
+ +-----+ +------------------+ +----+
+ | | |
+ DCH DCH DCCH/CCCH
+ | RACH/BCCH
+ | |
+ +-------------------------------------+
+ | MAC | Medium Access
+ | | Layer
+ +-------------------------------------+
+ |
+ +-------------------------------------+
+ | PHY | Physical Layer
+ +-------------------------------------+
+ |
+ |
+ ((*))
+ FL/RL radio channels
+ separated by FDD
+
+ Figure 2: LDACS Protocol Stack in the AS and GS
+
+7.3.1. LDACS Physical Layer
+
+ The physical layer provides the means to transfer data over the radio
+ channel. The LDACS GS supports bidirectional links to multiple
+ aircraft under its control. The FL direction at the G2A connection
+ and the RL direction at the A2G connection are separated by Frequency
+ Division Duplex (FDD). FL and RL use a 500 kHz channel each. The GS
+ transmits a continuous stream of Orthogonal Frequency Division
+ Multiplexing Access (OFDM) symbols on the FL. In the RL, different
+ aircraft are separated in time and frequency using Orthogonal
+ Frequency Division Multiple Access (OFDMA). Thus, aircraft transmit
+ discontinuously on the RL via short radio bursts sent in precisely
+ defined transmission opportunities allocated by the GS.
+
+7.3.2. LDACS Data Link Layer
+
+ The data link layer provides the necessary protocols to facilitate
+ concurrent and reliable data transfer for multiple users. The LDACS
+ data link layer is organized in two sub-layers: the medium access
+ sub-layer and the Logical Link Control (LLC) sub-layer. The medium
+ access sub-layer manages the organization of transmission
+ opportunities in slots of time and frequency. The LLC sub-layer
+ provides acknowledged point-to-point logical channels between the
+ aircraft and the GS using an Automatic Repeat reQuest (ARQ) protocol.
+ LDACS also supports unacknowledged point-to-point channels and G2A
+ broadcast transmission.
+
+7.3.2.1. Medium Access Control (MAC) Services
+
+ The MAC time framing service provides the frame structure necessary
+ to realize slot-based time-division multiplex-access on the physical
+ link. It provides the functions for the synchronization of the MAC
+ framing structure and the PHY layer framing. The MAC time framing
+ provides a dedicated time slot for each logical channel.
+
+ The MAC sub-layer offers access to the physical channel to its
+ service users. Channel access is provided through transparent
+ logical channels. The MAC sub-layer maps logical channels onto the
+ appropriate slots and manages the access to these channels. Logical
+ channels are used as interface between the MAC and LLC sub-layers.
+
+7.3.2.2. Data Link Services (DLSs)
+
+ The DLS provides acknowledged and unacknowledged (including broadcast
+ and packet mode voice) bidirectional exchange of user data. If user
+ data is transmitted using the acknowledged DLS, the sending DLS
+ entity will wait for an acknowledgement from the receiver. If no
+ acknowledgement is received within a specified time frame, the sender
+ may automatically try to retransmit its data. However, after a
+ certain number of failed retries, the sender will suspend further
+ retransmission attempts and inform its client of the failure.
+
+ The DLS uses the logical channels provided by the MAC:
+
+ 1. A GS announces its existence and access parameters in the
+ Broadcast Channel (BCCH).
+ 2. The Random-Access Channel (RACH) enables the AS to request access
+ to an LDACS cell.
+ 3. In the FL, the Common Control Channel (CCCH) is used by the GS to
+ grant access to Data Channel (DCH) resources.
+ 4. The reverse direction is covered by the RL, where ASs need to
+ request resources before sending. This happens via the Dedicated
+ Control Channel (DCCH).
+ 5. User data itself is communicated in the DCH on the FL and RL.
+
+ Access to the FL and RL DCH is granted by the scheduling mechanism
+ implemented in the LME discussed below.
+
+7.3.2.3. Voice Interface (VI) Services
+
+ The VI provides support for virtual voice circuits. Voice circuits
+ may be either set up permanently by the GS (e.g., to emulate voice
+ party line) or created on demand.
+
+7.3.2.4. LDACS Management Entity (LME) Services
+
+ The mobility management service in the LME provides support for
+ registration and de-registration (cell entry and cell exit), scanning
+ RF channels of neighboring cells, and handover between cells. In
+ addition, it manages the addressing of aircraft within cells.
+
+ The resource management service provides link maintenance (power,
+ frequency, and time adjustments), support for adaptive coding and
+ modulation, and resource allocation.
+
+ The resource management service accepts resource requests from/for
+ different ASs and issues resource allocations accordingly. While the
+ scheduling algorithm is not specified and a point of possible vendor
+ differentiation, it is subject to the following requirements:
+
+ 1. Resource scheduling must provide channel access according to the
+ priority of the request.
+ 2. Resource scheduling must support "one-time" requests.
+ 3. Resource scheduling must support "permanent" requests that
+ reserve a resource until the request is canceled (e.g., for
+ digital voice circuits).
+
+7.3.3. LDACS Subnetwork Layer and Protocol Services
+
+ Lastly, the SNP layer of LDACS directly interacts with IPv6 traffic.
+ Incoming ATN/IPS IPv6 packets are forwarded over LDACS from and to
+ the aircraft. The final IP addressing structure in an LDACS subnet
+ still needs to be defined; however, the current layout consists of
+ the five network segments: Air Core Net, Air Management Net, Ground
+ Core Net, Ground Management Net, and Ground Net. Any protocols that
+ the ATN/IPS [ICAO2015] defines as mandatory will reach the aircraft;
+ however, listing these here is out of scope. For more information on
+ the technicalities of the above ATN/IPS layer, please refer to
+ [ICAO2015], [RTCA2019], and [ARI2021].
+
+ The DLS provides functions that are required for the transfer of
+ user-plane data and control plane data over the LDACS access network.
+ The security service provides functions for secure user data
+ communication over the LDACS access network. Note that the SNP
+ security service applies cryptographic measures as configured by the
+ GS.
+
+7.4. LDACS Mobility
+
+ LDACS supports Layer 2 handovers to different LDACS cells. Handovers
+ may be initiated by the aircraft (break-before-make) or by the GS
+ (make-before-break). Make-before-break handovers are only supported
+ between GSs connected to each other and usually GSs operated by the
+ same service provider.
+
+ When a handover between the AS and two interconnected GSs takes
+ place, it can be triggered by the AS or GS. Once that is done, new
+ security information is exchanged between the AS, GS1, and GS2 before
+ the "old" connection is terminated between the AS and GS1 and a "new"
+ connection is set up between the AS and GS2. As a last step,
+ accumulated user data at GS1 is forwarded to GS2 via a ground
+ connection before it is sent via GS2 to the AS. While some
+ information for handover is transmitted in the LDACS DCH, the
+ information remains in the "control plane" part of LDACS and is
+ exchanged between LMEs in the AS, GS1, and GS2. As such, local
+ mobility takes place entirely within the LDACS network and utilizes
+ the PMIPv6 protocol [RFC5213]. The use of PMIPv6 is currently not
+ mandated by standardization and may be vendor-specific. External
+ handovers between non-connected LDACS access networks or different
+ aeronautical data links are handled by the FCI multilink concept.
