Variable Structure Theory Based Integrated Guidance/Autopilot Design for Highly Maneuverable Flying Vehicles
博士 === 國立臺灣大學 === 電機工程學研究所 === 91 === In this thesis, we propose a variable structure based nonlinear integrated guidance/autopilot system design for flying vehicles using optimal control theory with highly maneuverable actuators, which are mainly consisting of pulse type actuators, thrust vector co...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
2003
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| Online Access: | http://ndltd.ncl.edu.tw/handle/65816180566242921715 |