Bo Lin
Abstract
A Bank-to-Turn autopilot of missile is designed based on adaptive sliding-mode control theory. In the design process, cross-coupled effect among three channels is taken into account. And robustness is guaranteed by setting an uncertain bound. Simulations results show that the method is valid.
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A Bank-to-Turn autopilot of missile is designed based on adaptive sliding-mode control theory. In the design process, cross-coupled effect among three channels is taken into account. And robustness is guaranteed by setting an uncertain bound. Simulations results show that the method is valid.
Key concepts: Missile, Autopilot, Control theory (sociology), Robustness (evolution), Variable structure control, Computer science, Adaptive control, Robust control