Autopilot Design of a BTT Missile with a Front Lateral Jet to Enhance the Output Transient Responses
碩士 === 國立臺灣大學 === 電機工程學研究所 === 91 === In this thesis, a bank-to-turn autopilot design method is studied for a tail-controlled missile with a front lateral jet. The six degrees-of-freedom dynamical model of a short-range missile is described first. Then the linearization technique and lin...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2003
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| Online Access: | http://ndltd.ncl.edu.tw/handle/26595024847914685397 |