Guidance and Attitude Control of Missile Interceptor
碩士 === 國立交通大學 === 電機與控制工程系所 === 96 === The thesis investigates three-dimensional midcourse and terminal guidance laws for missile interceptor and the associated divert and attitude control system design. Since the commanded guidance acceleration, in both the midcourse phase and terminal phase, is ac...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2008
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| Online Access: | http://ndltd.ncl.edu.tw/handle/49151549804706335393 |