Robust Enhanced Control Strategy of a Solar Power Satellite Using Multiple Sensors
2019; American Institute of Aeronautics and Astronautics; Volume: 43; Issue: 2 Linguagem: Inglês
10.2514/1.g004733
ISSN1533-3884
AutoresKaiming Zhang, S. Felix Wu, Zhigang Wu,
Tópico(s)Solar and Space Plasma Dynamics
ResumoNo AccessEngineering NotesRobust Enhanced Control Strategy of a Solar Power Satellite Using Multiple SensorsKaiming Zhang, Shunan Wu 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 and Zhigang WuDalian University of Technology, 116024 Dalian, People's Republic of ChinaPublished Online:25 Oct 2019https://doi.org/10.2514/1.G004733SectionsRead 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. https://doi.org/10.1126/science.162.3856.857 CrossrefGoogle Scholar[2] Carrington C., Fikes J., Gerry M., Perkinson D., Feingold H. and Olds J., "The Abacus/Reflector and Integrated Symmetrical Concentrator: Concepts for Space Solar Power Collection and Transmission," AIAA Paper 2000-3067, July 2000. https://doi.org/10.2514/6.2000-3067 Google Scholar[3] Sasaki S., Tanaka K., Higuchi K., Okuizumi N., Kawasaki S., Shinohara N., Senda K. and Ishimura K., "A New Concept of Solar Power Satellite: Tethered-SPS," Acta Astronautica, Vol. 60, No. 3, 2007, pp. 153–165. https://doi.org/10.1016/j.actaastro.2006.07.010 CrossrefGoogle Scholar[4] Seboldt W., Klimke M., Leipold M. and Hanowski W., "European Sail Tower SPS Concept," Acta Astronautica, Vol. 48, No. 5, 2001, pp. 785–792. https://doi.org/10.1016/S0094-5765(01)00046-7 CrossrefGoogle Scholar[5] Hou X., Wang L., Zhang X. and Zhou L., "Concept Design on Multi-Rotary Joints SPS," Journal of Astronautics, Vol. 26, No. 11, 2015, pp. 1332–1338. https://doi.org/10. 3873/j.issn.1000-1328.2015.11.016 Google Scholar[6] Oglevie R. E., "Attitude Control of Large Solar Power Satellites," Proceedings of AIAA Guidance and Control Conference, AIAA, Reston, VA, 1978, pp. 571–578. Google Scholar[7] Wie B. and Roithmayr C. M., "Attitude and Orbit Control of a Very Large Geostationary Solar Power Satellite," Journal of Guidance, Control, and Dynamics, Vol. 28, No. 3, 2005, pp. 439–451. https://doi.org/10.2514/1.6813 LinkGoogle Scholar[8] McNally I. J., Scheeres D. J. and Radice G., "Attitude Dynamics of Large Geosynchronous Solar Power Satellites," AIAA/AAS Astrodynamics Specialist Conference, AIAA Paper 2014-4123, 2014. https://doi.org/10.2514/6.2014-4123 LinkGoogle Scholar[9] Wu S., Zhang K., Peng H., Wu Z. and Radice G., "Robust Optimal Sun-Pointing Control of a Large Solar Power Satellite," Acta Astronautica, Vol. 127, Oct.–Nov. 2016, pp. 226–234. https://doi.org/10.1016/j.actaastro.2016.05.019 CrossrefGoogle Scholar[10] Li Q., Wang B., Deng Z., Ouyang H. and Wei Y., "A Simple Orbit-Attitude Coupled Modelling Method for Large Solar Power Satellites," Acta Astronautica, Vol. 145, April 2018, pp. 83–92. https://doi.org/10.1016/j.actaastro.2017.12.037 CrossrefGoogle Scholar[11] Li Q., Deng Z., Zhang K. and Wang B., "Precise Attitude Control of Multirotary-Joint Solar-Power Satellite," Journal of Guidance, Control, and Dynamics, Vol. 41, No. 6, 2018, pp. 1435–1442. https://doi.org/10.2514/1.G003309 LinkGoogle Scholar[12] Hu Q. and Zhang J., "Attitude Control and Vibration Suppression for Flexible Spacecraft Using Control Moment Gyroscopes," Journal of Aerospace Engineering, Vol. 29, No. 1, 