DocumentCode :
3294019
Title :
Optimal control design using Sequential Linear Programming
Author :
Verlohren, C. ; Singh, T. ; Singla, P.
Author_Institution :
Dept. of Mech. & Aerosp. Eng., State Univ. of New York at Buffalo, Buffalo, NY, USA
fYear :
2010
fDate :
June 30 2010-July 2 2010
Firstpage :
1562
Lastpage :
1567
Abstract :
The focus of this paper is on the development of an iterative Linear Programming based approach for the determination of optimal controllers for nonlinear systems. The optimal control problem is posed in a Mayer form and a one-dimensional search technique such as the bisection algorithm is used on the cost function to converge to the optimal solution. A polynomial representation for the variation of the control profile is used to arrive at discrete time approximation of the perturbation dynamics about nominal trajectories. A linear program is then used to determine perturbations to the nominal control to satisfy terminal and transient constraints. The proposed technique is illustrated on some benchmark problems.
Keywords :
control system synthesis; discrete time systems; linear programming; nonlinear control systems; optimal control; Mayer form; bisection algorithm; discrete time approximation; iterative linear programming; nonlinear systems; one-dimensional search technique; optimal control design; perturbation dynamics; polynomial representation; sequential linear programming; transient constraints; Aerospace engineering; Control systems; Cost function; Friction; Iterative algorithms; Iterative methods; Linear programming; Nonlinear control systems; Nonlinear systems; Optimal control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2010
Conference_Location :
Baltimore, MD
ISSN :
0743-1619
Print_ISBN :
978-1-4244-7426-4
Type :
conf
DOI :
10.1109/ACC.2010.5531549
Filename :
5531549
Link To Document :
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