DocumentCode
488146
Title
Trajectory Optimization for Real-Time Guidance: Part 1, Time-Varying LQR on a Parallel Processor
Author
Psiaki, Mark L. ; Park, Kihong
Author_Institution
Assistant Professor, Mechanical and Aerospace Engineering, Cornell University, Ithaca, New York 14853-7501
fYear
1990
fDate
23-25 May 1990
Firstpage
248
Lastpage
253
Abstract
A key algorithmic element of a real-time trajectory optimization hardware/software implementation is presented, the QP solver element. The purpose of the effort is to make nonlinear trajectory optimization fast enough to provide real-time commands during guidance of a vehicle such as an aero-maneuvering orbiter. Many methods of nonlinear programming require the solution of a quadratic program (QP) at each iteration. In the trajectory optimization case the QP has a special Dynamic Programming structure, a LQR-like structure. QP algorithm speed is increased by taking advantage of this special structure and by parallel implementation.
Keywords
Aerospace engineering; Costs; Dynamic programming; Hardware; Jacobian matrices; Navigation; Quadratic programming; Software algorithms; Time varying systems; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1990
Conference_Location
San Diego, CA, USA
Type
conf
Filename
4790736
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