Robust Missile Guidance Law Design with Time Delay in Acceleration
碩士 === 國立交通大學 === 電控工程研究所 === 100 === This paper studies the design of missile guidance law using the combination of SMC and ISMC technologies. The presented guidance law is shown to be able to compensate for the presence of uncertainty, including target estimation error, and time lag in acceleratio...
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| Format: | Others |
| Language: | zh-TW |
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2012
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| Online Access: | http://ndltd.ncl.edu.tw/handle/17923697511485497596 |