Title: Lyapunov-Based Guidance Law for Impact Time Control and Simultaneous Arrival
Abstract: No AccessEngineering NoteLyapunov-Based Guidance Law for Impact Time Control and Simultaneous ArrivalAbdul Saleem and Ashwini RatnooAbdul SaleemDepartment of Aerospace Engineering, Indian Institute of Science, Bangalore 560 012, India*Ph.D. Research Scholar, Autonomous Vehicles Laboratory, Department of Aerospace Engineering; .Search for more papers by this author and Ashwini RatnooDepartment of Aerospace Engineering, Indian Institute of Science, Bangalore 560 012, India†Assistant Professor, Autonomous Vehicles Laboratory, Department of Aerospace Engineering; .Search for more papers by this authorPublished Online:1 Jul 2015https://doi.org/10.2514/1.G001349SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Guelman M., Idan M. and Golan O. M., “Three Dimensional Minimum Energy Guidance,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 31, No. 2, 1995, pp. 835–841. doi:https://doi.org/10.1109/7.381933 IEARAX 0018-9251 CrossrefGoogle Scholar[2] Zarchan P., “Tactical and Strategic Missile Guidance,” Progress in Astronautics and Aeronautics, 6th ed., AIAA, Reston, VA, 2012, pp. 569–600. Google Scholar[3] Lu P., Doman D. B. and Schierman J. D., “Adaptive Terminal Guidance for Hypervelocity Impact in Specified Direction,” Journal of Guidance, Control, and Dynamics, Vol. 29, No. 2, 2006, pp. 269–278. doi:https://doi.org/10.2514/1.14367 JGCDDT 0162-3192 LinkGoogle Scholar[4] Ratnoo A. and Ghose D., “Impact Angle Constrained Interception of Stationary Targets,” Journal of Guidance, Control, and Dynamics, Vol. 31, No. 6, 2008, pp. 1816–1821. doi:https://doi.org/10.2514/1.37864 JGCDDT 0162-3192 LinkGoogle Scholar[5] Erer K. S. and Merttopçuoglu O., “Indirect Impact Angle Control Against Stationary Targets Using Biased Pure Proportional Navigation,” Journal of Guidance, Control, and Dynamics, Vol. 35, No. 2, 2012, pp. 700–704. doi:https://doi.org/10.2514/1.52105 JGCDDT 0162-3192 LinkGoogle Scholar[6] Tahk M. J., Ryoo C. K. and Cho H., “Recursive Time-to-Go Estimation for Homing Guidance Missiles,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 38, No. 1, 2002, pp. 13–24. doi:https://doi.org/10.1109/7.993225 IEARAX 0018-9251 CrossrefGoogle Scholar[7] Shin H. S., Cho H. and Tsourdos A., “Time-to-Go Estimation Using Guidance Command History,” Proceedings of the 18th IFAC World Congress, Elsevier Science Ltd., Kidlington, Oxford, Aug. 2011, pp. 5531–5536. doi:https://doi.org/10.3182/20110828-6-it-1002.03074 Google Scholar[8] Dhananjay N. and Ghose D., “Accurate Time-to-Go Estimation for Proportional Navigation Guidance,” Journal of Guidance, Control, and Dynamics, Vol. 37, No. 4, 2014, pp. 1378–1383. doi:https://doi.org/10.2514/1.G000082 JGCDDT 0162-3192 LinkGoogle Scholar[9] Jeon I. S., Lee J. I. and Tahk M. J., “Impact Time Control Guidance Law for Anti Ship Missiles,” IEEE Transactions on Control Systems Technology, Vol. 14, No. 2, 2006, pp. 260–266. doi:https://doi.org/10.1109/TCST.2005.863655 IETTE2 1063-6536 CrossrefGoogle Scholar[10] Lee J. I., Jeon I. S. and Tahk M. J., “Guidance Law to Control Impact Time and Angle,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 43, No. 1, 2007, pp. 301–310. doi:https://doi.org/10.1109/TAES.2007.357135 IEARAX 0018-9251 CrossrefGoogle Scholar[11] Kumar S. R. and Ghose D., “Sliding Mode Control Based Guidance Law with Impact Time Constraints,” 2013 American Control Conference, IEEE Publ., Piscataway, NJ, June 2013, pp. 5760–5765. doi:https://doi.org/10.1109/ACC.2013.6580740 Google Scholar[12] Kumar S. R. and Ghose D., “Impact Time and Angle Control Guidance,” Guidance, Navigation, and Control (GNC) Conference, AIAA Paper 2015-0616, Jan. 2015. doi:https://doi.org/10.2514/6.2015-0616 LinkGoogle Scholar[13] Kim T. H., Lee C. H., Jeon I. S. and Tahk M. J., “Augmented Polynomial Guidance with Impact Time and Angle Constraints,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 49, No. 4, 2013, pp. 2806–2817. doi:https://doi.org/10.1109/taes.2013.6621856 IEARAX 0018-9251 CrossrefGoogle Scholar[14] Kim M. and Kim Y., “Error Dynamics-Based Lyapunov Guidance Law for Stationary Target Observation,” Proceedings of the 18th IFAC World Congress, Elsevier Science Ltd., Kidlington, Oxford, Aug. 2011, pp. 2042–2047. doi:https://doi.org/10.3182/20110828-6-it-1002.00129 Google Scholar[15] Kim M. and Kim Y., “Lyapunov-Based Pursuit Guidance Law with Impact Angle Constraint,” Proceedings of the 19th IFAC World Congress, Elsevier Science Ltd., Kidlington, Oxford, Aug. 2014, pp. 2509–2514. doi:https://doi.org/10.3182/20140824-6-za-1003.00233 Google Scholar Previous article Next article
Publication Year: 2016
Publication Date: 2016-01-01
Language: en
Type: article
Indexed In: ['crossref']
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Cited By Count: 133
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