Control/Structure Integrated Design for Flexible Spacecraft Undergoing On-Orbit Maneuvers
Author:
Affiliation:
1. BHP Information Technology, Hamilton, New South Wales 2303, Australia
2. University of Queensland, Brisbane, Queensland 4072, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.4039
Reference24 articles.
1. Interdisciplinary interactions and dynamic systems integration
2. An Integrated Approach to the Minimum Weight and Optimum Control Design of Space Structures
3. Control-augmented structural synthesis
4. Optimal structural modifications to enhance the active vibration control of flexible structures
5. Enhanced vibration controllability by minor structural modifications
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2. Operational modal analysis of a liquid-filled cylindrical structure with decreasing filling mass by multivariate stochastic parameter evolution methods;International Journal of Mechanical Sciences;2020-04
3. Design and optimization of a space net capture system based on a multi-objective evolutionary algorithm;Acta Astronautica;2020-02
4. Control-structure integrated multiobjective design for flexible spacecraft using MOEA/D;Structural and Multidisciplinary Optimization;2014-02-27
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