This paper describes an experimental study on an integrated servo control method. Conventional servo control schemes may experience performance degradation under the presence of physical constraints. An integrated scheme is proposed in this study to address this problem. In the proposed method, three controllers correspond to autopilot commands directly instead of four actuators. Various simulations and experiments show that the proposed integrated servo control method provides better performance than the conventional ones.
Experimental study on integrated servo control for canard-controlled missiles [Correspondence]
IEEE Transactions on Aerospace and Electronic Systems ; 52 , 3 ; 1467-1474
2016-06-01
1626439 byte
Article (Journal)
Electronic Resource
English
AIAA-2006-6569 Optimal Control Solution for Dual (Tail and Canard) Controlled Missiles
British Library Conference Proceedings | 2006
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