DocumentCode :
1853579
Title :
Parameter estimation in a failure detection system of a fighter aircraft
Author :
McCartney, David M. ; Skormin, Victor A.
Author_Institution :
Watson Sch. of Eng., Binghamton Univ., NY, USA
fYear :
1993
fDate :
24-28 May 1993
Firstpage :
462
Abstract :
This paper presents a failure detection and isolation (FDI) technique suitable for implementation in a self-repairing flight control system (SRFCS). The FDI employs simplex optimization procedure for on-line estimation of the system parameters affected by battle damage, thus providing the basis for the implementation of a variable-structure controller to augment surface commands due to surface impairments. In addition, the suggested FDI provides failure information to a positive pilot alert (PPA) system. The approach was verified by computer simulations which showed that characteristics of an impaired system can be dramatically improved by FDI and SRFCS
Keywords :
aerospace computing; aircraft control; built-in self test; digital simulation; fault location; military computing; military equipment; optimisation; parameter estimation; variable structure systems; battle damage; computer simulations; failure detection; failure isolation; fighter aircraft; online estimation; parameter estimation; positive pilot alert; self-repairing flight control; simplex optimization; surface commands; surface impairments; variable-structure controller; Actuators; Aerodynamics; Aerospace control; Aerospace electronics; Aircraft propulsion; Control systems; FCC; Fault detection; Military aircraft; Parameter estimation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace and Electronics Conference, 1993. NAECON 1993., Proceedings of the IEEE 1993 National
Conference_Location :
Dayton, OH
Print_ISBN :
0-7803-1295-3
Type :
conf
DOI :
10.1109/NAECON.1993.290957
Filename :
290957
Link To Document :
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