+
+7.5. LDACS Management Interfaces and Protocols
+
+ LDACS management interfaces and protocols are currently not be
+ mandated by standardization. The implementations currently available
+ use SNMP for management and Radius for Authentication, Authorization,
+ and Accounting (AAA). Link state (link up, link down) is reported
+ using the ATN/IPS Aircraft Protocol (AIAP) mandated by ICAO WG-I for
+ multilink.
+
+8. Reliability and Availability
+
+8.1. Below Layer 1
+
+ Below Layer 1, aeronautics usually rely on hardware redundancy. To
+ protect availability of the LDACS link, an aircraft equipped with
+ LDACS will have access to two L-band antennae with triple redundant
+ radio systems as required for any safety relevant aeronautical
+ systems by ICAO.
+
+8.2. Layers 1 and 2
+
+ LDACS has been designed with applications related to the safety and
+ regularity of flight in mind; therefore, it has been designed as a
+ deterministic wireless data link (as far as this is possible).
+
+ Based on channel measurements of the L-band channel, LDACS was
+ designed from the PHY layer up with robustness in mind. Channel
+ measurements of the L-band channel [SCH2016] confirmed LDACS to be
+ well adapted to its channel.
+
+ In order to maximize the capacity per channel and to optimally use
+ the available spectrum, LDACS was designed as an OFDM-based FDD
+ system that supports simultaneous transmissions in FL in the G2A
+ connection and RL in the A2G connection. The legacy systems already
+ deployed in the L-band limit the bandwidth of both channels to
+ approximately 500 kHz.
+
+ The LDACS physical layer design includes propagation guard times
+ sufficient for operation at a maximum distance of 200 nautical miles
+ (nm) from the GS. In actual deployment, LDACS can be configured for
+ any range up to this maximum range.
+
+ The LDACS physical layer supports adaptive coding and modulation for
+ user data. Control data is always encoded with the most robust
+ coding and modulation (FL: Quadrature Phase-Shift Keying (QPSK),
+ coding rate 1/2; RL: QPSK, coding rate 1/3).
+
+ LDACS medium access layer on top of the physical layer uses a static
+ frame structure to support deterministic timer management. As shown
+ in Figures 3 and 4, LDACS framing structure is based on Super-Frames
+ (SFs) of 240 ms (milliseconds) duration corresponding to 2000 OFDM
+ symbols. OFDM symbol time is 120 microseconds, sampling time is 1.6
+ microseconds, and guard time is 4.8 microseconds. The structure of
+ an SF is depicted in Figure 3 along with its structure and timings of
+ each part. FL and RL boundaries are aligned in time (from the GS
+ perspective) allowing for deterministic slots for control and DCHs.
+ This initial AS time synchronization and time synchronization
+ maintenance is based on observing the synchronization symbol pairs
+ that repetitively occur within the FL stream being sent by the
+ controlling GS [GRA2020]. As already mentioned, LDACS data
+ transmission is split into user data (DCH) and control (BCCH and CCCH
+ in FL; RACH and DCCH in RL) as depicted with corresponding timings in
+ Figure 4.
+
+
+ ^
+ | +---------+------------+------------+------------+------------+
+ | FL | BCCH | MF | MF | MF | MF |
+ | | 6.72 ms | 58.32 ms | 58.32 ms | 58.32 ms | 58.32 ms |
+ F +---------+------------+------------+------------+------------+
+ r <----------------- Super-Frame (SF) - 240 ms ----------------->
+ e
+ q +---------+------------+------------+------------+------------+
+ u RL | RACH | MF | MF | MF | MF |
+ e | 6.72 ms | 58.32 ms | 58.32 ms | 58.32 ms | 58.32 ms |
+ n +---------+------------+------------+------------+------------+
+ c <----------------- Super-Frame (SF) - 240 ms ----------------->
+ y
+ ------------------------------ Time -------------------------------->
+ |
+
+ Figure 3: SF Structure for LDACS
+
+
+ ^
+ | +--------------+-----------------+------------------+
+ | FL | DCH | CCCH | DCH |
+ | | 25.92 ms | 2.16 - 17.28 ms | 15.12 - 30.24 ms |
+ F +--------------+-----------------+------------------+
+ r <----------- Multiframe (MF) - 58.32 ms ----------->
+ e
+ q +---------------+----------------------------------+
+ u RL | DCCH | DCH |
+ e | 2.8 - 24.4 ms | 33.84 - 55.44 ms |
+ n +---------------+----------------------------------+
+ c <----------- Multiframe (MF) - 58.32 ms ---------->
+ y
+ ----------------------------- Time ---------------------->
+ |
+
+ Figure 4: MF Structure for LDACS
+
+ LDACS cell entry is conducted with an initial control message
+ exchange via the RACH and the BCCH.
+
+ After cell entry, LDACS medium access is always under the control of
+ the GS of a radio cell. Any medium access for the transmission of
+ user data on a DCH has to be requested with a resource request
+ message stating the requested amount of resources and class of
+ service. The GS performs resource scheduling on the basis of these
+ requests and grants resources with resource allocation messages.
+ Resource request and allocation messages are exchanged over dedicated
+ contention-free control channels (DCCH and CCCH).
+
+ The purpose of QoS in LDACS medium access is to provide prioritized
+ medium access at the bottleneck (the wireless link). Signaling of
+ higher-layer QoS requests to LDACS is implemented on the basis of
+ Differentiated Services (Diffserv) classes CS01 (lowest priority) to
+ CS07 (highest priority).
+
+ In addition to having full control over resource scheduling, the GS
+ can send forced handover commands for off-loading or channel
+ management, e.g., when the signal quality declines and a more
+ suitable GS is in the AS's reach. With robust resource management of
+ the capacities of the radio channel, reliability and robustness
+ measures are also anchored in the LME.
+
+ In addition to radio resource management, the LDACS control channels
+ are also used to send keepalive messages when they are not otherwise
+ used. Since the framing of the control channels is deterministic,
+ missing keepalive messages can be immediately detected. This
+ information is made available to the multilink protocols for fault
+ management.
+
+ The protocol used to communicate faults is not defined in the LDACS
+ specification. It is assumed that vendors would use industry
+ standard protocols like the Simple Network Management Protocol or the
+ Network Configuration Protocol (NETCONF) where security permits.
+
+ The LDACS data link layer protocol, running on top of the medium
+ access sub-layer, uses ARQ to provide reliable data transmission on
+ the DCH. It employs selective repeat ARQ with transparent
+ fragmentation and reassembly to the resource allocation size to
+ minimize latency and overhead without losing reliability. It ensures
+ correct order of packet delivery without duplicates. In case of
+ transmission errors, it identifies lost fragments with deterministic
+ timers synced to the medium access frame structure and initiates
+ retransmission.
