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Journal of Projectiles, Rockets, Missiles and Guidance >

2015 , Vol. 35 >Issue 2: 118 - 120,125

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2015.02.030

BALLISIIC AND AIRDYNAMICS

Research on Simulation and Measurement System of a Two-dimensional Trajectory Correction Mechanism

  • ZHANG Dongxu ,
  • YAO Xiaoxian ,
  • CHEN Shuang ,
  • ZHANG Xin
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  • School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

Received date: 2014-03-14

  Online published: 2025-05-26

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Abstract

The simulation and measurement system was designed for a new type of two-dimensional trajectory correction mechanism in order to measure the parameters and dynamic performance of the new correction mechanism. With the simulation and measurement system, the working situation of the correction mechanism could be simulated and the pivotal parameters such as relative speed, electromagnetic torque and winding current could be sampled, stored and analyzed to evaluate the correction mechanism. Experiment shows that the simulation and measurement system has stable performance and the measurement results could lay experimental foundation for design and control of the correction mechanism.

Key words： virtual instrument; trajectory correction mechanism; micro generator; measurement system

Cite this article

ZHANG Dongxu , YAO Xiaoxian , CHEN Shuang , ZHANG Xin . Research on Simulation and Measurement System of a Two-dimensional Trajectory Correction Mechanism[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(2) : 118 -120,125 . DOI: 10.15892/j.cnki.djzdxb.2015.02.030

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