Accession Number:

ADA009171

Title:

Fault-Tolerant Digital Airborne Data System Flight Test.

Descriptive Note:

Final rept. May 73-Aug 74,

Corporate Author:

HUGHES AIRCRAFT CO CULVER CITY CALIF

Personal Author(s):

Report Date:

1974-08-01

Pagination or Media Count:

54.0

Abstract:

A fault-tolerant data multiplexing and transmission system for fly-by-wire flight control application was successfully flight tested. The Fault-Tolerant Digital Airborne Data System F-DADS was adapted and installed as a link in the fly-by-wire flight control system of the USAFCALSPAN Total In-Flight Simulator TIFS aircraft. Sixteen analog signals, including pilot inputs, elevator, rudder, etc., autopilot feedback, attitude, rates, etc., were time multiplexed and transmitted via a serial digital data bus. F-DADS data terminals were redundant for failure protection. In addition to a conventional twisted pair wire data bus the multiplex link was operated with a fiber optic data bus and a microwave data bus which are immune to almost all types of electromagnetic interference.

Subject Categories:

  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE