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- W2225589210 abstract "No AccessEngineering NoteGeometric Attitude Motion Planning for Spacecraft with Pointing and Actuator ConstraintsJames D. Biggs and Lucy ColleyJames D. BiggsPolitecnico di Milano, 20156 Milan, Italy*Associate Professor, Department of Aerospace Science and Technology; .Search for more papers by this author and Lucy ColleyUniversity of Strathclyde, Glasgow, Scotland G1 1XJ, United KingdomUndergraduate Student, Department of Mechanical and Aerospace Engineering; .Search for more papers by this authorPublished Online:8 Jan 2016https://doi.org/10.2514/1.G001514SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Hablani H. B., Attitude Commands Avoiding Bright Objects and Maintaining Communication with Ground Station, Journal of Guidance, Control, and Dynamics, Vol. 39, No. 1, 1999, pp. 759–767. doi:https://doi.org/10.2514/2.4469 LinkGoogle Scholar[2] McInnes C. R., Large Angle Slew Maneuverss with Autonomous Sun Vector Avoidance, Journal of Guidance, Control, and Dynamics, Vol. 17, No. 4, 1994, pp. 875–877. doi:https://doi.org/10.2514/3.21283 LinkGoogle Scholar[3] Kjellberg H. C. and Lightsey E. G., Discretized Constrained Attitude Pathfinding and Control for Satellites, Journal of Guidance, Control, and Dynamics, Vol. 36, No. 5, 2013, pp. 1301–1309. doi:https://doi.org/10.2514/1.60189 LinkGoogle Scholar[4] Frazzoli E., Dahleh M. A., Feron E. and Kornfeld R., A Randomized Attitude Slew Planning Algorithm for Autonomous Spacecraft, AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2001-4155, 2001. Google Scholar[5] Boyarko G., Romano M. and Yakimenko O., Time-Optimal Reorientation of a Spacecraft Using an Inverse Dynamics Optimization Method, Journal of Guidance, Control, and Dynamics, Vol. 34, No. 4, 2011, pp. 1197–1208. doi:https://doi.org/10.2514/1.4944 LinkGoogle Scholar[6] Caubet A. and Biggs J., A Motion Planning Method for Spacecraft Attitude Maneuvers Using Single Polynomials, AAS/AIAA Astrodynamics Specialist Conference, American Astronautical Soc./AIAA, Reston, VA, Aug. 2015. Google Scholar[7] Spindler K., Optimal Attitude Control of a Rigid Body, Applied Mathematics and Optimization, Vol. 34, No. 1, 1996, pp. 79–90. doi:https://doi.org/10.1007/BF01182474 CrossrefGoogle Scholar[8] Jurdjevic V., Geometric Control Theory, Advanced Studies in Mathematics, Vol. 52, Cambridge Univ. Press, New York, 1997, pp. 362–401. Google Scholar[9] Biggs J., Maclean C. and Caubet A., Heteroclinic Optimal Control Solutions for Attitude Motion-Planning, Australian Control Conference, IEEE Publ., Piscataway, NJ, 2013, pp. 218–223. doi:https://doi.org/10.1109/AUCC.2013.6697276 Google Scholar[10] Mathematica, Software Package, Ver. 10.2, Wolfram Research, Inc., Champaign, IL, 2015.. Google Scholar[11] Maclean C., Pagnozzi D. and Biggs J., Planning Natural Repointing Manoeuvres for Nano-Spacecraft, IEEE Transactions on Aerospace and Electronic Systems, Vol. 50, No. 3, pp. 2129–2145. doi:https://doi.org/10.1109/TAES.2014.130417 CrossrefGoogle Scholar Previous article Next article" @default.
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