An optimal control approach to robust control of nonlinear spacecraft rendezvous system with θ-D technique
In this paper, a new optimal robust control design approach is proposed for the task of spacecraft rendezvous such that both the stabilization and optimal performance are achieved. An approximate closed-form solution to the nonlinear optimal control problem is obtained by employing the θ-D technique...
| Main Authors: | , , |
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| Format: | Journal Article |
| Published: |
ICIC International
2013
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| Subjects: | |
| Online Access: | http://hdl.handle.net/20.500.11937/12266 |