+
+8.3. Beyond Layer 2
+
+ LDACS availability can be increased by appropriately deploying LDACS
+ infrastructure. This means proliferating the number of terrestrial
+ GSs. However, there are four aspects that need to be taken into
+ consideration: (1) scarcity of aeronautical spectrum for data link
+ communication (tens of MHz in the L-band in the case of LDACS), (2)
+ an increase in the number of GSs also increases the individual
+ bandwidth for aircraft in the cell, as fewer aircraft have to share
+ the spectrum, (3) covering worldwide terrestrial ATM via LDACS is
+ also a question of cost and the possible reuse of spectrum, which
+ makes it not always possible to decrease cell sizes, and (4) the
+ Distance Measuring Equipment (DME) is the primary user of the
+ aeronautical L-band, which means any LDACS deployment has to take DME
+ frequency planning into account.
+
+ While aspect (2) provides a good reason alongside increasing
+ redundancy for smaller cells than the maximum range LDACS was
+ developed for (200 nm), the other three need to be respected when
+ doing so. There are preliminary works on LDACS cell planning, such
+ as [MOST2018], where the authors concluded that 84 LDACS cells in
+ Europe would be sufficient to serve European air traffic for the next
+ 20 years.
+
+ For redundancy reasons, the aeronautical community has decided not to
+ rely on a single communication system or frequency band. It is
+ envisioned to have multiple independent data link technologies in the
+ aircraft (e.g., terrestrial and satellite communications) in addition
+ to legacy VHF voice.
+
+ However, as of now, no reliability and availability mechanisms that
+ could utilize the multilink architecture have been specified on Layer
+ 3 and above. Even if LDACS has been designed for reliability, the
+ wireless medium presents significant challenges to achieve
+ deterministic properties such as low packet error rate, bounded
+ consecutive losses, and bounded latency. Support for high
+ reliability and availability for IP connectivity over LDACS is highly
+ desirable, but support needs to be adapted to the specific use case.
+
+9. Security Considerations
+
+ The goal of this section is to inform the reader about the state of
+ security in aeronautical communications and the state security
+ considerations applicable for all ATN/IPS traffic and to provide an
+ overview of the LDACS link-layer security capabilities.
+
+9.1. Security in Wireless Digital Aeronautical Communications
+
+ Aviation will require secure exchanges of data and voice messages for
+ managing the air traffic flow safely through the airspaces all over
+ the world. Historically, Communication Navigation Surveillance (CNS)
+ wireless communications technology emerged from the military and a
+ threat landscape where inferior technological and financial
+ capabilities of adversaries were assumed [STR2016]. The main
+ communications method for ATC today is still an open analog voice
+ broadcast within the aeronautical VHF band. Currently, information
+ security is mainly procedural and based by using well-trained
+ personnel and proven communications procedures. This communication
+ method has been in service since 1948. However, the world has
+ changed since the emergence of civil aeronautical CNS applications in
+ the 70s.
+
+ Civil applications have significant lower spectrum available than
+ military applications. This means that several military defense
+ mechanisms such as frequency hopping or pilot symbol scrambling (and
+ thus a defense-in-depth approach starting at the physical layer) are
+ infeasible for civil systems. With the rise of cheap Software-
+ Defined Radios (SDRs), the previously existing financial barrier is
+ almost gone, and open source projects such as GNU radio [GNU2021]
+ allow for a new type of unsophisticated listener and possible
+ attacker.
+
+ Most CNS technology developed in ICAO relies on open standards; thus,
+ syntax and semantics of wireless digital aeronautical communications
+ should be expected to be common knowledge for attackers. With
+ increased digitization and automation of civil aviation, the human as
+ control instance is being taken gradually out of the loop.
+ Autonomous transport drones or single-piloted aircraft demonstrate
+ this trend. However, without profound cybersecurity measures, such
+ as authenticity and integrity checks of messages in-transit on the
+ wireless link or mutual entity authentication, this lack of a control
+ instance can prove disastrous. Thus, future digital communications
+ will need additional embedded security features to fulfill modern
+ information security requirements like authentication and integrity.
+ These security features require sufficient bandwidth, which is beyond
+ the capabilities of currently deployed VHF narrowband communications
+ systems. For voice and data communications, sufficient data
+ throughput capability is needed to support the security functions
+ while not degrading performance. LDACS is a data link technology
+ with sufficient bandwidth to incorporate security without losing too
+ much user data throughput.
+
+9.2. Security in Depth
+
+ ICAO Doc 9896 [ICAO2015] foresees transport layer security for all
+ aeronautical data transmitted via the ATN/IPS, as described in ARINC
+ 858 [ARI2021]. This is realized via Datagram Transport Layer
+ Security (DTLS) 1.3 [RFC9147].
+
+ LDACS also needs to comply with in-depth security requirements as
+ stated in ARINC 858 for the radio access technologies transporting
+ ATN/IPS data. These requirements imply that LDACS must provide Layer
+ 2 security in addition to any higher-layer mechanisms. Specifically,
+ ARINC 858 [ARI2021] states that data links within the FCI need to
+ provide
+
+ | a secure channel between the airborne radio systems and the peer
+ | radio access endpoints on the ground [...] to ensure
+ | authentication and integrity of air-ground message exchanges in
+ | support of an overall defense-in-depth security strategy.
+
+9.3. LDACS Security Requirements
+
+ Overall, cybersecurity for CNS technology shall protect the following
+ business goals [MAE20181]:
+
+ 1. Safety: The system must sufficiently mitigate attacks that
+ contribute to safety hazards.
+ 2. Flight regularity: The system must sufficiently mitigate attacks
+ that contribute to delays, diversions, or cancelations of
+ flights.
+ 3. Protection of business interests: The system must sufficiently
+ mitigate attacks that result in financial loss, reputation
+ damage, disclosure of sensitive proprietary information, or
+ disclosure of personal information.
+
+
+ To further analyze assets, derive threats, and create protection
+ scenarios, several threat and risk analyses were performed for LDACS
+ [MAE20181] [MAE20191]. These results allowed the derivation of
+ security scope and objectives from the requirements and the conducted
+ threat and risk analysis. Note, IPv6 security considerations are
+ briefly discussed in Section 9.7 while a summary of security
+ requirements for link-layer candidates in the ATN/IPS is given in
+ [ARI2021], which states:
+
+ | Since the communication radios connect to local airborne networks
+ | in the aircraft control domain, [...] the airborne radio systems
+ | represent the first point of entry for an external threat to the
+ | aircraft. Consequently, a secure channel between the airborne
+ | radio systems and the peer radio access endpoints on the ground is
+ | necessary to ensure authentication and integrity of air-ground
+ | message exchanges in support of an overall defense-in-depth
+ | security strategy.
+
+9.4. LDACS Security Objectives
+
+ Security considerations for LDACS are defined by the official SARPS
+ document by ICAO [ICAO2022]:
+
+ * LDACS shall provide a capability to protect the availability and
+ continuity of the system.
+ * LDACS shall provide a capability including cryptographic
+ mechanisms to protect the integrity of messages in transit.
+ * LDACS shall provide a capability to ensure the authenticity of
+ messages in transit.
+ * LDACS should provide a capability for non-repudiation of origin
+ for messages in transit.
+ * LDACS should provide a capability to protect the confidentiality
+ of messages in transit.
+ * LDACS shall provide an authentication capability.
