Time-optimal Attitude Reorientation Research of a Rigid Spacecraft

Xi-Jing Wang, Na Wang, Tao Hong, Min Tian

Abstract

The modified switching time optimization algorithm is used to solve minimum-time problem for the rest-torest reorientation of a non-inertial asymmetrical rigid-body spacecraft. The essential conditions for solving the problem is inducted with the minimum value principle. Based on the idea of homotopy algorithm, the relaxation time factor introduced into the Genetic algorithm, which is optimized to determine the switch features without the gyroscopic coupling. The improved Simulated Annealing method (Simulated Annealing SA) to determine the optimal trajectory of the switch point. Computer simulation results show its practicability.

References

  1. Feiyue Li, and Peter M. Bainum, vol. 13, no. 1, 1990. Numerical Approach for Solving Rigid Spacecraft Minimum Time Attitude Maneuvers. Journal of Guidance Control and Dynamics.
  2. Bilimoria, K. D., and Wie, B., Vol.16, No.3, 1993. TimeOptimal Three-Axis Reorientation of Rigid Spacecraft. Journal of Guidance Control and Dynamics.
  3. Xiaoli Bai and John L. Junkins, vol. 32, no. 4, 2009. New Results for Time-Optimal Three-Axis Reorientation of a Rigid Spacecraft. Journal of Guidance Control and Dynamics.
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Paper Citation


in Harvard Style

Wang X., Wang N., Hong T. and Tian M. (2015). Time-optimal Attitude Reorientation Research of a Rigid Spacecraft . In Proceedings of the Information Science and Management Engineering III - Volume 1: ISME, ISBN 978-989-758-163-2, pages 481-485. DOI: 10.5220/0006029004810485


in Bibtex Style

@conference{isme15,
author={Xi-Jing Wang and Na Wang and Tao Hong and Min Tian},
title={Time-optimal Attitude Reorientation Research of a Rigid Spacecraft},
booktitle={Proceedings of the Information Science and Management Engineering III - Volume 1: ISME,},
year={2015},
pages={481-485},
publisher={SciTePress},
organization={INSTICC},
doi={10.5220/0006029004810485},
isbn={978-989-758-163-2},
}


in EndNote Style

TY - CONF
JO - Proceedings of the Information Science and Management Engineering III - Volume 1: ISME,
TI - Time-optimal Attitude Reorientation Research of a Rigid Spacecraft
SN - 978-989-758-163-2
AU - Wang X.
AU - Wang N.
AU - Hong T.
AU - Tian M.
PY - 2015
SP - 481
EP - 485
DO - 10.5220/0006029004810485