Application of Optimal Fitting in the Static Thrust Line Measurement of Solid Rocket Motor

Author:

Zhang Chun Fu1,Yan Qi Jin1,Zhang Jun1

Affiliation:

1. Yancheng Institute of Technology

Abstract

This paper takes a certain solid rocket engine as the research object, and studies the optimal measuring techniques of static trust line based on coordinate conversion. A simulation was taken to measure the thrust line of a rocket motor which has concave arc-paraboloid structure. The experiment proved that the technique proposed in this paper provided higher measuring efficiency and better accuracy.

Publisher

Trans Tech Publications, Ltd.

Reference5 articles.

1. Lai Pinan, Tian Weiping, Yu Zhenyong: Simulation Calculation of the Misalignment and Deflection of Thrust Line of Solid Rocket Motor. Journal Of Solid Rocket Technology, Vol. 22(1991), p.35.

2. Taur Der Ren,Chem Jeng Shing: Optimal Thrust Vector Control of Tactical Missiles,AIAA-97-3475, (1997).

3. Wang Chengxuan: Optimal Design of Internal Contour For Solid Motor Nozzle. Journal of Astronautics. Vol. 17, (1996), p.64.

4. Liu Jianbin, Tian Zhenyu, Guo Weibin, Hao Kegang: Research on Algorithm Mode of Optimization Problems. Computer Engineering and Applications. Vol. 23, (2005), p.27.

5. Grafarend E. W., Awange L. J.: Nonlinear analysis of the three dimensional datum transformation. Journal of Geodesy. Vol. 77, (2003), p.66.

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