Journal of Projectiles, Rockets, Missiles and Guidance >
Autopilot Topologies Research Based on Optimal Control
Received date: 2010-04-02
Online published: 2025-05-30
Autopilot design was researched based on optimal control. The connection between classical and optimal control for missile longitudinal autopilot was established. The focus of this paper is to examine three loop topologies and determine the best in terms of robustness. It's shown that there is transformation that can provide equivalent closed loop properties for different topologies, but the open loop properties will be different.
Key words： tactical missile; autopilot; optimal control; robustness
WANG Jianqi , YANG Yurong , HUA Jianlin , LI Younian . Autopilot Topologies Research Based on Optimal Control[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(1) : 63 -66 . DOI: 10.15892/j.cnki.djzdxb.2011.01.045
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