An optimal control approach to spacecraft rendezvous on elliptical orbit
In this paper, we consider a linear quadratic regulator control problem for spacecraft rendezvous in an elliptical orbit. A new spacecraft rendezvous model is established. On the basis of this model, a linear quadratic regulator control problem is formulated. A parametric Lyapunov differential equat...
| Main Authors: | , , |
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| Format: | Journal Article |
| Published: |
John Wiley and Sons, Ltd.
2014
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| Subjects: | |
| Online Access: | http://hdl.handle.net/20.500.11937/39357 |