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Journal of Projectiles, Rockets, Missiles and Guidance >

2021 , Vol. 41 >Issue 1: 40 - 43

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2021.01.009

Modeling and Control Strategy Design of Vertically Launching Missiles Based on Quaternion

  • WANG Qishuang ,
  • LIU Junsheng ,
  • TAN Tianhan ,
  • LI Yongsheng ,
  • CHANG Guannan
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  • Xi’an Modern Control Technology Research Institute,Xi’an 710065,China

Received date: 2019-12-08

  Online published: 2025-02-11

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Abstract

Singular points exist when using the traditional Euler Angles to describe vertical-launching missile’s movement. This article, therefore, builds a quaternion-based mathematics model to analyze the spatial movement of vertical-launching missiles, realizing the design of pitching, yawing, and rolling function of the triple-channel controller. It also discusses various turn strategies and verifies the validity of the mathematic model and the design of tripper-channel controller with the rolling-after-turning strategy in ballistic trajectory simulation.

Key words： vertically launching; quaternion; attitude control; turn strategy; modeling and simulation

Cite this article

WANG Qishuang , LIU Junsheng , TAN Tianhan , LI Yongsheng , CHANG Guannan . Modeling and Control Strategy Design of Vertically Launching Missiles Based on Quaternion[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2021 , 41(1) : 40 -43 . DOI: 10.15892/j.cnki.djzdxb.2021.01.009

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