2016, Paper 4015027. https://doi.org/10.1061/(ASCE)AS.1943-5525.0000513 Google Scholar[13] Hu Q., Su L., Cao Y. and Zhang J., "Decentralized Simple Adaptive Control for Large Space Structures," Journal of Sound and Vibration, Vol. 427, Aug. 2018, pp. 95–119. https://doi.org/10.1016/j.jsv.2018.04.033 CrossrefGoogle Scholar[14] Canavin J. R. and Likins P. W., "Floating Reference Frames for Flexible Spacecraft," Journal of Spacecraft, Vol. 14, No. 12, 1977, pp. 724–732. https://doi.org/10.2514/3.57256 LinkGoogle Scholar[15] Francis B. A. and Wonham W. M., "The Internal Model Principle of Control Theory," Automatica, Vol. 12, No. 5, 1976, pp. 457–465. https://doi.org/10.1016/0005-1098(76)90006-6 CrossrefGoogle Scholar[16] Skelton R. E., "Cost Decomposition of Linear Systems with Application to Model Reduction," International Journal of Control, Vol. 32, No. 6, 2007, pp. 1031–1055. https://doi.org/10.1080/00207178008910039 Google Scholar[17] Jia S. and Shan J., "Optimal Actuator Placement for Constrained Gyroelastic Beam Considering Control Spillover," Journal of Guidance, Control, and Dynamics, Vol. 41, No. 9, 2018, pp. 2073–2081. https://doi.org/10.2514/1.G003560 LinkGoogle Scholar[18] Yang C., Liang K., Zhang X. and Geng X., "Sensor Placement Algorithm for Structural Health Monitoring with Redundancy Elimination Model Based on Sub-Clustering Strategy," Mechanical Systems and Signal Processing, Vol. 124, June 2019, pp. 369–387. https://doi.org/10.1016/j.ymssp.2019.01.057 CrossrefGoogle Scholar[19] Yang C., Zheng W. and Zhang X., "Optimal Sensor Placement for Spatial Lattice Structure Based on Three-Dimensional Redundancy Elimination Model," Applied Mathematical Modelling, Vol. 66, Feb. 2019, pp. 576–591. https://doi.org/10.1016/j.apm.2018.09.034 CrossrefGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byA review of dynamic analysis on space solar power station13 July 2022 | Astrodynamics, Vol. 7, No. 2Recursive identification of inertia tensor parameters of space solar power satellite based on distributed placement of attitude sensorsAerospace Science and Technology, Vol. 130Effect Analysis of Gravity Gradient on Attitude–Elastic Motion of a Solar Power SatelliteKaiming Zhang, Shunan Wu and Zhigang Wu22 August 2022 | AIAA Journal, Vol. 60, No. 10Distributed cooperative control for vibration suppression of a flexible satelliteAerospace Science and Technology, Vol. 128Multibody dynamics and robust attitude control of a MW-level solar power satelliteAerospace Science and Technology, Vol. 111Database-driven Safe Flight Envelope Protection for Impaired AircraftYe Zhang, YingZhi Huang, Q Ping Chu and Coen C. de Visser5 January 2020 What's Popular Volume 43, Number 2February 2020 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 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAeronauticsAviationAviation RiskAviation SafetyAvionicsControl TheoryFeedback ControlGuidance, Navigation, and Control SystemsSensorsTransducers KeywordsSensorsSolar Power SatelliteAttitude Control SystemLinear Quadratic RegulatorElectric ThrustersCost AnalysisNumerical SimulationProportional DampingPropellantJapan Aerospace Exploration AgencyAcknowledgmentsThis 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 Received7 August 2019Accepted19 September 2019Published online25 October 2019
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