DocumentCode
490322
Title
Nonlinear Control of High Performance Aircraft
Author
Mohler, R.R.
Author_Institution
Oregon State University, Department of Electrical and Computer Engineering, Corvallis, OR 97331
fYear
1993
fDate
2-4 June 1993
Firstpage
1395
Lastpage
1399
Abstract
Nonlinear adaptive control and time-optimal control of highly maneuverable, nonlinear, longitudinal aircraft dynamics are studied here. Minimum-time control by means of horizontal stabilators is desired as a performance yardstick and as a basis for sub-time-optimal neural-net-generated feedback control. Another feedback control utilizes a nonlinear time-series model reference for extremely large rapid changes in angle of attack. Simulation results are presented for the F18/HARV (high angle-of-attack research vehicle).
Keywords
Adaptive control; Aerodynamics; Aerospace control; Aircraft; Computer simulation; Nonlinear dynamical systems; Processor scheduling; Robust control; Size control; Vehicle dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1993
Conference_Location
San Francisco, CA, USA
Print_ISBN
0-7803-0860-3
Type
conf
Filename
4793100
Link To Document