Blended Control System Design for Missile with Tail and Lateral Thrust
碩士 === 國立交通大學 === 電控工程研究所 === 103 === This thesis investigates the control about blended control for missile actuator with tail and lateral thrust. Tail controller changes angle of attack to generate lateral force by aerodynamic. To achieve requirements of steady-state and transient performance, tai...
| Main Authors: | , |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2014
|
| Online Access: | http://ndltd.ncl.edu.tw/handle/47385830808422806230 |