DocumentCode :
825456
Title :
Multiple control input design for identification of light aircraft
Author :
Wells, William R. ; Ramachandran, S.
Author_Institution :
Wright State University, Dayton, OH, USA
Volume :
22
Issue :
6
fYear :
1977
fDate :
12/1/1977 12:00:00 AM
Firstpage :
985
Lastpage :
987
Abstract :
This paper establishes a design technique for control input histories resulting in higher confidence levels in the estimate of lateral stability and control derivatives of light aircraft, and which cause dynamic motion favorable to reductions in numerical divergence tendencies in the identification algorithms. A combined aileron and rudder input design is demonstrated for the Cessna 172 aircraft.
Keywords :
Aircraft control; Linear systems, stochastic continuous-time; Parameter identification; Aerospace control; Aircraft; Algorithm design and analysis; Automatic control; History; Lighting control; Motion control; Stability; Switches; Vectors;
fLanguage :
English
Journal_Title :
Automatic Control, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9286
Type :
jour
DOI :
10.1109/TAC.1977.1101653
Filename :
1101653
Link To Document :
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