+ * LDACS shall provide a capability to authorize the permitted
+ actions of users of the system and to deny actions that are not
+ explicitly authorized.
+ * If LDACS provides interfaces to multiple domains, LDACS shall
+ provide capability to prevent the propagation of intrusions within
+ LDACS domains and towards external domains.
+
+
+ Work in 2022 includes a change request for these SARPS aims to limit
+ the "non-repudiation of origin of messages in transit" requirement
+ only to the authentication and key establishment messages at the
+ beginning of every session.
+
+9.5. LDACS Security Functions
+
+ These objectives were used to derive several security functions for
+ LDACS required to be integrated in the LDACS cybersecurity
+ architecture: Identification, Authentication, Authorization,
+ Confidentiality, System Integrity, Data Integrity, Robustness,
+ Reliability, Availability, and Key and Trust Management. Several
+ works investigated possible measures to implement these security
+ functions [BIL2017] [MAE20181] [MAE20191].
+
+9.6. LDACS Security Architecture
+
+ The requirements lead to an LDACS security model, including different
+ entities for identification, authentication, and authorization
+ purposes ensuring integrity, authenticity, and confidentiality of
+ data. A draft of the cybersecurity architecture of LDACS can be
+ found in [ICAO2022] and [MAE20182], and respective updates can be
+ found in [MAE20191], [MAE20192], [MAE2020], and [MAE2021].
+
+9.6.1. Entities
+
+ A simplified LDACS architectural model requires the following
+ entities: network operators such as the Societe Internationale de
+ Telecommunications Aeronautiques (SITA) [SIT2020] and ARINC
+ [ARI2020]; both entities provide access to the ground IPS network via
+ an A/G LDACS router. This router is attached to an internal LDACS
+ access network that connects via further AC-Rs to the different LDACS
+ cell ranges, each controlled by a GS (serving one LDACS cell), with
+ several interconnected GSs spanning a local LDACS access network.
+ Via the A/G wireless LDACS data link AS, the aircraft is connected to
+ the ground network. Via the aircraft's VI and network interface, the
+ aircraft's data can be sent via the AS back to the GS, then to the
+ LDACS local access network, AC-Rs, LDACS access network, A/G LDACS
+ router, and finally to the ground IPS network [ICAO2015].
+
+9.6.2. Entity Identification
+
+ LDACS needs specific identities for the AS, the GS, and the network
+ operator. The aircraft itself can be identified using the 24-bit
+ ICAO identifier of an aircraft [ICAO2022], the call sign of that
+ aircraft, or the recently founded privacy ICAO address of the Federal
+ Aviation Administration (FAA) program with the same name [FAA2020].
+ It is conceivable that the LDACS AS will use a combination of
+ aircraft identification, radio component identification, and even
+ operator feature identification to create a unique LDACS AS
+ identification tag. Similar to a 4G's eNodeB-serving network
+ identification tag, a GS could be identified using a similar field.
+ The identification of the network operator is similar to 4G (e.g.,
+ E-Plus, AT&T, and TELUS), in the way that the aeronautical network
+ operators are listed (e.g., ARINC [ARI2020] and SITA [SIT2020]).
+
+9.6.3. Entity Authentication and Key Establishment
+
+ In order to anchor trust within the system, all LDACS entities
+ connected to the ground IPS network will be rooted in an LDACS-
+ specific chain-of-trust and PKI solution, quite similar to AeroMACS's
+ approach [CRO2016]. These certificates, residing at the entities and
+ incorporated in the LDACS PKI, provide proof of the ownership of
+ their respective public key and include information about the
+ identity of the owner and the digital signature of the entity that
+ has verified the certificate's content. First, all ground
+ infrastructures must mutually authenticate to each other, negotiate
+ and derive keys, and then secure all ground connections. How this
+ process is handled in detail is still an ongoing discussion.
+ However, established methods to secure the user plane by IPsec
+ [RFC4301] and IKEv2 [RFC7296] or the application layer via TLS 1.3
+ [RFC8446] are conceivable. The LDACS PKI with its chain-of-trust
+ approach, digital certificates, and public entity keys lay the
+ groundwork for this step. In a second step, the AS with the LDACS
+ radio aboard approaches an LDACS cell and performs a cell-attachment
+ procedure with the corresponding GS. This procedure consists of (1)
+ the basic cell entry [GRA2020] and (2) a MAKE procedure [MAE2021].
+
+ Note that LDACS will foresee multiple security levels. To address
+ the issue of the long service life of LDACS (i.e., possibly greater
+ than 30 years) and the security of current pre-quantum cryptography,
+ these security levels include pre-quantum and post-quantum
+ cryptographic solutions. Limiting security data on the LDACS data
+ link as much as possible to reserve as much space for actual user
+ data transmission is key in the LDACS security architecture. This is
+ also reflected in the underlying cryptography. Pre-quantum solutions
+ will rely on elliptic curves [NIST2013], while post-quantum solutions
+ consider Falcon [SON2021] [MAE2021] or similar lightweight PQC
+ signature schemes and CRYSTALS-KYBER or SABER as key establishment
+ options [AVA2021] [ROY2020].
+
+9.6.4. Message-In-Transit Confidentiality, Integrity, and Authenticity
+
+ The key material from the previous step can then be used to protect
+ LDACS Layer 2 communications via applying encryption and integrity
+ protection measures on the SNP layer of the LDACS protocol stack. As
+ LDACS transports AOC and ATS data, the integrity of that data is most
+ important while confidentiality only needs to be applied to AOC data
+ to protect business interests [ICAO2022]. This possibility of
+ providing low-layered confidentiality and integrity protection
+ ensures a secure delivery of user data over the wireless link.
+ Furthermore, it ensures integrity protection of LDACS control data.
+
+9.7. Considerations on LDACS Security Impact on IPv6 Operational
+ Security
+
+ In this part, considerations on IPv6 operational security in
+ [RFC9099] and interrelations with the LDACS security additions are
+ compared and evaluated to identify further protection demands. As
+ IPv6 heavily relies on the Neighbor Discovery Protocol (NDP)
+ [RFC4861], integrity and authenticity protection on the link layer,
+ as provided by LDACS, already help mitigate spoofing and redirection
+ attacks. However, to also mitigate the threat of remote DDoS
+ attacks, neighbor solicitation rate-limiting is recommended by
+ [RFC9099]. To prevent the threat of DDoS and DoS attacks in general
+ on the LDACS access network, rate-limiting needs to be performed on
+ each network node in the LDACS access network. One approach is to
+ filter for the total amount of possible LDACS AS-GS traffic per cell
+ (i.e., of up to 1.4 Mbit/s user data per cell and up to the amount of
+ GS per service provider network times 1.4 Mbit/s).
+
+10. IANA Considerations
+
+ This document has no IANA actions.
+
+11. Informative References
+
+ [ARI2019] ARINC, "AOC AIR-GROUND DATA AND MESSAGE EXCHANGE FORMAT",
+ ARINC 633, January 2019,
+ <https://standards.globalspec.com/std/13152055/
+ ARINC%20633>.
