Honeywell Understanding Database Systems for Enhanced Network Router Functionality

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4 DATABASES

Honeywell pioneered the concept of airline reconfiguration and partitioned software for datalink systems in the early 1990s. The reconfiguration concept has continually evolved and improved as each new product has been introduced. Reconfiguration started in the industry with the Honeywell Mark II ACARS unit, and expanded with the B-777 and Mark II CMU. This design concept has continued to be improved resulting in the Mark III CMU being the most flexible and powerful system available today providing unparalleled flexibility in defining the AOC application. In addition, the reconfiguration concept has been expanded to allow support for ATC (Certification related processing). This allows the system to easily be expanded for current and future ATC processing. The architecture for supporting such reconfiguration is centered around the Database design contained with the Mark III CMU. Changes to these databases do not require embedded operational software changes, making changes much simpler and faster (and not prone to software coding errors). Further, like our Mark II CMU, the approach supports the ability of airlines making changes to the AOC database, using a PC-based tool, without impacting the certification of the unit.

There are three primary databases contained with the Mark III CMU. The AMI database defines the airlines AOC functions. This is the database that either Honeywell or the Airline can create, and update at any time, using a PC based tool (GBST). The second database is the HGI database. The HGI is a database similar to the AMI, but contains information that is considered by certification authorities as requiring certification control. As an example, ATC messages and the corresponding MCDU screens are defined in the HGI database. The HGI database is only modifiable by Honeywell, and does require changes to be under certification control. The third database is the FIDB database. This database defines the mapping between external (input) parameters received from other subsystems on the aircraft and the corresponding parameters used within the CMU as well as in the GBST reconfiguration tool. The FIDB database approach provides a significant improvement over other previous reconfiguration systems, by allowing the CMU to have a single database for all aircraft types, with the FIDB defining aircraft differences. With this approach, single database part numbers can be used across an airlines complete fleet of aircraft, rather than separate database part numbers for each fleet type. Further information on these databases and reconfiguration are provided in the following sections.

4.1 FIDB

The Flexible Input Data Base (FIDB) is a cornerstone of the Mark III CMU database design. Aircraft parameter data for each aircraft type is captured in mini-FIDBs. All of the mini-FIDBs are collected into a single master FIDB that contains aircraft data for all aircraft types. For a given customer, data for that customer's aircraft types are put into the Customer FIDB. (See Figure 10).

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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 ArincArinc System InterfacesMark III CMU Interfaces Device Interface Baseline Specificati GrowthCMU Subnetwork InterfacesArinc VDR SDU Hfdr Arinc 750 VHF Data Radio VDRFlight Deck Devices Interfaces UHFControl and Display Unit CDU Mcdu Midu CDUPerformance Computer PZ LRU InterfacesFlight Management Computer FMC Aircraft Condition Monitoring System AcmsOther Interfaces Pcmcia Software OverviewMIL-STD-1553B OooiCMF VIACMU AOC HGI AMI Fidb Gbst Database DesignCertification Baseline Functionality AOA VDLM2Operations Uplink ProcessingDownlink Processing World RegionsBite System PagesDMT and DLT APM VDL ModeGrowth Functionality Data LoadingMil-STD Pcmcia Data LoadingArinc 761 Satcom Weather GraphicsRRI Encryption/AuthenticationATN 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 CCAInput/Output CCA Power Supply CCAProcessor CCA Spare CCAs Growth Detailed Interface DefinitionCMC McduPrntr ADLVOICE/DATA MON SDI PGM VHF PGMOooi SEL CMUUnit Size Mechanical Packaging Unit WeightUnit Connectors and Mounts Cooling RequirementsEnvironmental Specifications Waterproofness DO-160D Section Power Input DO-160D SectionInduced Signal Susceptibility DO-160D Section Fluids Susceptibility DO-160D Section2 28 Vdc Input Power Requirements Power Requirements1 115 Vac Input Power Requirements 3 28 Vdc Backup Input Power Requirements Power Interrupt RequirementsTechnical Summary