DocumentCode :
3019195
Title :
System identification technology for estimating reentry vehicle aerodynamic coefficients
Author :
Gupta, N.K. ; Hall, W.E.
Author_Institution :
Systems Control, Inc., Palo Alto, California
fYear :
1977
fDate :
7-9 Dec. 1977
Firstpage :
686
Lastpage :
693
Abstract :
This paper describes the development and application of a system identification technology to obtain accurate estimates of maneuvering reentry vehicle aerodynamic coefficients from flight data. The impact of the specific maneuvering reentry vehicle characteristics on system identification is described and appropriate solutions are proposed. Examples illustrate the effectiveness of the technology.
Keywords :
Aerodynamics; Control systems; Digital simulation; Missiles; Navigation; System identification; Testing; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control including the 16th Symposium on Adaptive Processes and A Special Symposium on Fuzzy Set Theory and Applications, 1977 IEEE Conference on
Conference_Location :
New Orleans, LA, USA
Type :
conf
DOI :
10.1109/CDC.1977.271658
Filename :
4045928
Link To Document :
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