+
+ [ARI2020] "Aeronautical Radio Incorporated (ARINC) Industry
+ Activities", <https://www.aviation-ia.com/>.
+
+ [ARI2021] ARINC, "INTERNET PROTOCOL SUITE (IPS) FOR AERONAUTICAL
+ SAFETY SERVICES PART 1 AIRBORNE IPS SYSTEM TECHNICAL
+ REQUIREMENTS", ARINC 858P1, June 2021,
+ <https://standards.globalspec.com/std/14391274/858p1>.
+
+ [AVA2021] Avanzi, R., Bos, J., Ducas, L., Kiltz, E., Lepoint, T.,
+ Lyubashevsky, V., Schanck, J.M., Schwabe, P., Seiler, G.,
+ and D. Stehlé, "CRYSTALS-KYBER - Algorithm Specification
+ and Supporting Documentation (version 3.02)", August 2021,
+ <https://pq-crystals.org/kyber/data/kyber-specification-
+ round3-20210804.pdf>.
+
+ [BEL2019] Bellido-Manganell, M. A. and M. Schnell, "Towards Modern
+ Air-to-Air Communications: the LDACS A2A Mode", IEEE/AIAA
+ 38th Digital Avionics Systems Conference (DASC), pp. 1-10,
+ DOI 10.1109/DASC43569.2019.9081678, September 2019,
+ <https://doi.org/10.1109/DASC43569.2019.9081678>.
+
+ [BEL2021] Bellido-Manganell, M.A., Gräupl, T., Heirich, O., Mäurer,
+ N., Filip-Dhaubhadel, A., Mielke, D.M., Schalk, L.M.,
+ Becker, D., Schneckenburger, N., and M. Schnell, "LDACS
+ Flight Trials: Demonstration and Performance Analysis of
+ the Future Aeronautical Communications System", IEEE
+ Transactions on Aerospace and Electronic Systems, Vol. 58,
+ Issue 1, pp. 615-634, DOI 10.1109/TAES.2021.3111722,
+ September 2021,
+ <https://doi.org/10.1109/TAES.2021.3111722>.
+
+ [BIL2017] Bilzhause, A., Belgacem, B., Mostafa, M., and T. Gräupl,
+ "Datalink security in the L-band digital aeronautical
+ communications system (LDACS) for air traffic management",
+ IEEE Aerospace and Electronic Systems Magazine, Vol. 32,
+ Issue 11, pp. 22-33, DOI 10.1109/MAES.2017.160282,
+ November 2017, <https://doi.org/10.1109/MAES.2017.160282>.
+
+ [BOE2019] Boegl, T., Rautenberg, M., Haindl, R., Rihacek, C., Meser,
+ J., Fantappie, P., Pringvanich, N., Micallef, J., Hauf,
+ K., MacBride, J., Sacre, P., v.d. Eiden, B., Gräupl, T.,
+ and M. Schnell, "LDACS White Paper - A Roll-out Scenario",
+ International Civil Aviation Organization, Communications
+ Panel - Data Communications Infrastructure Working Group -
+ Third Meeting, pp. 1-8, October 2019.
+
+ [CRO2016] Crowe, B., "Proposed AeroMACS PKI specification is a model
+ for global and National Aeronautical PKI Deployments",
+ Integrated Communications, Navigation and Surveillance
+ Conference (ICNS), pp. 1-19,
+ DOI 10.1109/ICNSURV.2016.7486405, April 2016,
+ <https://doi.org/10.1109/ICNSURV.2016.7486405>.
+
+ [DO350A] RTCA, "Safety and Performance Requirements Standard for
+ Baseline 2 ATS Data Communications (Baseline 2 SPR
+ Standard)", Vol. 1 & 2, RTCA DO-350, March 2016,
+ <https://standards.globalspec.com/std/10003192/rtca-do-
+ 350-volume-1-2>.
+
+ [EURO2019] European Organization for Civil Aviation Equipment
+ (EUROCAE), "Technical Standard of Aviation Profiles for
+ ATN/IPS", ED 262, September 2019,
+ <https://eshop.eurocae.net/eurocae-documents-and-reports/
+ ed-262/>.
+
+ [FAA2020] Federal Aviation Administration, "ADS-B Privacy", February
+ 2023,
+ <https://www.faa.gov/air_traffic/technology/equipadsb/
+ privacy>.
+
+ [GNU2021] GNU Radio Project, "GNU Radio", <http://gnuradio.org>.
+
+ [GRA2011] Gräupl, T. and M. Ehammer, "LDACS1 data link layer
+ evolution for ATN/IPS", IEEE/AIAA 30th Digital Avionics
+ Systems Conference (DASC), pp. 1-28,
+ DOI 10.1109/DASC.2011.6096230, October 2011,
+ <https://doi.org/10.1109/DASC.2011.6096230>.
+
+ [GRA2018] Gräupl, T., Schneckenburger, N., Jost, T., Schnell, M.,
+ Filip, A., Bellido-Manganell, M.A., Mielke, D.M., Mäurer,
+ N., Kumar, R., Osechas, O., and G. Battista, "L-band
+ Digital Aeronautical Communications System (LDACS) flight
+ trials in the national German project MICONAV", Integrated
+ Communications, Navigation, Surveillance Conference
+ (ICNS), pp. 1-7, DOI 10.1109/ICNSURV.2018.8384881, April
+ 2018, <https://doi.org/10.1109/ICNSURV.2018.8384881>.
+
+ [GRA2020] Gräupl, T., "Initial LDACS A/G Specification", SESAR2020
+ - PJ14-W2-60, D3.1.210, December 2020,
+ <https://www.ldacs.com/wp-content/uploads/2013/12/SESAR202
+ 0_PJ14-W2-60_D3_1_210_Initial_LDACS_AG_Specification_00_01
+ _00-1_0_updated.pdf>.
+
+ [ICAO2015] International Civil Aviation Organization (ICAO), "Manual
+ on the Aeronautical Telecommunication Network (ATN) using
+ Internet Protocol Suite (IPS) Standards and Protocol",
+ ICAO 9896, January 2015,
+ <https://standards.globalspec.com/std/10026940/icao-9896>.
+
+ [ICAO2018] International Civil Aviation Organization (ICAO),
+ "Handbook on Radio Frequency Spectrum Requirements for
+ Civil Aviation", Vol. 1, ICAO Spectrum Strategy, Policy
+ Statements and Related Information, Doc 9718, AN/957, July
+ 2018, <https://www.icao.int/safety/FSMP/Documents/Doc9718/
+ Doc.9718%20Vol.%20I%20(AdvanceUneditedVersion%202021).pdf>
+ .
+
+ [ICAO2019] International Civil Aviation Organization (ICAO), "Manual
+ on VHF Digital Link (VDL) Mode 2", Second Edition,
+ Doc 9776, 2015, <https://store.icao.int/en/manual-on-vhf-
+ digital-link-vdl-mode-2-doc-9776>.
