A Comparsion of New and Existing Proportional Navigation Guidance Laws
碩士 === 淡江大學 === 航空太空工程學系 === 87 === The purpose of this thesis is to investigate the influence on performance of the proportional navigation missile guidance law. In the terminal guidance system, proportional navigation guidance law has been implemented for years. Various guidance laws we...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1998
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| Online Access: | http://ndltd.ncl.edu.tw/handle/73429029606514950280 |