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Optimal Attitude Sensors Placement for a Solar Power Satellite Considering Control–Structure Interaction

2019; American Institute of Aeronautics and Astronautics; Volume: 57; Issue: 10 Linguagem: Inglês

10.2514/1.j058570

1533-385X

Kaiming Zhang, S. Felix Wu, Yuliang Liu, Zhigang Wu,

Spacecraft Design and Technology

No AccessTechnical NotesOptimal Attitude Sensors Placement for a Solar Power Satellite Considering Control–Structure InteractionKaiming Zhang, Shunan Wu, Yuliang Liu and Zhigang WuKaiming ZhangDalian University of Technology, 116024 Dalian, People's Republic of China, Shunan WuDalian University of Technology, 116024 Dalian, People's Republic of China, Yuliang LiuDalian University of Technology, 116024 Dalian, People's Republic of China and Zhigang WuDalian University of Technology, 116024 Dalian, People's Republic of ChinaPublished Online:5 Aug 2019https://doi.org/10.2514/1.J058570SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Glaser P. E., "Power from the Sun: Its Future," Science, Vol. 162, No. 3856, 1968, pp. 857–861. doi:https://doi.org/10.1126/science.162.3856.857 CrossrefGoogle Scholar[2] Hyland D. C., Junkins J. L. and Longman R. 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Google Scholar Previous article FiguresReferencesRelatedDetailsCited byRecursive identification of inertia tensor parameters of space solar power satellite based on distributed placement of attitude sensorsAerospace Science and Technology, Vol. 130Optimal Attitude Sensor Placement and Modal Frequency Identification of Large Space StructureMultibody dynamics and robust attitude control of a MW-level solar power satelliteAerospace Science and Technology, Vol. 111Dynamics and on-orbit assembly strategies for an orb-shaped solar arrayActa Astronautica, Vol. 178 What's Popular Volume 57, Number 10October 2019Special Section on Asymptotic Analyses, Dynamics, and Aeroelasticity CrossmarkInformationCopyright © 2019 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAvionicsControl SystemsControl TheoryGuidance, Navigation, and Control SystemsSatellitesSensorsSpace SystemsSpace Systems and VehiclesSpacecraftsTransducers KeywordsSensorsSolar Power SatelliteAttitude Control SystemFinite Element ModelingDamping RatioLarge Space StructuresClosed Loop SystemGenetic AlgorithmPropellantFinite Element SoftwareAcknowledgmentsThis work was supported by the National Natural Science Foundation of China under Grant Nos. 11432010 and 11572069 and High-level Talent Innovation Support Program (2017RQ001).PDF Received23 April 2019Accepted5 July 2019Published online5 August 2019