NONLINEAR CONTROL DESIGN FOR MISSILE TERMINAL GUIDANCE
碩士 === 國立交通大學 === 電機與控制工程系 === 88 === In this thesis, we study the interception problem of homing missiles. From the robust stabilization point of view, we propose two of robust control techniques and use them on the design of missile guidance law. When the missile pursuits the target, th...
| Main Authors: | , |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
2000
|
| Online Access: | http://ndltd.ncl.edu.tw/handle/66094603515549287920 |