A fault-tolerant air data/inertial reference system

A fault-tolerant air data inertial reference system (ADIRS) is described. The system consists of a fault-tolerant air data inertial reference unit, a secondary air data attitude reference unit, and six air data modules. The ADIRS replaces the conventional inertial reference and air data systems on a...

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Main Author: McClary, C.R.
Format: Conference Proceeding
Language:English
Subjects:
Add-drop multiplexers
Aerospace control
Aerospace electronics
Air navigation
Aircraft
Airplanes
Computer architecture
Condition monitoring
Costs
Fault tolerance
Fault tolerant systems
Hardware
Interfaces (computer)
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description A fault-tolerant air data inertial reference system (ADIRS) is described. The system consists of a fault-tolerant air data inertial reference unit, a secondary air data attitude reference unit, and six air data modules. The ADIRS replaces the conventional inertial reference and air data systems on aircraft and uses ARINC 629 bidirectional serial digital data bus interfaces. The ADIRS is designed to be the inertial and air data reference for the ARINC 651 integrated modular avionics distributed architecture and provides low life cycle cost and high availability through high reliability, simple high-integrity monitoring, and deferred maintenance.< >
doi_str_mv 10.1109/PLANS.1992.185817
format conference_proceeding
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ispartof IEEE PLANS 92 Position Location and Navigation Symposium Record, 1992, p.40-45
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source IEEE Electronic Library (IEL) Conference Proceedings
subjects Add-drop multiplexers
Aerospace control
Aerospace electronics
Air navigation
Aircraft
Airplanes
Computer architecture
Condition monitoring
Costs
Fault tolerance
Fault tolerant systems
Hardware
Interfaces (computer)
title A fault-tolerant air data/inertial reference system
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