Paper Title:
Optimal Guidance Law Design for Interception of Ballistic Missiles during the Boost Phase
  Abstract

An optimal guidance law for interception of ballistic missile during the boost phase is presented in this paper. The kinematics characteristics of tactical missile during its boost phase are analyzed firstly. Then based on the kinematics given and assumption, the relative kinematics equations between target and missile are established. Optimal guidance law via LQ optimization is derived under the specified cost function. The time-to-go estimation method is also given in the paper. In the end of this paper, simulation is executed and the results validate that the deduced guidance law satisfy the direct hit index.

  Info
Periodical
Chapter
Chapter 6: Energy & Electronic
Edited by
Robin G. Qiu and Yongfeng Ju
Pages
655-659
DOI
10.4028/www.scientific.net/AMM.135-136.655
Citation
W. W. Zhou, X. G. Liang, "Optimal Guidance Law Design for Interception of Ballistic Missiles during the Boost Phase", Applied Mechanics and Materials, Vols. 135-136, pp. 655-659, 2012
Online since
October 2011
Export
Price
$32.00
Share

In order to see related information, you need to Login.

In order to see related information, you need to Login.

Authors: Yan Kai Cui, Li Fu, Xiao Geng Liang, Ling Luo
Abstract:Aiming at terminal guidance law design of airborne boost-phase ballistic missile interception under acceleration of target without...
15
Authors: Cong Ying Li, Jin Yong Yu, Lei Han, Wen Guang Zhang
Abstract:Integrated guidance, control and maneuver for anti-vessel missiles against vessel targets was studied. Firstly, the integrated guidance and...
126
Authors: He Huang, Zhi Fu Zhu
Chapter 3: Mechanical, Electronic and Material Engineering
Abstract:Guidance law The optimal direct-impact guidance law for space-based anti-missile of ballistic missile in boost phase is considered. First the...
1749
Authors: Zhi Ping Li, Jun Zhou, Jian Guo Guo
Chapter 1: Research and Engineering in the Field of Control and Intelligent Systems
Abstract:A new nonlinear robust guidance law was proposed by considering autopilot dynamics. Firstly, the mathematic model was built according to...
77
Authors: Xiao Ju Duan, Xiao Zhong Xue, Peng Yun Liu
Chapter 3: Mechatronics, Robotics and Control
Abstract:A new approach is designed to the guidance of rocket-propelled missile with multiple object constraints. It allows the rocket-propelled...
256