BTT导弹自动驾驶仪多变量频域设计方法  

AUTOPILOT DESIGN USING THE INVERSE NYQUIST ARRAY METHOD FOR A BANK-TO-TURN MISSILE

作　　者：郑建华[1] 栾泽威[1] 崔平远[1] 杨涤[1] 

机构地区：[1]哈尔滨工业大学

出　　处：《宇航学报》1994年第3期24-29,共6页Journal of Astronautics

摘　　要：本文用多变量频域理论中的逆奈奎斯特阵列（ＩＮＡ）法设计某型ＢＴＴ导弹自动驾驶仪。首先建立ＢＴＴ导弹控制系统模型，并在某特征点设计驾驶仪的预补偿器、主控制器和反馈增益阵。而后在最严峻的激励作用下，对设计的驾驶仪进行非线性仿真。结果表明：导弹跟踪性能良好；补偿后俯仰—偏航通道间的耦合作用明显降低；设计方法物理概念清晰，易于工程实现。This paper presents an application of the inverse Nyquist Array(INA) technique to autopilot design of a highly maneuverable Bank-to-Turn(BTT) missile in which there is severe cross-coupling that is proportional to roll rate between the pitch and yaw axes.First,the pitch and yaw channels are analysed and the interactions are decreased with a constant precompensator matrix designed by the INA method.A maincontroller and a feedback gain matrix are then desighed for the approximately decoupled system to meet the desired dynamic performance and stable accuracy.Finally,the performance of the autopilot designed is evaluated in a non-linear simulation of autopilot with crucial excitation.The results demonstrate that,for the compensated system, the crosscoupling is boviously decreased.Excellent performance in terms of good command following properties and small side-slip is obtained.The pyhsical concept of design method is clear and the designed controllers are easy for physical implementation.

关 键 词：导弹 BTT导弹 自动驾驶仪 多变量频域 

分 类 号：TJ765.2[兵器科学与技术—武器系统与运用工程]