[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]
BLAAISTIC AND AIRDYNAMICS

Optimization Design of Control Phase Trajectory About Extended Range Guided Projectile

  • ZHENG Yousheng ,
  • YANG Jianying ,
  • TANG Dilian ,
  • ZHOU Haiying
Expand
  • 1 Peking University,Beijing 100871,China
    2 Hongdu Aviation Industry Group Ltd, Nanchang 330024,China
    3 College of Civil and Environmental Engineering,East China Institute of Technology,Jiangxi Fuzhou 344000,China
    4 Yangzi College,East China Institute of Technology,Nanchang 330013,China

Received date: 2009-12-16

  Online published: 2025-05-28

Abstract

Some extended range guided projectile trajectory is best designed by this paper, In order to can control projectile flying path, the control phase was separate into sliding phase, accelerating phase and compensation over gravity phase go on research. According to the characteristic of guided projectile sliding phase, the exterior trajectory model was established, then give out a trajectory optimization arithmetic about gliding phase. The arithmetic need not go multifarious grads calculation, the calculation time much lesser to sequence quadratic programming algorithm. The simulation result indicate that the scheme of trajectory not only improve the projectile range, but also advance the projectile hit probability.

Cite this article

ZHENG Yousheng , YANG Jianying , TANG Dilian , ZHOU Haiying . Optimization Design of Control Phase Trajectory About Extended Range Guided Projectile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(6) : 155 -158 . DOI: 10.15892/j.cnki.djzdxb.2010.06.024

[an error occurred while processing this directive]

References

[1]
HG Bock, KJ Plitt. A multiple shooting algorithm for direct solution of optimal control problems[C]// Proc. of the IFAC 9th World Congress Budapest, 1984.
[2]
钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学[M]. 北京: 北京理工大学出版社, 2000.
[3]
史金光, 王中原, 易文俊, 等. 滑翔增程弹弹道特性分析[J]. 兵工学报, 2006, 27 (2): 210- 214.
[4]
高庆丰, 刘莉, 陈罗婧, 等. 末制导炮弹发动机点火时间的确定[J]. 弹道学报, 2005 (1): 88- 92.
[5]
胡朝江, 陈士橹. 改进直接多重打靶算法及其应用[J]. 飞行力学, 2004, 22 (1): 14- 17.
[6]
林国华, 胡朝江. 序列二次规划法解最优控制问题[J]. 飞行力学, 1994, 12 (4): 45- 49.
[7]
屈香菊. 直接多重打靶法在轨迹优化方面的应用[J]. 飞行力学, 1992, 10 (1): 13- 22.
[8]
蒋明, 宋卫东, 王泽川. 激光末制导炮弹过重力补偿比例导引律的分析[J]. 军械工程学院学报, 2007 (1): 47- 50.
Outlines

/

[an error occurred while processing this directive]