Honeywell Mark III manual Atn, Rri, Encryption/Authentication

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support as part of the baseline the text Weather uplinks which has become standard use within the Air transport industry.

ATN

The industry has embarked on the definition of a new communications standard named the Aeronautical Telecommunications Network (ATN). The ATN offers a standardized, robust, and efficient communications mechanism that provides additional services. Honeywell has been a leading member of the international consortium, Aeronautical Communication Inc. (ACI) developing this new communications software. The ATN is the ICAO defined solution to be used world wide as the industry transitions much of today’s ATC voice communication to datalink in the years ahead.

ACI has developed both the Router Reference Implementation (RRI), which is the communications stack, and the Application Service Elements (ASEs), which are the algorithmic portion of the CNS/ATM-1 applications. ASEs have been developed for Controller Pilot Data Link Communications (CPDLC), Automatic Dependent Surveillance (ADS), Context Management (CM) and Flight Information Services (FIS). ACI developed both the RRI and the ASEs to be portable and therefore readily hostable in a number of different target environments, both in avionics and ground systems. An integrator would only have to port the RRI & ASEs to the target environment and then add the display portion of the applications along with subnetwork- specific interfaces (see Figure 9).

Applications

ASEs

RRI

Subnetworks

Figure 9 ATN

As the only CMU manufacturer involved in the actual development of the ATN software, Honeywell provides our customers with a unique capability of having engineering and technical support as this new technology is fielded in the years ahead. The Mark III CMU was specifically developed to support the addition of this new ATN software, without any hardware modifications to the unit. This will be a future upgrade option for the Mark III CMU.

Encryption/Authentication

Encryption and authentication are key issues surrounding secure data communications. Encryption involves the encoding of the broadcast bit stream using a secure encryption key. Authentication involves ensuring that only authorized users are accessing the application services. The Mark III CMU is designed to support

HONEYWELL Aerospace Electronic Systems

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Contents Honeywell Aerospace Electronic Systems Honeywell Aerospace Electronic Systems Introduction Mark III CMU OverviewDatalink Capability for Today and Tomorrow Honeywell Datalink Experience, Products, and Services Page Hardware Overview ArincSystem Interfaces Mark III CMU Interfaces DeviceArinc Interface Baseline Specificati GrowthSubnetwork Interfaces Arinc VDR SDU HfdrCMU Arinc 750 VHF Data Radio VDRFlight Deck Devices Interfaces UHFControl and Display Unit CDU Mcdu Midu CDULRU Interfaces Flight Management Computer FMCPerformance Computer PZ Aircraft Condition Monitoring System AcmsOther Interfaces Software Overview MIL-STD-1553BPcmcia OooiCMF VIACMU AOC HGI AMI Fidb Gbst Database DesignCertification Baseline Functionality AOA VDLM2Operations Uplink ProcessingDownlink Processing World RegionsSystem Pages DMT and DLTBite VDL Mode Growth FunctionalityAPM Data LoadingPcmcia Data Loading Arinc 761 SatcomMil-STD Weather GraphicsEncryption/Authentication ATNRRI Page Databases FidbGbst Fidb ArchitectureFidb HGI AMI Menus Main MenuMain Menu CDU Main Menu Supporting Regional / Business Jet CDUs ATS Menu System Menu Uplinks Clearance UplinkClearance Message Elements Clearance Message References Reject Reasons Reject Reasons Values Downlinks Diversion Report DownlinkDiversion Reasons Divert Message Elements Print Definition Logic UnitsPreferred Channel Management Oooi Logic UnitRegions US Map Areas Mechanical Design Interconnect CCAPower Supply CCA Processor CCAInput/Output CCA Spare CCAs Growth Detailed Interface DefinitionMcdu PrntrCMC ADLSDI PGM VHF PGM OooiVOICE/DATA MON SEL CMUMechanical Packaging Unit Weight Unit Connectors and MountsUnit Size Cooling RequirementsEnvironmental Specifications Power Input DO-160D Section Induced Signal Susceptibility DO-160D SectionWaterproofness DO-160D Section Fluids Susceptibility DO-160D SectionPower Requirements 1 115 Vac Input Power Requirements2 28 Vdc Input Power Requirements 3 28 Vdc Backup Input Power Requirements Power Interrupt RequirementsTechnical Summary