DocumentCode
488145
Title
Finite Element Solution of Optimal Control Problems with Inequality Constraints
Author
Bless, Robert R. ; Hodges, Dewey H.
Author_Institution
Graduate Research Assistant, School of Aerospace Engineering. Student Member, AIAA; Georgia Institute of Technology, Atlanta, Georgia
fYear
1990
fDate
23-25 May 1990
Firstpage
242
Lastpage
247
Abstract
A temporal finite element method based on a weak Hamiltonian form of the necessary conditions is summarized for optimal control problems. Very crude shape functions (so simple that element numerical quadrature is not necessary) can be used to develop an efficient procedure for obtaining candidate solutions (i.e., those which satisfy all the necessary conditions) even for highly nonlinear problems. An extension of the formulation allowing for discontinuities in the states and derivatives of the states is given. Furthermore, the theory to include control inequality constraints is fully developed. Finally, an Advanced Launch Vehicle (ALV) model is presented. The model involves staging and control constraints, thus demonstrating the full power of the weak formulation to date. Numerical results are presented along with total elapsed computer time required to obtain the results. The speed and accuracy in obtaining the results make this method a strong candidate for a real-time guidance algorithm.
Keywords
Aerospace engineering; Constraint theory; Equations; Finite element methods; Intelligent vehicles; Lagrangian functions; Navigation; Optimal control; Performance analysis; Shape;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1990
Conference_Location
San Diego, CA, USA
Type
conf
Filename
4790735
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