AvionicsZone - Avionics Solutions from Honeywell
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Vehicle Management
A400M Product List

Auto Flight Air Data IMA


Auto Flight
     Flight Control Systems
  • Provides Flight Director Commands to Instruments
       - Yaw Damping, Turn Coordination
       -Autopilot, Automatic Pitch Trim
       -Processes Servo and Trim Actuator Command Signals
  • Dual 1750 Processors for Fail Passive / Fail Safe Operation
  • Systems available for Single or Dual Installation
  • “Smart” Servos include integrated power amplifiers
  • Honeywell provides the USAF Standard Autopliot
       -C-130 ARP
       -C-130J
       -C-141
  • International Customers include:
       -Belgian, Spain, Indonesia, Australia, New Zealand Botswana






     Flight Control Systems
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F-16 Digital Flight Control System
  • System Features
       - First production fly-by-wire digital FCS
       - First flight critical use of MIL-STD-1750A
       - Single, quad redundant, LRU!



F-2 Digital Flight Control Computer

  • System Features
       -Providing 3 identical Digital Central Processing and Input/Output Processor (CPU/IOP) SRUs per aircraft for core flight control function in triplex FLCC


C-141/C-130 Automatic Flight Control Subsystem (AFCS)





F-2 Flight Control Engineering Test Station
  • Provides a complete Triplex Simulated Vehicle Environment with Individual Computer Control for all Inputs and Outputs
  • Presents a High-fidelity Electronic & Mechanical Equivalent of the Aircraft to the F-2 FLCC
  • Stand-Alone Automated Testing and Connection to the Vehicle’s “Iron-bird” for Complete Integrated Closed-loop Testing




USAF E-8C JSTARS Program
  • Contract received in Feb 1999 for modification of E-6A DAU design
  • 25 DAUs, 18 CPs
  • Prime is Northrop Grumman
  • YAW Damper Monitor Contract Pending
  • FAA Certification In-Process




E-8C Digital Auto-Pilot Unit

     Flight Control Systems Experience
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Flight Control Systems Experience Chart

Air Data

     Honeywell Air Data Solutions

  • Honeywell Micro Air Data Computer Product Family
  • Air Data Multi-Function Probe (ADMFP)


     Honeywell HG1131 Micro Air Data Computer
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  • Physical Characteristics Size: 7.6" x 4.5" x 3" Weight: 2.1 pounds Power: 6 watts, 28 Vdc MTBF: 80,000 hrs. “AUC” 49,900 hrs. “AUF” BIT: 95% Coverage Convection Cooled Qualification: Full MIL-STD-810 and MIL-STD-461 EMI/EMC
  • Fully Qualified, off-the-shelf
  • In volume production for the U.S. Air Force


     Centralized Air Data System vs. Distributed Air Data System
    Centralized Air Data System
  • Shipset weight: ~ 35 lbs
  • Shipset cost: ~ $85K
    Distributed Air Data System
  • Shipset weight: ~ 15 lbs
  • Shipset cost: ~ $45K
    Eliminates:
  • Pilot/static nose probe
  • Side mount pitot/static probe
  • CADC
  • Flight control PSA
  • Differential pressure sensor (2 qty)
  • ~28 ft. of pneumatic lines
     Multifunction Probe / ADMFP
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IMA

     Common VIA Development Team Development Plan

     CVDT FMS Product Line Architectural Model
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     USAF C-5 AMP Program
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  • Customer: Lockheed Martin
  • End user: USAF
  • Time Frame: Contract awarded January 1999
  • System Capabilities:
  • Integrated Computing Platform (VIA)
  • Commercial COTS Computers
  • ARINC 653 Operating System
  • ARINC 659 Backplane
  • Flight Management Function
  • ARINC 739 Control Display Units
  • ARINC 758 Communication Management Function
  • Flight Director/Autopilot/SCAS/Load Alleviation Function
  • Seven 6x8 Displays
  • AFMSS Compatible Navigation Database
  • Integrated w/ suite of new Navigation Sensors
  • Integrated w/ suite of new Comm and Nav Radios
     USAF C-5 AMP Program


     USAF KC-10 Program
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  • Customer: Boeing
  • End user: USAF
  • Time Frame: Contract awarded November 1999
  • System Capabilities
  • Integrated Computing Platform (VIA)
  • ARINC 758 Communication Management Function
  • Commercial COTS Computers
  • ARINC 653 Operating System
  • ARINC 659 Backplane
  • Flight Management Function
  • ARINC 739 Control Display Units
  • AFMSS Compatible Navigation Database
  • Integrated w/ new MMR and existing INS
  • Integrated w/ Nav Radios
  • Four 6.7 x 6.7 “D” Displays
    •      Summary

    • Honeywell possesses a unique blend of products and system integration experience that can be utilized to develop a cost effective, mission capable avionics solution
    • Honeywell is eager to work with Airbus Military Company on developing an avionics solution that will make the A400M aircraft European Staff Requirement compliant