BTT导弹自动驾驶仪自适应变结构设计

Design of BTT Missile Autopolot Using Variable Structure Adaptive Control Theory

文中应用自适应变结构控制理论,设计了倾斜转弯导弹的自动驾驶仪。在设计过程中保留通道间的耦合因素,并通过给定被控对象参数摄动和外部扰动的范围,保证了很好的鲁棒性和稳定性。仿真结果表明这种设计方法的有效性。

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.