Distributed Optimization Method for Spacecraft Attitude Control and Vibration Suppression

No AccessEngineering NotesDistributed Optimization Method for Spacecraft Attitude Control and Vibration SuppressionYabo Hu, Franco Bernelli-Zazzera Yunhai GengYabo HuHarbin Institute of Technology, 150001 Harbin, People’s Republic China*Ph.D. Candidate, Research Center Satellite Technology; .Search more papers by this author, Bernelli-ZazzeraPolytechnic University Milan, 20156 Italy†Full Professor, Department Aerospace Science . Senior Member AIAA.Search author GengHarbin China‡Professor, authorPublished Online:1 Feb 2023https://doi.org/10.2514/1.G007097SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Singhose W. E., Banerjee A. K. Seering P., “Slewing Flexible with Deflection-Limiting Input Shaping,” Journal Guidance, Control, Dynamics, Vol. 20, No. 2, 1997, pp. 291–298. https://doi.org/10.2514/2.4036 LinkGoogle Scholar[2] Fracchia G., Biggs J. D. Ceriotti M., “Analytical Low-Jerk Reorientation Maneuvers Multi-Body Structures,” Acta Astronautica, 178, Jan. 2021, 1–14. https://doi.org/10.1016/j.actaastro.2020.08.020 CrossrefGoogle Scholar[3] Zhong C., Chen Z. Guo Y., “Attitude Disturbance Rejection,” IEEE Transactions on Electronic Systems, 53, 1, 2017, 101–110. https://doi.org/10.1109/TAES.2017.2649259 Scholar[4] Gennaro S. D., “Output Tracking Spacecraft,” Automatica, 38, 10, 2002, 1719–1726. https://doi.org/10.1016/S0005-1098(02)00082-1 Google Scholar[5] Hu Q. Ma “Variable Structure Active Suppression During Maneuver,” 9, 4, 2005, 307–317. https://doi.org/10.1016/j.ast.2005.02.001 Scholar[6] D’Eleuterio G. Hughes “Dynamics Gyroelastic Continua,” Applied Mechanics, 51, 1984, 415–422. https://doi.org/10.1115/1.3167634 Scholar[7] P. 1987, 401–405. https://doi.org/10.2514/3.20231 Scholar[8] Damaren C. “Optimal Large Space Structures Using Distributed Gyricity,” 12, 5, 1989, 723–731. https://doi.org/10.2514/3.20467 Scholar[9] “Controllability Observability Vehicles,” 14, 1991, 886–894. https://doi.org/10.2514/3.20728 Scholar[10] Q., Jia Y. Xu S., “Adaptive Linear Structural Moment Gyroscopes,” 37, 3, 2014, 990–996. https://doi.org/10.2514/1.62267 Scholar[11] Zhang J., Engineering, 29, 2016, Paper 04015027. https://doi.org/10.1061/(asce)as.1943-5525.0000513 Scholar[12] H., Modal Analysis Body Variable Speed Computational Nonlinear 11, 044506. https://doi.org/10.1115/1.4033438 Scholar[13] “Recursive Dynamics Algorithm Multibody Systems Variable-Speed 36, 2013, 1388–1398. https://doi.org/10.2514/1.59070 Scholar[14] Geng Wu B. Kong X., “Vibration Maneuver CMGs,” 72, 2018, 183–192. https://doi.org/10.1016/j.ast.2017.11.005 Scholar[15] “Space Gyroscope Null Motion,” 42, 2019, 2272–2278. https://doi.org/10.2514/1.g004344 Scholar[16] B., “Flexible Actuators,” 43, 2020, 2141–2147. https://doi.org/10.2514/1.G005190 Scholar[17] “Simultaneous via Allocation,” 44, 1853–1861. https://doi.org/10.2514/1.G005834 Scholar[18] Chang Huang Meng Liu Z., “Distributed Allocation Takeover Cellular Robot,” 41, 2499–2506. https://doi.org/10.2514/1.G003626 Scholar[19] W., Constrained Cellularized System,” 45, 2022, 385–393. https://doi.org/10.2514/1.G006266 Scholar[20] T.-H., Nedić Scaglione A., Consensus-Based Primal-Dual Perturbation Method,” Automatic 59, 6, 1524–1538. https://doi.org/10.1109/TAC.2014.2308612 Scholar[21] Han T., Cai K., Lin Yan Fu “A Resource over Dynamic Digraphs,” Signal Processing, 65, 2600–2612. https://doi.org/10.1109/TSP.2017.2669896 Scholar[22] Ozdaglar “Subgradient Methods Saddle-Point Problems,” Theory Applications, 142, 2009, 205–228. https://doi.org/10.1007/s10957-009-9522-7 Scholar[23] Ishii “Average Consensus General Strongly Connected 48, 2012, 2750–2761. https://doi.org/10.1016/j.automatica.2012.08.003 Scholar Previous article Next FiguresReferencesRelatedDetails What's Popular Volume 46, Number 4April 2023 CrossmarkInformationCopyright © the American Aeronautics Astronautics, Inc. All rights reserved. requests copying permission reprint should be submitted CCC at www.copyright.com; employ eISSN 1533-3884 initiate your request. See also AIAA Rights Permissions www.aiaa.org/randp. TopicsAerospace SciencesAlgorithms Data StructuresAstrodynamicsAstronauticsAttitude ControlComputing, Information, CommunicationControl SystemsData ScienceGuidance, Navigation, SystemsMechanical VibrationsOptimization AlgorithmSpacecraft ControlStructural EngineeringStructures, Design Test KeywordsSpacecraft ControlOptimization AlgorithmVibration SuppressionDistributed SystemMomentum Exchange ActuatorDistributed OptimizationAcknowledgmentsThe work reported in Note is partially supported China Scholarship Council National Natural Foundation (61903214).PDF Received5 July 2022Accepted23 December 2022Published online1 February