A Guidance Law Design Using the Combination of SDRE and ISMC Control Schemes
碩士 === 國立交通大學 === 電控工程研究所 === 101 === This thesis explores the design of robust guidance law for missile interception task, in which the target maneuver is treated as disturbances. In this thesis, we combine the state dependent Riccati equation (SDRE) and integral-type sliding mode control (ISMC) sc...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
2013
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| Online Access: | http://ndltd.ncl.edu.tw/handle/g74jc9 |