DocumentCode
2064340
Title
A multirate predictive approach to orbit control of small spacecraft
Author
Rossi, Matteo ; Lovera, Marco
Author_Institution
Dipt. di Elettronica e Inf., Politecnico di Milano, Italy
Volume
3
fYear
2002
fDate
2002
Firstpage
1843
Abstract
The problem of orbit control for a small spacecraft is analysed and a solution based on predictive control is proposed. In particular, it is shown how a typical system requirement related to the actual implementation of the control action can be readily taken into account via a multirate formulation.
Keywords
MIMO systems; attitude control; dynamics; matrix algebra; predictive control; space vehicles; MIMO system; dynamics; matrix algebra; multirate control; orbit control; predictive control; small spacecraft; Aerospace industry; Control engineering; Control systems; Control theory; Error correction; Low earth orbit satellites; Predictive control; Propulsion; Space vehicles; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2002. Proceedings of the 2002
ISSN
0743-1619
Print_ISBN
0-7803-7298-0
Type
conf
DOI
10.1109/ACC.2002.1023835
Filename
1023835
Link To Document