摘要
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.
出处
《弹箭与制导学报》
CSCD
北大核心
2005年第2期24-26,共3页
Journal of Projectiles,Rockets,Missiles and Guidance