Path planning for maneuver of the satellite based on a multi-objective evolutionary algorithm

SHEN Xiao-ning; ZHOU Duan; GUO Yu; CHEN Qing-wei; HU Wei-li

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Path planning for maneuver of the satellite based on a multi-objective evolutionary algorithm

更新时间：2026-07-07

- Path planning for maneuver of the satellite based on a multi-objective evolutionary algorithm
- Vol. 25, Issue 8, (2010)
- 作者机构：
  
  1. 南京信息工程大学信息与控制学院,南京,210044
  2. 南京理工大学自动化学院,南京,210094
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2010
- 稿件说明：
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SHEN Xiao-ning, ZHOU Duan, GUO Yu, et al. Path planning for maneuver of the satellite based on a multi-objective evolutionary algorithm[J]. 2010, 25(8).
DOI：

SHEN Xiao-ning, ZHOU Duan, GUO Yu, et al. Path planning for maneuver of the satellite based on a multi-objective evolutionary algorithm[J]. 2010, 25(8). DOI：

摘要

建立了带挠性帆板卫星姿态控制问题的多目标优化模型

并基于一种多目标优化精英进化算法

规划卫星姿态机动的最优路径

以进一步提高卫星姿态控制系统的控制性能.仿真结果表明

所提方法只需运行一次

便能够有效地规划出一组多样性较好的非支配路径解

供决策者在不同的工作目标下选择

有效地缓解了卫星快速性、姿态稳定度、卫星机动所激发的帆板低振动强度之间的矛盾.

Abstract

The multi-objective optimization model for the attitude control of the flexible satellite was constructed

and a multi-objective optimization elitist evolutionary algorithm was applied to the path planning for large angle maneuver of flexible satellite

in order to further improve the performance of the attitude control system.Simulation results indicate that the proposed approach could find a diverse set of non-dominated path solutions efficiently in one run

whereby the decision maker can make a choice in the case of different working requirements.Meanwhile

the conflicts among criterions of rapidity

stability degree of the attitude and low vibration of solar panel caused by maneuver of the satellite can be alleviated.

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先进航空发动机协同创新中心

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