Control reconfigurable combat aircraft piloted simulation development

Author

Mercadante, Richard ; Wheeler, Philip N. ; Mix, Marilyn ; Farley, John ; Chandler, Phillip R.

Author_Institution

Grumman Aircraft Syst., Bethpage, NY, USA

fYear

1988

fDate

23-27 May 1988

Firstpage

512

Abstract

The AFWAL/FIG control reconfigurable combat aircraft (CRCA) effort, part of the Self-Repairing Flight Control System (SRFCS) Program, exploits reconfiguration to maintain mission capability. Specifically, reconfigurable control laws, fault detection and isolation (FDI) logic, and a positive pilot alert (PPA) system have been developed for an advanced-tactical-fighter-class aircraft simulation. The authors describe the six degree-of-freedom CRCA piloted simulation conducted at the USAF Large Amplitude Multimode Aerospace Research Simulator (LAMARS) facility. The aircraft simulation, damage/failure aerodynamic math modeling, flight control computer (FCC) software, pilot/vehicle interface, and simulation environment are discussed

Keywords

aerospace computer control; aerospace simulation; aircraft; fault location; Self-Repairing Flight Control System; advanced-tactical-fighter-class aircraft; aerospace simulation; aircraft simulation; damage/failure aerodynamic math modeling; fault detection and isolation; flight control computer; pilot/vehicle interface; positive pilot alert; reconfigurable combat aircraft piloted simulation; reconfigurable control laws; self repairing flight control; simulation environment; six degree-of-freedom; software; Aerodynamics; Aerospace control; Aerospace simulation; Aircraft; Computational modeling; Computer interfaces; Computer simulation; Control systems; Fault detection; Reconfigurable logic;

fLanguage

English

Publisher

ieee

Conference_Titel

Aerospace and Electronics Conference, 1988. NAECON 1988., Proceedings of the IEEE 1988 National

Conference_Location

Dayton, OH

Type

conf

DOI

10.1109/NAECON.1988.195056

Filename

195056