DocumentCode :
1137109
Title :
An Approach to Optimization of Terminal Rendezvous
Author :
Koivo, A.J. ; Repperger, D.W.
Author_Institution :
Purdue University Lafayette, Ind. 47907
Issue :
2
fYear :
1972
fDate :
3/1/1972 12:00:00 AM
Firstpage :
218
Lastpage :
228
Abstract :
The optimal solution is presented to a cooperative game which is described by a common quadratic cost functional subject to linear ordinary differential equation constraints. The optimal feedback controller is constructed for both players when all components of the state vector can be measured. For the case that only some components of the state vector are available, the optimal feedback controller is designed using a dynamic observer. As a specific application, the approach is used in determining the optimal feedback controllers for two satellites which are performing a rendezvous on a circular orbit. Simulation results are presented to illustrate the applicability of the approach.
Keywords :
Adaptive control; Angular velocity; Cost function; Earth; Equations; Extraterrestrial measurements; Mathematical model; Satellites; Vectors; Vehicles;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.1972.309493
Filename :
4102932
Link To Document :
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