Dynamics and Control of a Probe Tethered to an Asteroid
2018; American Institute of Aeronautics and Astronautics; Volume: 41; Issue: 7 Linguagem: Inglês
10.2514/1.g003386
ISSN1533-3884
Autores Tópico(s)Planetary Science and Exploration
ResumoNo AccessEngineering NoteDynamics and Control of a Probe Tethered to an AsteroidRui Zhong and Yue WangRui ZhongBeihang University, 100083 Beijing, People's Republic of China and Yue WangBeihang University, 100083 Beijing, People's Republic of ChinaPublished Online:30 Apr 2018https://doi.org/10.2514/1.G003386SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Wen H., Jin D. and Hu H., "Advances in Dynamics and Control of Tethered Satellite Systems," Acta Mechanica Sinica, Vol. 24, No. 3, 2008, pp. 229–241. doi:https://doi.org/10.1007/s10409-008-0159-9 LHHPAE 0567-7718 CrossrefGoogle Scholar[2] National Research Council, "NASA Space Technology Roadmaps and Priorities: Restoring NASA's Technological Edge and Paving the Way for a New Era in Space," National Academies Press, Washington, D.C., 2012, Appendix E 16–17. Google Scholar[3] Ziegler S. W. and Cartmell M. P., "Using Motorised Tethers for Payload Orbital Transfer," Journal of Spacecraft and Rockets, Vol. 38, No. 6, 2001, pp. 904–913. doi:https://doi.org/10.2514/2.3762 JSCRAG 0022-4650 LinkGoogle Scholar[4] Bischof B., "Roger—Robotic Geostationary Orbit Restorer," 54th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law, Paper IAC-03-IAA.5.2.08, 2003. Google Scholar[5] Qi R., Misra A. K. and Zuo Z., "Active Debris Removal Using Double-Tethered Space-Tug System," Journal of Guidance, Control and Dynamics, Vol. 40, No. 5, 2017, pp. 720–728. doi:https://doi.org/10.2514/1.G000699 Google Scholar[6] Qi R. and Misra A. K., "Dynamics of Double-Pyramid Satellite Formations Interconnected by Tethers and Coulomb Forces," Journal of Guidance, Control, and Dynamics, Vol. 39, No. 6, 2016, pp. 1265–1277. doi:https://doi.org/10.2514/1.G001781 LinkGoogle Scholar[7] Zhong R. and Zhu Z. H., "Optimal Current Switching Control of Electrodynamic Tethers for Fast Deorbit," Journal of Guidance, Control, and Dynamics, Vol. 37, No. 5, 2014, pp. 1501–1511. doi:https://doi.org/10.2514/1.G000385 JGCODS 0731-5090 LinkGoogle Scholar[8] Li G. Q. and Zhu Z. H., "Long-Term Dynamic Modeling of Tethered Spacecraft Using Nodal Position Finite Element Method and Symplectic Integration," Celestial Mechanics & Dynamical Astronomy, Vol. 123, No. 4, 2015, pp. 363–386. doi:https://doi.org/10.1007/s10569-015-9640-5 CrossrefGoogle Scholar[9] French D. B. and Mazzoleni A. P., "Use of Tethered Ballast Mass for Near Earth Object (NEO) Collision Avoidance," 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA Paper 2015-1181, 2015. Google Scholar[10] French D. B. and Mazzoleni A. P., "Asteroid Diversion Using a Long Tether and Ballast," Journal of Spacecraft and Rockets, Vol. 46, No. 3, 2009, pp. 645–661. doi:https://doi.org/10.2514/1.40828 JSCRAG 0022-4650 LinkGoogle Scholar[11] Mashayekhi M. J. and Misra A. K., "Tether Assisted Near Earth Object Diversion," Acta Astronautica, Vol. 75, June–July 2012, pp. 71–77. doi:https://doi.org/10.1016/j.actaastro.2011.12.018 AASTCF 0094-5765 CrossrefGoogle Scholar[12] Mashayekhi M. J. and Misra A. K., "Optimization of Tether-Assisted Asteroid Deflection," Journal of Guidance, Control, and Dynamics, Vol. 37, No. 3, 2014, pp. 898–906. doi:https://doi.org/10.2514/1.60176 JGCODS 0731-5090 LinkGoogle Scholar[13] Bazzocchi M. C. F. and Emami M. R., "A Systematic Assessment of Asteroid Redirection Methods for Resource Exploitation," 8th Symposium on Space Resource Utilization, AIAA Paper 2015-1181, 2015. LinkGoogle Scholar[14] Barucci M. A., Dotto E. and Levasseur-Regourd A. C., "Space Missions to Small Bodies: Asteroids and Cometary Nuclei," Astronomy & Astrophysics Review, Vol. 19, No. 1, 2011, p. 48. doi:https://doi.org/10.1007/s00159-011-0048-2 CrossrefGoogle Scholar[15] Mashayekhi M. J., Misra A. K. and Keshmiri M., "Dynamics of a Tether System Connected to an Irregularly Shaped Celestial Body," The Journal of the Astronautical Sciences, Vol. 63, No. 3, 2016, pp. 206–220. doi:https://doi.org/10.1007/s40295-016-0088-y CrossrefGoogle Scholar[16] Zhong R. and Wang Y., "Research on the Tether Assisted Observation of an Asteroid," Acta Astronautica, Vol. 123, June–July 2016, pp. 310–319. doi:https://doi.org/10.1016/j.actaastro.2016.03.027 AASTCF 0094-5765 CrossrefGoogle Scholar[17] Wen H., Zhu Z. H., Jin D. and Hu H., "Space Tether Deployment Control with Explicit Tension