宇航计测技术 ›› 2021, Vol. 41 ›› Issue (2): 49-53.doi: 10.12060/j.issn.1000-7202.2021.02.09

• 精密测试技术 • 上一篇    下一篇

飞行器质心偏差极限值计算方法研究

张艳玲, 洪蓓, 刘佳佳   

  1. 北京宇航系统工程研究所,北京 100076
  • 出版日期:2021-04-01 发布日期:2022-02-22
  • 作者简介:张艳玲(1981-),女,硕士,高级工程师,主要研究方向:飞行器弹道设计。

Research on Calculational Method of Limit Values for Flight Vehicles Centroidal Deviation

Zhang Yanling, Hong Bei , Liu Jiajia   

  1. Beijing Institute of Astronautical Systems Engineering, 100076, China
  • Online:2021-04-01 Published:2022-02-22

摘要: 针对飞行器的质心偏差极限值问题,首先经推导给出了质心偏差的理论计算公式,通过对理论公式的分析指出了其不足,随后分析了质心偏差分析的穷举法、蒙特卡洛方法和最优化方法,最后针对一种典型飞行器,对各种方法进行了实例分析。通过对计算结果的讨论,说明蒙特卡洛方法对偏差的分布较为有效,而穷举法和最优化方法对偏差极限值分析效果最好。

关键词: 质量质心, 质心误差, 误差分析

Abstract: This article is concerned with the centroidal deviation of flight vehicle. First, calculation formulas of centroidal deviation are given through theoretical derivation. The following analysis reveals the deficiency of these formulas. Then, exhaustive method, Monte Carlo method and an optimization method are investigated to research centroidal deviation. After that, examples of typical flight vehicle’s centroidal deviation are presented utilizing the above methods. The findings of the present study show that Monte Carlo method is most effective for distribution characteristics of centroidal deviation, whereas exhaustive method and optimization method perform better on deviation limit value analysis.

Key words: Mass centroid, Centroid error, error analysis