+
+ [ICAO2022] International Civil Aviation Organization (ICAO), "CHAPTER
+ 13 L-Band Digital Aeronautical Communications System
+ (LDACS)", International Standards and Recommended
+ Practices, Annex 10 - Aeronautical Telecommunications,
+ Volume III, Communication Systems, 2022,
+ <https://www.ldacs.com/wp-content/uploads/2023/03/
+ WP06.AppA-DCIWG-6-LDACS_SARPs.pdf>.
+
+ [KAMA2010] Kamali, B., "An overview of VHF civil radio network and
+ the resolution of spectrum depletion", Integrated
+ Communications, Navigation, and Surveillance Conference,
+ pp. F4-1-F4-8, DOI 10.1109/ICNSURV.2010.5503256, May 2010,
+ <https://doi.org/10.1109/ICNSURV.2010.5503256>.
+
+ [KAMA2018] Kamali, B., "AeroMACS: An IEEE 802.16 Standard-Based
+ Technology for the Next Generation of Air Transportation
+ Systems", DOI 10.1002/9781119281139, September 2018,
+ <https://doi.org/10.1002/9781119281139>.
+
+ [LISP-GB-ATN]
+ Haindl, B., Lindner, M., Moreno, V., Portoles-Comeras, M.,
+ Maino, F., and B. Venkatachalapathy, "Ground-Based LISP
+ for the Aeronautical Telecommunications Network", Work in
+ Progress, Internet-Draft, draft-haindl-lisp-gb-atn-08, 23
+ September 2022, <https://datatracker.ietf.org/doc/html/
+ draft-haindl-lisp-gb-atn-08>.
+
+ [MAE20181] Mäurer, N. and A. Bilzhause, "Paving the way for an it
+ security architecture for LDACS: A datalink security
+ threat and risk analysis", IEEE Integrated Communications,
+ Navigation, Surveillance Conference (ICNS), pp. 1-11,
+ DOI 10.1109/ICNSURV.2018.8384828, April 2018,
+ <https://doi.org/10.1109/ICNSURV.2018.8384828>.
+
+ [MAE20182] Mäurer, N. and A. Bilzhause, "A Cybersecurity Architecture
+ for the L-band Digital Aeronautical Communications System
+ (LDACS)", IEEE/AIAA 37th Digital Avionics Systems
+ Conference (DASC), pp. 1-10,
+ DOI 10.1109/DASC.2018.8569878, September 2018,
+ <https://doi.org/10.1109/DASC.2018.8569878>.
+
+ [MAE20191] Mäurer, N., Gräupl, T., and C. Schmitt, "Evaluation of the
+ LDACS Cybersecurity Implementation", IEEE 38th Digital
+ Avionics Systems Conference (DASC), pp. 1-10,
+ DOI 10.1109/DASC43569.2019.9081786, September 2019,
+ <https://doi.org/10.1109/DASC43569.2019.9081786>.
+
+ [MAE20192] Mäurer, N. and C. Schmitt, "Towards Successful Realization
+ of the LDACS Cybersecurity Architecture: An Updated
+ Datalink Security Threat- and Risk Analysis", IEEE
+ Integrated Communications, Navigation and Surveillance
+ Conference (ICNS), pp. 1-13,
+ DOI 10.1109/ICNSURV.2019.8735139, April 2019,
+ <https://doi.org/10.1109/ICNSURV.2019.8735139>.
+
+ [MAE2020] Mäurer, N., Gräupl, T., Gentsch, C., and C. Schmitt,
+ "Comparing Different Diffie-Hellman Key Exchange Flavors
+ for LDACS", IEEE/AIAA 39th Digital Avionics Systems
+ Conference (DASC), pp. 1-10,
+ DOI 10.1109/DASC50938.2020.9256746, October 2020,
+ <https://doi.org/10.1109/DASC50938.2020.9256746>.
+
+ [MAE2021] Mäurer, N., Gräupl, T., Gentsch, C., Guggemos, T.,
+ Tiepelt, M., Schmitt, C., and G. Dreo Rodosek, "A Secure
+ Cell-Attachment Procedure for LDACS", IEEE European
+ Symposium on Security and Privacy Workshops (EuroS&PW),
+ pp. 1-10, DOI 10.1109/EuroSPW54576.2021.00019, September
+ 2021, <https://doi.org/10.1109/EuroSPW54576.2021.00019>.
+
+ [MAE20211] Mäurer, N., Gräupl, T., Bellido-Manganell, M.A., Mielke,
+ D.M., Filip-Dhaubhadel, A., Heirich, O., Gerberth, D.,
+ Felux, M., Schalk, L.M., Becker, D., Schneckenburger, N.,
+ and M. Schnell, "Flight Trial Demonstration of Secure GBAS
+ via the L-band Digital Aeronautical Communications System
+ (LDACS)", IEEE Aerospace and Electronic Systems Magazine,
+ Vol. 36, Issue 4, pp. 8-17, DOI 10.1109/MAES.2021.3052318,
+ April 2021, <https://doi.org/10.1109/MAES.2021.3052318>.
+
+ [MOST2018] Mostafa, M., Bellido-Manganell, M.A.., and T. Gräupl,
+ "Feasibility of Cell Planning for the L-Band Digital
+ Aeronautical Communications System Under the Constraint of
+ Secondary Spectrum Usage", IEEE Transactions on Vehicular
+ Technology, Vol. 67, Issue 10, pp. 9721-9733,
+ DOI 10.1109/TVT.2018.2862829, October 2018,
+ <https://doi.org/10.1109/TVT.2018.2862829>.
+
+ [NIST2013] National Institute of Standards and Technology (NIST),
+ "Digital Signature Standard (DSS)", FIPS PUB 186-4,
+ DOI 10.6028/NIST.FIPS.186-4, July 2013,
+ <https://doi.org/10.6028/NIST.FIPS.186-4>.
+
+ [OSE2019] Osechas, O., Narayanan, S., Crespillo, O.G., Zampieri, G.,
+ Battista, G., Kumar, R., Schneckenburger, N., Lay, E.,
+ Belabbas, B., and M. Meurer, "Feasibility Demonstration of
+ Terrestrial RNP with LDACS", 32nd International Technical
+ Meeting of the Satellite Division of The Institute of
+ Navigation, pp. 3254-3265, DOI 10.33012/2019.17119,
+ September 2019, <https://doi.org/10.33012/2019.17119>.
+
+ [RAW-TECHNOS]
+ Thubert, P., Ed., Cavalcanti, D., Vilajosana, X., Schmitt,
+ C., and J. Farkas, "Reliable and Available Wireless
+ Technologies", Work in Progress, Internet-Draft, draft-
+ ietf-raw-technologies-06, 30 November 2022,
+ <https://datatracker.ietf.org/doc/html/draft-ietf-raw-
+ technologies-06>.
+
+ [RAW-USE-CASES]
+ Bernardos, C. J., Ed., Papadopoulos, G. Z., Thubert, P.,
+ and F. Theoleyre, "RAW Use-Cases", Work in Progress,
+ Internet-Draft, draft-ietf-raw-use-cases-09, 13 March
+ 2023, <https://datatracker.ietf.org/doc/html/draft-ietf-
+ raw-use-cases-08>.
