|Table of Contents|

Profile Planning for Attitude Maneuver of Flexible SpacecraftsBased on Multi-objective Optimization

《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

Issue:
2012年05期
Page:
846-
Research Field:
Publishing date:

Info

Title:
Profile Planning for Attitude Maneuver of Flexible SpacecraftsBased on Multi-objective Optimization
Author(s):
ZHOU Duan1SHEN Xiao-ning2GUO Yu1CHEN Qing-wei1HU Wei-li1
1. School of Automation,NUST,Nanjing 210094,China;2. School of Information andControl,Nanjing University of Information Science and Technology,Nanjing 210044,China
Keywords:
flexible spacecrafts attitude maneuver multi-objective optimization r-dominanceprofile planning
PACS:
TP18
DOI:
-
Abstract:
To solve the conflicts between rapidity and stability in the attitude maneuver control,aprofile planning and parameters optimization for the large angle maneuver of flexible spacecrafts arestudied here. Based on the dynamics analysis of flexible spacecrafts, a robust maneuver controlstrategy is designed,and a asymmetric trapezoidal speed profile is proposed. The multi-objective opti-mization model of the profile planning is constructed for the large angle rapid maneuver of flexiblespacecrafts,and an improved r-dominance multi-objective optimization algorithm for the planning isproposed to ensure the solution diversity and modify the expression of the decision maker爷spreferences. Simulation results demonstrate the effectiveness of the profile planning and the proposedoptimization method.

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Last Update: 2012-11-26