无人系统（英文）2025，Vol.13Issue(2)：591-608,18.DOI:10.1142/S2301385025500359
Optimal Control Approach to Design a Three-Loop Autopilot for a Tactical Missile
Optimal Control Approach to Design a Three-Loop Autopilot for a Tactical Missile
A.M.Abu El-Wafa 1Mohammed A.H.Abozied 1Yehia Z.Elhalwagy 1Hossam M.Hendy1
作者信息
- 1. Guidance Department,Military Technical College,Kobry Elkobba,Cairo 11766,Egypt
- 折叠
摘要
关键词
LQR/lagrange multipliers/Riccati equation/performance-indexKey words
LQR/lagrange multipliers/Riccati equation/performance-index引用本文复制引用
A.M.Abu El-Wafa,Mohammed A.H.Abozied,Yehia Z.Elhalwagy,Hossam M.Hendy..Optimal Control Approach to Design a Three-Loop Autopilot for a Tactical Missile[J].无人系统（英文）,2025,13(2):591-608,18.
