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• W2892054190 abstract "No AccessEngineering NoteActive Defense Guidance Law via Cooperative Identification and EstimationXinguang Zou, Di Zhou, Runle Du and Jiaqi LiuXinguang ZouHarbin Institute of Technology, 150001 Harbin, People’s Republic of China*Associate Professor, School of Electrical Engineering and Automation, Mailbox 327; .Search for more papers by this author, Di ZhouHarbin Institute of Technology, 150001 Harbin, People’s Republic of China†Professor, Department of Control Science and Engineering, Mailbox 327; (Corresponding Author).Search for more papers by this author, Runle DuNational Key Laboratory of Science and Technology on Test Physics and Numerical Mathematics, 100076 Beijing, People’s Republic of China‡Staff Engineer, P.O. Box 9200-76-7; .Search for more papers by this author and Jiaqi LiuNational Key Laboratory of Science and Technology on Test Physics and Numerical Mathematics, 100076 Beijing, People’s Republic of China§Staff Engineer, P.O. Box 9200-76-7; .Search for more papers by this authorPublished Online:2 Sep 2018https://doi.org/10.2514/1.G003372SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Boyell R. L., “Defending a Moving Target Against Missile or Torpedo Attack,” IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-12, No. 4, 1976, pp. 522–526. doi:https://doi.org/10.1109/TAES.1976.308338 IEARAX 0018-9251 CrossrefGoogle Scholar[2] Shima T., “Optimal Cooperative Pursuit and Evasion Strategies Against a Homing Missile,” Journal of Guidance, Control, and Dynamics, Vol. 34, No. 2, 2011, pp. 414–425. doi:https://doi.org/10.2514/1.51765 JGCODS 0731-5090 LinkGoogle Scholar[3] Prokopov O. and Shima T., “Linear Quadratic Optimal Cooperative Strategies for Active Aircraft Protection,” Journal of Guidance, Control, and Dynamics, Vol. 36, No. 3, 2013, pp. 753–764. doi:https://doi.org/10.2514/1.58531 JGCODS 0731-5090 LinkGoogle Scholar[4] Shaferman V. and Shima T., “Cooperative Multiple-Model Adaptive Guidance for an Aircraft Defending Missile,” Journal of Guidance, Control, and Dynamics, Vol. 33, No. 6, 2010, pp. 1801–1813. doi:https://doi.org/10.2514/1.49515 JGCODS 0731-5090 LinkGoogle Scholar[5] Rusnak I., Weiss H. and Hexner G., “Guidance Laws in Target-Missile-Defender Scenario with an Aggressive Defender,” 18th IFAC World Congress in Italy, International Federation of Automatic Control, Laxenburg, Austria, 2011, pp. 9349–9354. doi:https://doi.org/10.3182/20110828-6-IT-1002.02587 Google Scholar[6] Perelman A., Shima T. and Rusnak I., “Cooperative Differential Games Strategies for Active Aircraft Protection from a Homing Missile,” Journal of Guidance, Control, and Dynamics, Vol. 34, No. 3, 2011, pp. 761–773. doi:https://doi.org/10.2514/1.51611 JGCODS 0731-5090 LinkGoogle Scholar[7] Ratnoo A. and Shima T., “Line-of-Sight Interceptor Guidance for Defending an Aircraft,” Journal of Guidance, Control, and Dynamics, Vol. 34, No. 2, 2011, pp. 522–532. doi:https://doi.org/10.2514/1.50572 JGCODS 0731-5090 LinkGoogle Scholar[8] Yamasaki T., Balakrishnan S. N. and Takano H., “Geometrical Approach-Based Defense-Missile Intercept Guidance for Aircraft Protection Against Missile Attack,” Journal of Aerospace Engineering, Vol. 226, No. 8, 2012, pp. 1014–1028. doi:https://doi.org/10.1177/0954410011416053 Google Scholar[9] Zou X. G., Zhou D., Du R. L. and Liu J. Q., “Adaptive Nonsingular Terminal Sliding Mode Cooperative Guidance Law in Active Defense Scenario,” Journal of Aerospace Engineering, Vol. 230, No. 2, 2016, pp. 307–320. doi:https://doi.org/10.1177/0954410015591613 Google Scholar[10] Ratnoo A., “Analysis of Two-Stage Proportional Navigation with Heading Constraints,” Journal of Guidance, Control, and Dynamics, Vol. 39, No. 1, 2016, pp. 156–164. doi:https://doi.org/10.2514/1.G001262 JGCODS 0731-5090 LinkGoogle Scholar[11] Magill D. T., “Optimal Adaptive Estimation of Sampled Stochastic