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Experimental Implementation of Riemann–Stieltjes Optimal Control for Agile Imaging Satellites

2015; American Institute of Aeronautics and Astronautics; Volume: 39; Issue: 1 Linguagem: Inglês

10.2514/1.g001325

1533-3884

Mark Karpenko, Ronald J. Proulx,

Space Satellite Systems and Control

No AccessEngineering NoteExperimental Implementation of Riemann–Stieltjes Optimal Control for Agile Imaging SatellitesMark Karpenko and Ronald J. ProulxMark KarpenkoDepartment of Mechanical and Aerospace Engineering, Naval Postgraduate School, Monterey, California 93943 and Ronald J. ProulxDepartment of Mechanical and Aerospace Engineering, Naval Postgraduate School, Monterey, California 93943Published Online:23 Jul 2015https://doi.org/10.2514/1.G001325SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Karpenko M., Bhatt S., Bedrossian N. and Ross I. M., "Flight Implementation of Shortest-Time Maneuvers for Imaging Satellites," Journal of Guidance, Control, and Dynamics, Vol. 37, No. 4, 2014, pp. 1069–1079. doi:https://doi.org/10.2514/1.62867 JGCDDT 0162-3192 LinkGoogle Scholar[2] McFarland D., Swenson E., Black J. and Cobb R., "Near Real-Time Closed-Loop Optimal Control Feedback for Spacecraft Attitude Maneuvers," AIAA Modeling and Simulation Technologies Conference, AIAA Paper 2009-5814, Aug. 2009. doi:https://doi.org/10.2514/6.2009-5814 LinkGoogle Scholar[3] Ross I. M. and Karpenko M., "A Review of Pseudospectral Optimal Control: From Theory to Flight," Annual Reviews in Control, Vol. 36, No. 2, Dec. 2012, pp. 182–197. doi:https://doi.org/10.1016/j.arcontrol.2012.09.002 1367-5788 CrossrefGoogle Scholar[4] Ross I. M., A Primer on Pontryagin's Principle in Optimal Control, 2nd ed., Collegiate Publ., San Francisco, 2015, Chap. 1. Google Scholar[5] Ross I. M., Proulx R. J., Karpenko M. and Gong Q., "Riemann–Stieltjes Optimal Control Problems for Uncertain Dynamical Systems," Journal of Guidance, Control, and Dynamics, Vol. 38, No. 7, 2015, pp. 1251–1263. doi:https://doi.org/10.2514/1.G000505 JGCDDT 0162-3192 LinkGoogle Scholar[6] Ross I. M., Proulx R. J. and Karpenko M., "Unscented Optimal Control for Space Flight," 24th International Symposium on Space Flight Dynamics (ISSFD), John Hopkins Univ. Applied Physics Lab., Laurel, MD, May 2014, http://issfd.org/ISSFD_2014/ISSFD24_Paper_S12-5_Karpenko.pdf [retrieved 13 June 2015]. Google Scholar[7] Ross I. M., Proulx R. J. and Karpenko M., "Unscented Optimal Control for Orbital and Proximity Operations in an Uncertain Environment: A New Zermelo Problem," Proceedings of the AIAA/AAS Astrodynamics Specialist Conference, AIAA Paper 2014-4423, Aug. 2014. doi:https://doi.org/10.2514/6.2014-4423 LinkGoogle Scholar[8] Wie B., Space Vehicle Dynamics and Control, AIAA, Reston, VA, 1998, Chap. 7. Google Scholar[9] Fleming A. and Ross I. M., "Singularity-Free Optimal Steering of Control Moment Gyros," Proceedings of the AAS Astrodynamics Specialist Conference, American Astronautical Soc. Paper 2005-418, Springfield, VA, Aug. 2005. Google Scholar[10] Fleming A. and Ross I. M., "Minimum-Time Maneuvering of CMG-Driven Spacecraft," Proceedings of the AAS Astrodynamics Specialist Conference, American Astronautical Soc. Paper 2007-355, Springfield, VA, Aug. 2007. Google Scholar[11] Karpenko M. and Ross I. M., "Implementation of Shortest-Time Maneuvers for Generic CMG Steering Laws," Proceedings of the AIAA/AAS Astrodynamics Specialist Conference, AIAA Paper 2012-4959, Aug. 2012. doi:https://doi.org/10.2514/6.2012-4959 LinkGoogle Scholar[12] Vadali S. R., Walker S. R. and Oh H.-S., "Preferred Gimbal Angles for Single Gimbal Control Moment Gyros," Journal of Guidance, Control, and Dynamics, Vol. 13, No. 6, 1990, pp. 1090–1095. doi:https://doi.org/10.2514/3.20583 JGCDDT 0162-3192 LinkGoogle Scholar[13] McMickell B., Buchele P., Gisler G. and Andrus J., "Control Moment Gyroscope Based Momentum Control Systems in Small Satellites," U.S. Patent US8312782 B2, issued Nov. 20, 2012. Google Scholar Previous article Next article