Constraint and Saturation Function," Journal of Guidance, Control, and Dynamics, Vol. 39, No. 4, 2016, pp. 916–921. doi:https://doi.org/10.2514/1.G001356 JGCODS 0731-5090 LinkGoogle Scholar[18] Cong B., Liu X. and Chen Z., "Improved Adaptive Sliding Mode Control for a Class of Second-Order Mechanical Systems," Asian Journal of Control, Vol. 15, No. 6, 2013, pp. 1862–1866. doi:https://doi.org/10.1002/asjc.2013.15.issue-6 CrossrefGoogle Scholar[19] Werner R. and Scheeres D., "Exterior Gravitation of a Polyhedron Derived and Compared with Harmonic and Mascon Gravitation Representations of Asteroid 4769 Castalia," Celestial Mechanics and Dynamical Astronomy, Vol. 65, No. 3, 1997, pp. 313–344. doi:https://doi.org/10.1007/BF00053511 CrossrefGoogle Scholar[20] Yoo S. D. and Chung M. J., "A Variable Structure Control with Simple Adaptation Laws for Upper Bounds on the Norm of the Uncertainties," IEEE Transactions on Automatic Control, Vol. 37, No. 6, 1992, pp. 860–865. doi:https://doi.org/10.1109/9.256348 IETAA9 0018-9286 CrossrefGoogle Scholar[21] Biannic J.-M. and Tarbouriech S., "Optimization and Implementation of Dynamic Anti-Windup Compensators with Multiple Saturations in Flight Control Systems," Control Engineering Practice, Vol. 17, No. 6, 2009, pp. 703–713. doi:https://doi.org/10.1016/j.conengprac.2008.11.002 COEPEL 0967-0661 CrossrefGoogle Scholar[22] Wheeler G., Su C.-Y. and Stepanenko Y., "A Sliding Mode Controller with Improved Adaptation Laws for the Upper Bounds on the Norm of Uncertainties," Automatica, Vol. 34, No. 12, 1998, pp. 1657–1661. doi:https://doi.org/10.1016/S0005-1098(98)80024-1 ATCAA9 0005-1098 CrossrefGoogle Scholar[23] Corless M. and Leitmann G., "Continuous State Feedback Guaranteeing Uniform Ultimate Boundedness for Uncertain Dynamic Systems," IEEE Transactions on Automatic Control, Vol. 26, No. 5, 1981, pp. 1139–1144. doi:https://doi.org/10.1109/TAC.1981.1102785 IETAA9 0018-9286 CrossrefGoogle Scholar[24] Scheeres D. J., "Orbit Mechanics About Asteroids and Comets," Journal of Guidance, Control, and Dynamics, Vol. 35, No. 3, 2012, pp. 987–997. doi:https://doi.org/10.2514/1.57247 JGCODS 0731-5090 LinkGoogle Scholar[25] Scheeres D. J., "Close Proximity Dynamics and Control About Asteroids," 2014 American Control Conference (ACC), IEEE Publ., Piscataway, NJ, June 2014, pp. 1584–1598. Google Scholar[26] Byram S. M. and Scheeres D. J., "Stability of Sun-Synchronous Orbits in the Vicinity of a Comet," Journal of Guidance, Control, and Dynamics, Vol. 32, No. 5, 2009, pp. 1550–1559. doi:https://doi.org/10.2514/1.41655 JGCODS 0731-5090 LinkGoogle Scholar[27] Scheeres D. J., Sutter B. M. and Rosengren A. J., "Design, Dynamics and Stability of the OSIRIS-REx Sun-Terminator Orbits," The 23rd AAS/AIAA Space Flight Mechanics Meeting, AAS Paper 13-151, Univelt Inc., Escondido, CA, Feb. 2013, pp. 3263–3282. Google Scholar[28] Rosengren A. J. and Scheeres D. J., "Long-Term Dynamics of High Area-to-Mass Ratio Objects in High-Earth Orbit," Advances in Space Research, Vol. 52, No. 8, 2013, pp. 1545–1560. doi:https://doi.org/10.1016/j.asr.2013.07.033 ASRSDW 0273-1177 CrossrefGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byOrbit–attitude dynamics and control of spacecraft hovering over a captured asteroid in the earth–moon system16 January 2022 | Aerospace Systems, Vol. 5, No. 2Station-keeping of a solar weather detector by a tethered-sailcraft within elliptic Sun-Earth restricted three-body systemAdvances in Space Research, Vol. 68, No. 9Chaos in a tethered satellite system induced by atmospheric drag and Earth's oblateness10 August 2020 | Nonlinear Dynamics, Vol. 101, No. 2 What's Popular Volume 41, Number 7July 2018 CrossmarkInformationCopyright © 2018 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 ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAsteroidsPlanetary Science and ExplorationPlanetsPropulsion and PowerSolar PhysicsSpace AgenciesSpace MissionsSpace Science and TechnologySpace TethersSpacecraft Propulsion KeywordsAsteroidsElectrodynamic TetherSolar RadiationEarthPlanetary Data SystemSatellite Formation FlyingNumerical SimulationAsteroid MissionsFeedback ControlNumerical OptimizationAcknowledgmentsThe authors acknowledge the support of the National Natural Science Foundation of China (Grant Nos. 11772023 and 11602009) and the support of the Fundamental Research Funds for the Central Universities.PDF Received12 October 2017Accepted11 March 2018Published online30 April 2018
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