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Proceedings Paper

Emulation of rocket trajectory based on a six degree of freedom model
Author(s): Wenpeng Zhang; Fan Li; Zhong Wu; Rong Li
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Paper Abstract

In this paper, a 6-DOF motion mathematical model is discussed. It is consisted of body dynamics and kinematics block, aero dynamics block and atmosphere block. Based on Simulink, the whole rocket trajectory mathematical model is developed. In this model, dynamic system simulation becomes easy and visual. The method of modularization design gives more convenience to transplant. At last, relevant data is given to be validated by Monte Carlo means. Simulation results show that the flight trajectory of the rocket can be simulated preferably by means of this model, and it also supplies a necessary simulating tool for the development of control system.

Paper Details

Date Published: 13 October 2008
PDF: 8 pages
Proc. SPIE 7128, Seventh International Symposium on Instrumentation and Control Technology: Measurement Theory and Systems and Aeronautical Equipment, 71282H (13 October 2008); doi: 10.1117/12.806878
Show Author Affiliations
Wenpeng Zhang, Beijing Univ. of Aeronautics and Astronautics (China)
Fan Li, Beijing Univ. of Aeronautics and Astronautics (China)
Zhong Wu, Beijing Univ. of Aeronautics and Astronautics (China)
Rong Li, Beijing Univ. of Aeronautics and Astronautics (China)


Published in SPIE Proceedings Vol. 7128:
Seventh International Symposium on Instrumentation and Control Technology: Measurement Theory and Systems and Aeronautical Equipment

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