標題: 可變結構系統理論在飛彈導引律設計上之應用
Variable Structure System Theory Applied to the Design of Guidance Laws for Missile
作者: 陳永平
CHEN YON-PING
交通大學電機與控制工程系
關鍵字: 可變結構系統理論;飛彈;導引律;軌跡;Variable structure system theory;Missile;Guidance law;Trajectory
公開日期: 2002
官方說明文件#: NSC91-CS-7009-004
URI: http://hdl.handle.net/11536/92622
https://www.grb.gov.tw/search/planDetail?id=696768&docId=132064
Appears in Collections:Research Plans