Optimal Disturbance Attenuation Approach with Measurement Feedback to Missile Guidance

No AccessEngineering NotesOptimal Disturbance Attenuation Approach with Measurement Feedback to Missile GuidanceBarak Or, Joseph Z. Ben-Asher and Isaac YaeshBarak Or https://orcid.org/0000-0002-6615-7639University of Haifa, 3498838 Haifa, Israel*Ph.D. Candidate, Department of Marine Technologies. Student Member AIAA.Search for more papers by this author, Joseph Z. Ben-AsherTechnion, Israel Institute of Technology, 32000 Haifa, Israel†Professor, Faculty of Aerospace Engineering. Associate Fellow AIAA.Search for more papers by this author and Isaac YaeshElbit Systems, Ltd., 47100 Ramat Hasharon, Israel‡Head of Department, Israel Military Industries Advanced Systems Division.Search for more papers by this authorPublished Online:31 Mar 2021https://doi.org/10.2514/1.G005468SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Isaacs R., Differential Games: A Mathematical Theory with Applications to Warfare and Pursuit, Control and Optimization, Dover Publ., New York, 1999, Chaps. 1–4. Google Scholar[2] Bryson A. E. and Ho Y.-C., Applied Optimal Control: Optimization, Estimization and Control, Vol. 2, Hemisphere, Washington, D.C., 1975, Chaps. 4, 5, 12–14. Google Scholar[3] Ben-Asher J. Z. and Yaesh I., Advances in Missile Guidance Theory, Vol. 180, AIAA, Reston, VA, 1998, Chaps. 2–4. Google Scholar[4] Speyer J., “An Adaptive Terminal Guidance Scheme Based on an Exponential Cost Criterion with Application to Homing Missile Guidance,” IEEE Transactions on Automatic Control, Vol. 21, No. 3, 1976, pp. 371–375. https://doi.org/10.1109/TAC.1976.1101206 CrossrefGoogle Scholar[5] Ben-Asher J. Z. and Speyer J. L., “Games in Aerospace: Homing Missile Guidance,” Handbook of Dynamic Game Theory, Springer, Berlin, 2017, pp. 1–28. Google Scholar[6] Ben-Asher J. Z., Levinson S., Shinar J. and Weiss H., “Trajectory Shaping in Linear-Quadratic Pursuit-Evasion Games,” Journal of Guidance, Control, and Dynamics, Vol. 27, No. 6, 2004, pp. 1102–1105. https://doi.org/10.2514/1.9765 LinkGoogle Scholar[7] Oshman Y. and Davidson P., “Optimization of Observer Trajectories for Bearings-Only Target Localization,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 35, No. 3, 1999, pp. 892–902. https://doi.org/10.1109/7.784059 CrossrefGoogle Scholar[8] Speyer J. L. and Jacobson D. H., Primer on Optimal Control Theory, Vol. 20, SIAM, Philadelphia, 2010, pp. 231–254. Google Scholar[9] Or B., Ben-Asher J. Z. and Yaesh I., “Pursuit Evasion Games with Imperfect Information Revisited,” Israel Annual Conference on Aerospace Sciences, Technion—Israel Inst. of Technology, Haifa, Israel, 2018, pp. 1147–1170. Google Scholar[10] Shaked U. and Yaesh I., “Estimation Variance and H/Sub Infinity/-Error Minimization of Stationary Process with Perfect Measurements,” IEEE Transactions on Automatic Control, Vol. 35, No. 3, 1990, pp. 310–314. https://doi.org/10.1109/9.50343 Google Scholar[11] Green M. and Limebeer D. J., Robust Linear Control, Prentice-Hall, Hoboken, NJ, 1994, pp. 107–122. Google Scholar[12] Zermelo E., “Über das Navigationsproblem bei Ruhender Oder Veränderlicher Windverteilung,” ZAMM-Journal of Applied Mathematics and Mechanics/Zeitschrift für Angewandte Mathematik und Mechanik, Vol. 11, No. 2, 1931, pp. 114–124. https://doi.org/10.1002/zamm.19310110205 CrossrefGoogle Scholar[13] Or B., “Integrated Guidance/Estimation in Linear Quadratic Differential Games,” M.Sc. Thesis, Technion—Israel Inst. of Technology, Haifa, Israel, 2018. Google Scholar[14] Bar-Shalom Y., Li X. R. and Kirubarajan T., Estimation with Applications to Tracking and Navigation: Theory Algorithms and Software, Wiley, New York, 2004, p. 185. Google Scholar Previous article FiguresReferencesRelatedDetails What's Popular Volume 44, Number 5May 2021 CrossmarkInformationCopyright © 2021 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 eISSN 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAir NavigationControl TheoryGuidance, Navigation, and Control SystemsGuided MissilesKalman FilterMilitary ScienceMilitary TechnologyMissile DefenseMissile Guidance and ControlMissile Systems, Dynamics and TechnologyMissilesNavigational GuidanceOptimal Control Theory KeywordsMissile GuidanceMarine TechnologyKalman FilterOptimal ControlHeading AngleLinear Time InvariantNumerical SimulationProportional NavigationTarget MissilesRiccati EquationsPDF Received15 June 2020Accepted1 March 2021Published online31 March 2021