Processes,” IEEE Transactions on Automatic Control, Vol. 10, No. 4, 1965, pp. 434–439. doi:https://doi.org/10.1109/TAC.1965.1098191 IETAA9 0018-9286 CrossrefGoogle Scholar[12] Rusnak I., “Multiple Model-Based Terminal Guidance Law,” Journal of Guidance, Control, and Dynamics, Vol. 23, No. 4, 2000, pp. 742–746. doi:https://doi.org/10.2514/2.4593 JGCODS 0731-5090 LinkGoogle Scholar[13] Oshman Y., Shinar J. and Weizman S. A., “Using a Multiple-Model Adaptive Estimator in a Random Evasion Missile/Aircraft Encounter,” Journal of Guidance, Control, and Dynamics, Vol. 24, No. 6, 2001, pp. 1176–1186. doi:https://doi.org/10.2514/2.4833 JGCODS 0731-5090 LinkGoogle Scholar[14] Shima T., Oshman Y. and Shinar J., “Efficient Multiple Model Adaptive Estimation in Ballistic Missile Interception Scenarios,” Journal of Guidance, Control, and Dynamics, Vol. 25, No. 4, 2002, pp. 667–675. doi:https://doi.org/10.2514/2.4961 JGCODS 0731-5090 LinkGoogle Scholar[15] Shaferman V. and Shima T., “Cooperative Multiple-Model Adaptive Guidance for an Aircraft Defending Missile,” Journal of Guidance, Control, and Dynamics, Vol. 33, No. 6, 2010, pp. 1801–1813. doi:https://doi.org/10.2514/1.49515 JGCODS 0731-5090 LinkGoogle Scholar[16] Li X. R., Zhi X. R. and Zhang X. M., “Multiple-Model Estimation with Variable Structure-Part III: Model-Group Switching Algorithm,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 35, No. 1, 1999, pp. 225–241. doi:https://doi.org/10.1109/7.745694 IEARAX 0018-9251 CrossrefGoogle Scholar[17] Shtessel Y. B., Moreno J. A., Plestan F. and Poznyak A. S., “Super-Twisting Adaptive Sliding Mode Control: A Lyapunov Design,” 49th IEEE Conference on Decision and Control, IEEE Publ., Piscataway, NJ, Dec. 2010, pp. 5109–5113. doi:https://doi.org/10.1109/CDC.2010.5717908 Google Scholar[18] Levant A., “Sliding Order and Sliding Accuracy in Sliding Mode Control,” International Journal of Control, Vol. 58, No. 6, 1993, pp. 1247–1263. doi:https://doi.org/10.1080/00207179308923053 IJCOAZ 0020-7179 CrossrefGoogle Scholar[19] Zhou D., Sun S. and Teo K. L., “Guidance Laws with Finite Time Convergence,” Journal of Guidance, Control, and Dynamics, Vol. 32, No. 6, 2009, pp. 1838–1846. doi:https://doi.org/10.2514/1.42976 JGCODS 0731-5090 LinkGoogle Scholar Previous article FiguresReferencesRelatedDetailsCited byQuick identification of guidance law for an incoming missile using multiple-model mechanismChinese Journal of Aeronautics, Vol. 35, No. 9Pursuit-evasion game switching strategies for spacecraft with incomplete-informationAerospace Science and Technology, Vol. 119A Novel Recurrent Convolutional Neural Network-Based Estimation Method for Switching Guidance LawIEEE Access, Vol. 8Collaborative Estimation of State and Guidance Parameter for Interceptor Based on Variational Bayesian TechniqueIEEE Access, Vol. 8 What's Popular Volume 41, Number 11November 2018 CrossmarkInformationCopyright © 2018 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 ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAir-to-Air MissileControl SystemsControl TheoryGuidance, Navigation, and Control SystemsGuided MissilesKalman FilterMissile Guidance and ControlMissile Systems, Dynamics and TechnologyMissilesNavigational GuidanceOptimal Control Theory KeywordsGuidance SystemUnscented Kalman FilterLinear Time Invariant SystemCumulative Distribution FunctionFlight Path AngleProportional NavigationAir to Air MissilesMonte Carlo SimulationOptimal ControlSingle Input Single OutputAcknowledgmentsThis work is supported by the National Natural Science Foundation of China (grant nos. 61773142 and 61471023). The authors would like to thank X. R. Li, Huimin Chen, and especially the three anonymous reviewers for their many useful suggestions that substantially improved the quality of this Note.PDF Received7 October 2017Accepted25 June 2018Published online2 September 2018" @default.
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