Title: Composite Guidance Scheme for Impact Angle Control Against a Nonmaneuvering Moving Target
Abstract: No AccessEngineering NoteComposite Guidance Scheme for Impact Angle Control Against a Nonmaneuvering Moving TargetBong-Gyun Park, Hyuck-Hoon Kwon, Yoon-Hwan Kim and Tae-Hun KimBong-Gyun ParkLIG Nex1, Seongnam 463-400, Republic of Korea, Hyuck-Hoon KwonLIG Nex1, Seongnam 463-400, Republic of Korea, Yoon-Hwan KimLIG Nex1, Seongnam 463-400, Republic of Korea and Tae-Hun KimAgency for Defense Development, Daejeon 305-152, Republic of KoreaPublished Online:25 Jan 2016https://doi.org/10.2514/1.G001547SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Kim M. and Grider K. V., “Terminal Guidance for Impact Attitude Angle Constrained Flight Trajectories,” IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-9, No. 6, 1973, pp. 852–859. doi:https://doi.org/10.1109/TAES.1973.309659 CrossrefGoogle Scholar[2] Ryoo C. K., Cho H. and Tahk M. J., “Optimal Guidance Laws with Terminal Impact Angle Constraint,” Journal of Guidance, Control, and Dynamics, Vol. 28, No. 4, 2005, pp. 724–732. doi:https://doi.org/10.2514/1.839210.2514/1.8392 LinkGoogle Scholar[3] Ryoo C. K., Cho H. and Tahk M. J., “Time-to-Go Weighted Optimal Guidance with Impact Angle Constraints,” IEEE Transactions on Control Systems Technology, Vol. 14, No. 3, 2006, pp. 483–492. doi: 10.1109/TCST.2006.872525 CrossrefGoogle Scholar[4] Lu P., Doman D. and Schierman J., “Adaptive Terminal Guidance for Hypervelocity Impact in Specified Direction,” Journal of Guidance, Control, and Dynamics, Vol. 29, No. 2, 2006, pp. 269–278. doi: 10.2514/1.14367 LinkGoogle Scholar[5] Ratnoo A. and Ghose D., “Impact Angle Constrained Interception of Stationary Targets,” Journal of Guidance, Control, and Dynamics, Vol. 31, No. 6, 2008, pp. 1817–1822. doi:https://doi.org/10.2514/1.37864 LinkGoogle Scholar[6] Ratnoo A. and Ghose D., “Impact Angle Constrained Guidance Against Nonstationary Nonmaneuvering Targets,” Journal of Guidance, Control, and Dynamics, Vol. 33, No. 1, 2010, pp. 269–275. doi:https://doi.org/10.2514/1.45026 LinkGoogle Scholar[7] Erer K. S. and Merttopçuoğlu 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 LinkGoogle Scholar[8] Park B. G., Jeon B. J., Kim T. H., Tahk M. J. and Kim Y. H., “Composite Guidance Law for Impact Angle Control of Tactical Missiles with Passive Seekers,” Asia-Pacific International Symposium on Aerospace Technology, The Korean Soc. for Aeronautical & Space Sciences, Seoul, Korea, Nov. 2012, Paper 7.1.1. Google Scholar[9] Park B. G., Kim T. H., Tahk M. J. and Kim Y., H., “Composite Guidance Law for impact Angle Control of Passive Homing Missiles (in Korean),” Journal of the Korean Society for Aeronautical and Space Sciences, Vol. 42, No. 1, 2014, pp. 20–28. doi:https://doi.org/10.5139/JKSAS.2014.42.1.20 CrossrefGoogle Scholar[10] Park B. G., Kim T. H. and Tahk M. J., “Optimal Impact Angle Control Guidance Law Considering the Seeker’s Field-of-View Limits,” Journal of Aerospace Engineering, Vol. 227, No. 8, 2013, pp. 1347–1364. doi:https://doi.org/10.1177/0954410012452367 Google Scholar[11] Kim T. H., Park B. G. and Tahk M. J., “Bias-Shaping Method for Biased Proportional Navigation with Terminal-Angle Constraint,” Journal of Guidance, Control, and Dynamics, Vol. 36, No. 6, 2013, pp. 1810–1816. doi:https://doi.org/10.2514/1.59252 LinkGoogle Scholar[12] Tekin R. and Erer K. S., “Switched-Gain Guidance for Impact Angle Control Under Physical Constraints,” Journal of Guidance, Control, and Dynamics, Vol. 38, No. 2, 2015, pp. 205–216. doi:https://doi.org/10.2514/1.G000766 LinkGoogle Scholar[13] Erer K. S., Tekin R. and Özgören M. J., “Look Angle Constraint Impact Angle Control Based on Proportional Navigation,” AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2015-0091, Jan. 2015. doi: 10.2514/62015–0091 Google Scholar[14] Ratnoo A., “Analysis of Two-Stage Proportional Navigation with Heading Constraints,” Journal of Guidance, Control, and Dynamics (to be published). doi:https://doi.org/10.2514/1.G001262 Google Scholar[15] Guelman M., “Proportional Navigation with a Maneuvering Target,” IEEE Transactions on Aerospace and Electronic System, Vol. AES-8, No. 3, 1972, pp. 364–371. doi:https://doi.org/10.1109/TAES.1972.309520 CrossrefGoogle Scholar[16] Shneydor N. A., Missile Guidance and Pursuit: Kinematics, Dynamics and Control, Horwood Publ., Chichester, England, U.K., 1998, pp. 59–67. CrossrefGoogle Scholar[17] Kee P. E., Dong L. and Siong C. J., “Near Optimal Midcourse Guidance Law for Flight Vehicle,” AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 1998-0583, Jan. 1998. doi:10.2514/6.1998-583 Google Scholar Previous article Next article
Publication Year: 2016
Publication Date: 2016-05-01
Language: en
Type: article
Indexed In: ['crossref']
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Cited By Count: 51
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