3D guidance law of BTT missile considering movement coupling

被引：0

作者：

Peng, Shuangchun ^{[1
]}

Sun, Weimeng ^{[2
]}

Wang, Nan ^{[1
]}

Pan, Liang ^{[1
]}

Shen, Lincheng ^{[1
]}

机构：

[1] College of Mechatronics and Automation, National University of Defense Technology, Changsha 410073, China

[2] No.92854 Unit, People's Liberation Army, Zhanjiang 524009, China

来源：

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2010年 / 31卷 / 05期

关键词：

Kinematics;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

A new 3-dimensional (3D) guidance law is proposed to deal with the coupling of bank-to-turn (BTT) missile. First, through vector description the kinematic model is divided into the three terms of pitching, swerve and coupling. Pitching and swerve are described in the Cartesian space, while coupling is described in the SO(3) space. Then, corresponding to no ending constraints and ending constraints, guidance laws are designed using respectively the proportional control and the generalized proportional-derivative (PD) control, which can avoid both the complexity of the Lie-group method and the information loss of the traditional decoupling method. Simulation results show that the proposed guidance law can satisfy the guidance precision requirements of BTT missiles.

引用

页码：968 / 974

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