Simulating and Testing on Trajectory for Bomb with Parachute under Low Altitude Condition

Article Preview

Abstract:

With the development of precision guidance ammunitions, more and more parachutes are used for controlling speed and adjusting posture. At the same time, this will increase the complexity of movement for bomb with parachute. This paper created a simulating model of trajectory for bomb with parachute under low altitude condition. By the comparative study on theoretical trajectory and testing, it can determine the parameters and firing table, and it’s very useful for aircraft ammunition on research and development.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

670-675

Citation:

Online since:

September 2011

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2011 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Yingyuan Tian, Guozhao Yu and Jian Xiong: Ship Science and Technology (2009) (in chinese).

Google Scholar

[2] Yingyuan Tian, Xiaobo Hou and Cuilan Zhang: Mine Warfare & Ship Self-defence (2009) (in chinese).

Google Scholar

[3] Xingfang Qian, Ruixiong Lin and Yanan Zhao: Missile Flight Dynamics (Beijing Institute of Technology Press, Beijing 2006) (in chinese)

Google Scholar

[4] Yuwen Zhang: Torpedo Trajectory and Trajectory Design (Northwestern Polytechnical University Press, Xi'an 1999) (in chinese).

Google Scholar

[5] Shixing Yang, Naijin Li and Xuanzhi Xu: Aerial Torpedo Technology (Yunnan Science & Technology Press, Kunming 2001) (in chinese)

Google Scholar

[6] Lirong Wang and Jianping Wu: Parachute Theory and Application (China Astronautic Publishing House, Beijing 1997) (in chinese).

Google Scholar