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一种改进的巡飞弹侧向运动解耦设计
引用本文:刘鹏云,孙瑞胜.一种改进的巡飞弹侧向运动解耦设计[J].飞行力学,2011,29(3):52-55.
作者姓名:刘鹏云  孙瑞胜
作者单位:南京理工大学动力工程学院;
摘    要:针对巡飞弹侧向平面内诸多不对称因素带来的航向通道和滚转通道强耦合这一特点,研究了巡飞弹侧向运动的耦合特性和解耦控制问题.由于传统的静态补偿器设计模型计算量大、适用性有限,为此提出了静态上三角形式补偿器的一般模型,该模型采用逆奈奎斯特阵列法,保留了巡飞弹侧向通道传递函数矩阵第二行的行优势性,然后具体针对格氏圆圆心密集区域...

关 键 词:巡飞弹  解耦控制  逆奈奎斯特阵列法  解耦控制器

Decoupling design of lateral movement for loitering attack missile
LIU Peng-yun,SUN Rui-sheng.Decoupling design of lateral movement for loitering attack missile[J].Flight Dynamics,2011,29(3):52-55.
Authors:LIU Peng-yun  SUN Rui-sheng
Institution:LIU Peng-yun,SUN Rui-sheng(Institute of Power Engineeing,Nanjing University of Science and Technology,Nanjing 210094,China)
Abstract:With the characteristics of the several coupling effects between the yaw and roll planes of the loitering attack missile,this paper studies the coupling of the loitering attack missile in the side plane and the feasibility of the decoupling coutrol.For the reason that the traditional decoupling controller model has a large calculation and a limited usability,a new model which is triangle form is presented.The new model takes use of the Inverse Nyquist array method to design the yaw and roll channel dynamic ...
Keywords:loitering attack missile  decoupling control  inverse Nyquist array method  decoupling controller  
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