Optimal guidance and control in space technology
In this thesis, we deal with several optimal guidance and control problems of the spacecrafts arising from the study of lunar exploration. The research is composed of three parts: 1. Optimal guidance for the lunar module soft landing, 2. Spacecraft attitude control system design basing on double gim...
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| Format: | Thesis |
| Language: | English |
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Curtin University
2011
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| Online Access: | http://hdl.handle.net/20.500.11937/1503 |