To intercept high-speed, highly maneuverable targets at mid-to-high altitudes, this paper explores disturbance-rejection guidance laws for missiles with canard/tail rudder control. By integrating the canard/tail rudder composite control method with disturbance-rejection guidance laws, we significantly enhance the maneuverability, manipulation ability, and guidance precision of missiles. The optimal control algorithm refines the canard/tail rudder distribution strategy, while real-time disturbance-rejection compensates for unknown disturbances. Simulations show that this approach improves target interception performance and hit probability.
On Disturbance-Rejection Guidance Laws for Missiles with Canard/Tail Rudder Control
Lect. Notes Electrical Eng.
International Conference on Guidance, Navigation and Control ; 2024 ; Changsha, China August 09, 2024 - August 11, 2024
2025-03-02
11 pages
Article/Chapter (Book)
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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