A Unified, Configurable, Non-Iterative Guidance System For Launch Vehicles
A satellite launch vehicle not subjected to any perturbations, external or internal, could be guided along a trajectory by following a stored, pre-computed steering program. In practice, perturbations do occur, and in order to take account of them and to achieve an accurate injection, a closed loop...
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| Language: | en_US |
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2011
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| Online Access: | http://hdl.handle.net/2005/1065 |