DocumentCode
3047523
Title
Number crunching on the ACOSS model no. 2
Author
Gran, Ruben ; Rossi, Mattia
Author_Institution
Grumman Aerospace Corporation, Bethpage, NY
fYear
1982
fDate
8-10 Dec. 1982
Firstpage
909
Lastpage
911
Abstract
The spacecraft model called ACOSS Model Number II was used to develop a control system design for large space structures that has certain desirable characteristics. To achieve these characteristics the control design approach we use is based on an optimal reduced order control design technique that explicitly computes the minimum of an expected quadratic cost function using a numerical search algorithm. The algorithm, developed by Rossi [1], uses an explicit calculation of the gradient and Hessian tensors to guide a second order search. The algorithm and the "number crunching" on the ACOSS model are both described.
Keywords
Kalman filters; Optimal control; State feedback; Tellurium; Time of arrival estimation;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1982 21st IEEE Conference on
Conference_Location
Orlando, FL, USA
Type
conf
DOI
10.1109/CDC.1982.268276
Filename
4047379
Link To Document