Fuel Minimizing Control for Constrained Relative Satellite Orbits
In this paper, we study the fuel minimization problem of hovering satellite subject to a practical constraint on the trajectory of the deputy satellite. It is first shown that the constraint condition can be expressed equivalently as maximum flight time inequalities. On this basis, a cost function r...
| Main Authors: | , , , |
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| Format: | Journal Article |
| Published: |
WATAM Press
2011
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| Online Access: | http://hdl.handle.net/20.500.11937/48019 |