DocumentCode
792096
Title
Optimal nonlinear feedback control derived from quartic and higher-order performance criteria
Author
Bass, R.W. ; Webber, R.F.
Author_Institution
Hughes Aircraft Company, Los Angeles, CA, USA
Volume
11
Issue
3
fYear
1966
fDate
7/1/1966 12:00:00 AM
Firstpage
448
Lastpage
454
Abstract
Just as minimization of quadratic performance criteria leads to linear feedback, so it is shown here that minimization of integrals containing quartic or hexadic terms in the state variables leads, respectively, to cubic or quintic feedback. This idea is extended to the minimization of integrals of arbitrarily higher order combinations of the state variables, which is desirable in order to impose inequality constraints upon the state variables. Such laws are shown to be adaptive to actuator saturation (including even bang-bang operation). These results are proved by exhibiting a closed-form solution of the corresponding Hamilton-Jacobi equation, which also provides a globally valid Liapunov function. Prior results of Kalman, Haussler, and Rekasius for linear plants appear as special cases. A new constructive procedure for computing the coefficients of the higher-order feedback terms is also presented, together with a numerical application which illustrates remarkable effectiveness in the reduction of overshoots as compared to optimal linear control.
Keywords
Nonlinear systems; Optimal control; Actuators; Contracts; Equations; Feedback control; Helium; Jacobian matrices; Linear feedback control systems; Optimal control; Performance analysis; State feedback;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/TAC.1966.1098381
Filename
1098381
Link To Document