BALLISTIC AND AIRDYNAMICS

Research on the Design of Nonlinear Dynamic Inversion Control in Trajectory Correction

  • ZENG Yaohua ,
  • WANG Hua ,
  • HAN Jing ,
  • WANG Yining
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  • 1 School of Mechatronics Engineering, North University of China, Taiyuan 030051, China
    2 School of Astronautics, BUAA, Beijing 100083, China

Received date: 2009-07-14

  Online published: 2025-05-28

Abstract

Based on nonlinear inverse system theory, the three time-scale separation method was put forward for decoupling and linearizing the strong coupling and nonlinear trajectory correction equations. On the basis of the system states dynamic characteristics, the system was separated into three subsystems. Then, the inverse system controllers were designed for these subsystems separately, and the linear controllers were also done for the linearized systems by the Lyapunov function method. Finally, with the Matlab simulation, it was verified the efficiency of the inverse system method, and compared the system's dynamic performance by selecting different loop bandwidths. The results indicate that the method is correct and effective.

Cite this article

ZENG Yaohua , WANG Hua , HAN Jing , WANG Yining . Research on the Design of Nonlinear Dynamic Inversion Control in Trajectory Correction[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(3) : 131 -134 . DOI: 10.15892/j.cnki.djzdxb.2010.03.037

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