+
+ [RFC4301] Kent, S. and K. Seo, "Security Architecture for the
+ Internet Protocol", RFC 4301, DOI 10.17487/RFC4301,
+ December 2005, <https://www.rfc-editor.org/info/rfc4301>.
+
+ [RFC4861] Narten, T., Nordmark, E., Simpson, W., and H. Soliman,
+ "Neighbor Discovery for IP version 6 (IPv6)", RFC 4861,
+ DOI 10.17487/RFC4861, September 2007,
+ <https://www.rfc-editor.org/info/rfc4861>.
+
+ [RFC5213] Gundavelli, S., Ed., Leung, K., Devarapalli, V.,
+ Chowdhury, K., and B. Patil, "Proxy Mobile IPv6",
+ RFC 5213, DOI 10.17487/RFC5213, August 2008,
+ <https://www.rfc-editor.org/info/rfc5213>.
+
+ [RFC5795] Sandlund, K., Pelletier, G., and L. Jonsson, "The RObust
+ Header Compression (ROHC) Framework", RFC 5795,
+ DOI 10.17487/RFC5795, March 2010,
+ <https://www.rfc-editor.org/info/rfc5795>.
+
+ [RFC7296] Kaufman, C., Hoffman, P., Nir, Y., Eronen, P., and T.
+ Kivinen, "Internet Key Exchange Protocol Version 2
+ (IKEv2)", STD 79, RFC 7296, DOI 10.17487/RFC7296, October
+ 2014, <https://www.rfc-editor.org/info/rfc7296>.
+
+ [RFC8200] Deering, S. and R. Hinden, "Internet Protocol, Version 6
+ (IPv6) Specification", STD 86, RFC 8200,
+ DOI 10.17487/RFC8200, July 2017,
+ <https://www.rfc-editor.org/info/rfc8200>.
+
+ [RFC8446] Rescorla, E., "The Transport Layer Security (TLS) Protocol
+ Version 1.3", RFC 8446, DOI 10.17487/RFC8446, August 2018,
+ <https://www.rfc-editor.org/info/rfc8446>.
+
+ [RFC9099] Vyncke, É., Chittimaneni, K., Kaeo, M., and E. Rey,
+ "Operational Security Considerations for IPv6 Networks",
+ RFC 9099, DOI 10.17487/RFC9099, August 2021,
+ <https://www.rfc-editor.org/info/rfc9099>.
+
+ [RFC9147] Rescorla, E., Tschofenig, H., and N. Modadugu, "The
+ Datagram Transport Layer Security (DTLS) Protocol Version
+ 1.3", RFC 9147, DOI 10.17487/RFC9147, April 2022,
+ <https://www.rfc-editor.org/info/rfc9147>.
+
+ [RFC9300] Farinacci, D., Fuller, V., Meyer, D., Lewis, D., and A.
+ Cabellos, Ed., "The Locator/ID Separation Protocol
+ (LISP)", RFC 9300, DOI 10.17487/RFC9300, October 2022,
+ <https://www.rfc-editor.org/info/rfc9300>.
+
+ [RFC9301] Farinacci, D., Maino, F., Fuller, V., and A. Cabellos,
+ Ed., "Locator/ID Separation Protocol (LISP) Control
+ Plane", RFC 9301, DOI 10.17487/RFC9301, October 2022,
+ <https://www.rfc-editor.org/info/rfc9301>.
+
+ [RIH2018] Rihacek, C., Haindl, B., Fantappie, P., Pierattelli, S.,
+ Gräupl, T., Schnell, M., and N. Fistas, "L-band Digital
+ Aeronautical Communications System (LDACS) activities in
+ SESAR2020", Integrated Communications Navigation and
+ Surveillance Conference (ICNS), pp. 1-8,
+ DOI 10.1109/ICNSURV.2018.8384880, April 2018,
+ <https://doi.org/10.1109/ICNSURV.2018.8384880>.
+
+ [ROY2020] Roy, S.S. and A. Basso, "High-speed Instruction-set
+ Coprocessor for Lattice-based Key Encapsulation Mechanism:
+ Saber in Hardware", IACR Transactions on Cryptographic
+ Hardware and Embedded Systems, Vol. 2020, Issue 4, pp.
+ 443-466, DOI 10.13154/tches.v2020.i4.443-466, August 2020,
+ <https://doi.org/10.13154/tches.v2020.i4.443-466>.
+
+ [RTCA2019] Radio Technical Commission for Aeronautics (RTCA),
+ "Internet Protocol Suite Profiles", RTCA DO-379, September
+ 2019, <https://standards.globalspec.com/std/14224450/rtca-
+ do-379>.
+
+ [RTGWG-ATN-BGP]
+ Templin, F., Ed., Saccone, G., Dawra, G., Lindem, A., and
+ V. Moreno, "A Simple BGP-based Mobile Routing System for
+ the Aeronautical Telecommunications Network", Work in
+ Progress, Internet-Draft, draft-ietf-rtgwg-atn-bgp-19, 7
+ November 2022, <https://datatracker.ietf.org/doc/html/
+ draft-ietf-rtgwg-atn-bgp-19>.
+
+ [SAJ2014] Haindl, B., Meser, J., Sajatovic, M., Müller, S.,
+ Arthaber, H., Faseth, T., and M. Zaisberger, "LDACS1
+ conformance and compatibility assessment", IEEE/AIAA 33rd
+ Digital Avionics Systems Conference (DASC), pp. 1-11,
+ DOI 10.1109/DASC.2014.6979447, October 2014,
+ <https://doi.org/10.1109/DASC.2014.6979447>.
+
+ [SCH2016] Schneckenburger, N., Jost, T., Shutin, D., Walter, M.,
+ Thiasiriphet, T., Schnell, M., and U.C. Fiebig,
+ "Measurement of the l-band air-to-ground channel for
+ positioning applications", IEEE Transactions on Aerospace
+ and Electronic Systems, Vol. 52, Issue 5, pp. 2281-2297,
+ DOI 10.1109/TAES.2016.150451, October 2016,
+ <https://doi.org/10.1109/TAES.2016.150451>.
+
+ [SCHN2018] Schneckenburger, N., "A Wide-Band Air-Ground Channel
+ Model", Dissertation, Technischen Universitaet Ilmenau,
+ February 2018.
+
+ [SHU2013] Shutin, D., Schneckenburger, N., Walter, M., and M.
+ Schnell, "LDACS1 ranging performance - An analysis of
+ flight measurement results", IEEE 32nd Digital Avionics
+ Systems Conference (DASC), pp. 1-10,
+ DOI 10.1109/DASC.2013.6712567, October 2013,
+ <https://doi.org/10.1109/DASC.2013.6712567>.
+
+ [SIT2020] "Societe Internationale de Telecommunica Aéronautique
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+ and R. Karri, "FALCON", Hardware Architectures for Post-
+ Quantum Digital Signature Schemes, pp. 31-41,
+ DOI 10.1007/978-3-030-57682-0_3, 2021,
+ <https://doi.org/10.1007/978-3-030-57682-0_3>.
+
+ [STR2016] Strohmeier, M., Schäfer, M., Pinheiro, R., Lenders, V.,
+ and I. Martinovic, "On Perception and Reality in Wireless
+ Air Traffic Communication Security", IEEE Transactions on
+ Intelligent Transportation Systems, Vol. 18, Issue 6, pp.
