Title :
The Boeing 777 Fault Tolerant Air Data and Inertial Reference System-a new venture in working together
Author :
McIntyre, M.D.W. ; Gossett, Cynthia A.
Author_Institution :
Boeing Commercial Airplanes, Seattle, WA, USA
Abstract :
The Boeing Commercial Airplane Group has certified an all-new, integrated Fault Tolerant Air Data and Inertial Reference System (FT-ADIRS) on its 777 airliner. The FT-ADIRS consists of the Fault Tolerant Air Data and Inertial Reference Unit (FT-ADIRU), the Secondary Attitude and Air Data Reference Unit (SAARU), and six Air Data Modules (ADMs). New processes for the design, verification, and validation of the system were developed. The FT-ADIRS redundancy management and system performance were validated using a unique process whereby flight-recorded sensor data were replayed through actual production units. Faults were inserted in a Monte Carlo fashion to demonstrate the ability of the inertial navigation and air data functions to isolate and survive sensor faults in real-time
Keywords :
aircraft computers; aircraft control; aircraft navigation; fault tolerant computing; inertial navigation; modules; redundancy; reliability; system buses; Boeing 777; FT-ADIRS system; Monte Carlo simulation; accelerometer modules; air data inertial reference system; air data modules; commercial avionics; data-synchronous processor modules; design; display buses; fault tolerant system; flight control buses; inertial navigation; laser gyro modules; modular partitioning; redundancy management; secondary attitude and air data reference unit; sensor faults; system performance; validation; verification; Add-drop multiplexers; Airplanes; Fault tolerance; Fault tolerant systems; Monte Carlo methods; Process design; Production systems; Redundancy; Sensor systems; System performance;
Conference_Titel :
Digital Avionics Systems Conference, 1995., 14th DASC
Conference_Location :
Cambridge, MA
Print_ISBN :
0-7803-3050-1
DOI :
10.1109/DASC.1995.482827