Non-fragile guaranteed cost control for robust spacecraft orbit transfer with small thrust
This paper studies the robust orbit transfer problem for low earth orbit spacecraft rendezvous with parameter uncertainties and subject to input constraint and guaranteed cost control. The spacecraft rendezvous process can be divided into in-plane motion and out-of-plane motion because the Clohessy–...
| Main Authors: | , , |
|---|---|
| Format: | Journal Article |
| Published: |
Oxford University Press
2011
|
| Online Access: | http://hdl.handle.net/20.500.11937/46812 |