+ 1338-1357, DOI 10.1109/TITS.2016.2612584, October 2016,
+ <https://doi.org/10.1109/TITS.2016.2612584>.
+
+ [VIR2021] Virdia, A., Stea, G., and G. Dini, "SAPIENT: Enabling
+ Real-Time Monitoring and Control in the Future
+ Communication Infrastructure of Air Traffic Management",
+ IEEE Transactions on Intelligent Transportation Systems,
+ Vol. 22, Issue 8, pp. 4864-4875,
+ DOI 10.1109/TITS.2020.2983614, August 2021,
+ <https://doi.org/10.1109/TITS.2020.2983614>.
+
+Appendix A. Selected Information from DO-350A
+
+ This appendix includes the continuity, availability, and integrity
+ requirements applicable for LDACS defined in [DO350A].
+
+ The following terms are used here:
+
+ CPDLC: Controller-Pilot Data Link Communications
+ DT: Delivery Time (nominal) value for RSP
+ ET: Expiration Time value for RCP
+ FH: Flight Hour
+ MA: Monitoring and Alerting criteria
+ OT: Overdue Delivery Time value for RSP
+ RCP: Required Communication Performance
+ RSP: Required Surveillance Performance
+ TT: Transaction Time (nominal) value for RCP
+
+
+ +========================+=============+=============+
+ | | RCP 130 | RCP 130 |
+ +========================+=============+=============+
+ | Parameter | ET | TT95% |
+ +------------------------+-------------+-------------+
+ | Transaction Time (sec) | 130 | 67 |
+ +------------------------+-------------+-------------+
+ | Continuity | 0.999 | 0.95 |
+ +------------------------+-------------+-------------+
+ | Availability | 0.989 | 0.989 |
+ +------------------------+-------------+-------------+
+ | Integrity | 1E-5 per FH | 1E-5 per FH |
+ +------------------------+-------------+-------------+
+
+ Table 1: CPDLC Requirements for RCP 130
+
+ +========================+=========+=========+=========+=========+
+ | | RCP 240 | RCP 240 | RCP 400 | RCP 400 |
+ +========================+=========+=========+=========+=========+
+ | Parameter | ET | TT95% | ET | TT95% |
+ +------------------------+---------+---------+---------+---------+
+ | Transaction Time (sec) | 240 | 210 | 400 | 350 |
+ +------------------------+---------+---------+---------+---------+
+ | Continuity | 0.999 | 0.95 | 0.999 | 0.95 |
+ +------------------------+---------+---------+---------+---------+
+ | Availability | 0.989 | 0.989 | 0.989 | 0.989 |
+ +------------------------+---------+---------+---------+---------+
+ | Integrity | 1E-5 | 1E-5 | 1E-5 | 1E-5 |
+ | | per FH | per FH | per FH | per FH |
+ +------------------------+---------+---------+---------+---------+
+
+ Table 2: CPDLC Requirements for RCP 240/400
+
+ RCP Monitoring and Alerting Criteria in case of CPDLC:
+
+ MA-1: The system shall be capable of detecting failures and
+ configuration changes that would cause the communication service
+ to no longer meet the RCP specification for the intended use.
+ MA-2: When the communication service can no longer meet the RCP
+ specification for the intended function, the flight crew and/or
+ the controller shall take appropriate action.
+
+
+ +==============+========+========+========+========+========+=======+
+ | | RSP | RSP | RSP | RSP | RSP | RSP |
+ | | 160 | 160 | 180 | 180 | 400 | 400 |
+ +==============+========+========+========+========+========+=======+
+ | Parameter | OT | DT95% | OT | DT95% | OT | DT95% |
+ +--------------+--------+--------+--------+--------+--------+-------+
+ | Transaction | 160 | 90 | 180 | 90 | 400 | 300 |
+ | Time (sec) | | | | | | |
+ +--------------+--------+--------+--------+--------+--------+-------+
+ | Continuity | 0.999 | 0.95 | 0.999 | 0.95 | 0.999 | 0.95 |
+ +--------------+--------+--------+--------+--------+--------+-------+
+ | Availability | 0.989 | 0.989 | 0.989 | 0.989 | 0.989 | 0.989 |
+ +--------------+--------+--------+--------+--------+--------+-------+
+ | Integrity | 1E-5 | 1E-5 | 1E-5 | 1E-5 | 1E-5 | 1E-5 |
+ | | per FH | per FH | per FH | per FH | per | per |
+ | | | | | | FH | FH |
+ +--------------+--------+--------+--------+--------+--------+-------+
+
+ Table 3: ADS-C Requirements
+
+ RCP Monitoring and Alerting Criteria:
+
+ MA-1: The system shall be capable of detecting failures and
+ configuration changes that would cause the ADS-C service to no
+ longer meet the RSP specification for the intended function.
+ MA-2: When the ADS-C service can no longer meet the RSP
+ specification for the intended function, the flight crew and/or
+ the controller shall take appropriate action.
+
+
+Acknowledgements
+
+ Thanks to all contributors to the development of LDACS and ICAO
+ Project Team Terrestrial (PT-T), as well as to all in the RAW Working
+ Group for deep discussions and feedback.
+
+ Thanks to Klaus-Peter Hauf, Bart Van Den Einden, and Pierluigi
+ Fantappie for their comments on this document.
+
+ Thanks to the Chair of Network Security for input and to the Research
+ Institute CODE for their comments and improvements.
+
+ Thanks to the colleagues of the Research Institute CODE at the
+ UniBwM, who are working on the AMIUS project funded under the
+ Bavarian Aerospace Program by the Bavarian State Ministry of
+ Economics, Regional Development and Energy with the GA ROB-
+ 2-3410.20-04-11-15/HAMI-2109-0015, for fruitful discussions on
+ aeronautical communications and relevant security incentives for the
+ target market.
+
+ Thanks to SBA Research Vienna for continuous discussions on security
+ infrastructure issues in quickly developing markets such as the air
+ space and potential economic spillovers to used technologies and
+ protocols.
+
+ Thanks to the Aeronautical Communications group at the Institute of
+ Communications and Navigation of the German Aerospace Center (DLR).
+ With that, the authors would like to explicitly thank Miguel Angel
+ Bellido-Manganell and Lukas Marcel Schalk for their thorough
+ feedback.
+
+Authors' Addresses
+
+ Nils Mäurer (editor)
+ German Aerospace Center (DLR)
+ Münchner Strasse 20
+ 82234 Wessling
+ Germany
+ Email: Nils.Maeurer@dlr.de
+
+
+ Thomas Gräupl (editor)
+ German Aerospace Center (DLR)
+ Münchner Strasse 20
+ 82234 Wessling
+ Germany
+ Email: Thomas.Graeupl@dlr.de
+
+
+ Corinna Schmitt (editor)
+ Research Institute CODE, UniBwM
+ Werner-Heisenberg-Weg 39
+ 85577 Neubiberg
+ Germany
+ Email: corinna.schmitt@unibw.de