Guidance Law Design: Sliding Mode Control Approach
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 94 === In the previous time, most guidance law designs were chosen to be according to the line of sight rate, which is known as PNG law. The required missile maneuver command is calculated by means of the outer guidance loop alongside with the target information, w...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2006
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| Online Access: | http://ndltd.ncl.edu.tw/handle/85795984026601012063 |