DocumentCode
2983162
Title
Flight control system design using CAEBEL, a CACSD system
Author
Blackwell, A.L. ; Bhatia, R.P. ; Wang, C.J. ; Blackwell, C.C. ; Wood, T.L.
Author_Institution
Dept. of Mech. Eng., Texas Univ., Arlington, TX, USA
fYear
1988
fDate
23-27 May 1988
Firstpage
421
Abstract
CAEBEL, an information management system for control system design, has been used in the design and development of automatic control systems for tiltrotor aircraft. CAEBEL was used in conjunction with a real-time simulation of a generic tiltrotor aircraft. The manner in which the functions needed to simulate the tiltrotor aircraft control system functions were accommodated within the structure of CAEBEL, is detailed
Keywords
aerospace computing; aerospace control; aerospace simulation; control system CAD; digital simulation; management information systems; CACSD; CAEBEL; automatic control systems; control system design; flight control system; information management system; real-time simulation; tiltrotor aircraft; Aerospace control; Aircraft manufacture; Automatic control; Computational modeling; Control system synthesis; Control systems; Helicopters; Information management; Software systems; Vehicle dynamics;
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.1988.195045
Filename
195045
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