Loop-Shaping Approach to Mitigate Radome Effects in Homing Missiles
2017; American Institute of Aeronautics and Astronautics; Volume: 40; Issue: 7 Linguagem: Inglês
10.2514/1.g000850
ISSN1533-3884
Autores Tópico(s)Military Defense Systems Analysis
ResumoNo AccessEngineering NoteLoop-Shaping Approach to Mitigate Radome Effects in Homing MissilesItzik Klein and Ilan RusnakItzik KleinRAFAEL-Advanced Defense Systems, Ltd., 3102102 Haifa, Israel and Ilan RusnakRAFAEL-Advanced Defense Systems, Ltd., 3102102 Haifa, IsraelPublished Online:28 Feb 2017https://doi.org/10.2514/1.G000850SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Lin C. F., "Modeling-Design-Analysis-Simulation-Evaluation (MDASE) of NGC Processing," Modern Navigation Guidance and Control Processing, Prentice–Hall Series in Advanced Navigation, Guidance and Control and Their Applications, Prentice–Hall, Upper Saddle River, NJ, 1991, Chap. 2. Google Scholar[2] Siouris C. F., "Aerodynamic Forces and Coefficients," Missile Guidance and Control Systems, Springer–Verlag, New York, 2004, Chap. 3. Google Scholar[3] Zarchan P., "Proportional Navigation and Miss Distance," Tactical and Strategic Missile Guidance, AIAA, Reston, VA, 2012, Chap. 6. LinkGoogle Scholar[4] Nesline F. W. and Zarchan P., "Radome Induced Miss Distance in Aerodynamically Controlled Homing Missiles," AIAA Guidance and Control Conference, AIAA Paper 1984-1845, 1984. doi:https://doi.org/10.2514/6.1984-1845 LinkGoogle Scholar[5] Nesline F. W. and Zarchan P., "A New Look at Classical Versus Modern Homing Missile Guidance," Journal of Guidance, Control, and Dynamics, Vol. 4, No. 1, 1981, pp. 78–85. doi:https://doi.org/10.2514/3.56054 JGCODS 0162-3192 LinkGoogle Scholar[6] Dowling T., Lewis L. R. and Chinchillo A. R., "Radome Computer Compensation," Antennas and Propagation Society International Symposium, IEEE, Piscataway, NJ, 1979, pp. 602–605. doi:https://doi.org/10.1109/aps.1979.1148090 Google Scholar[7] Das R., "Advances in Active Radar Seeker Technology," Defense Science Journal, Vol. 55, No. 3, 2005, pp. 329–336. doi:https://doi.org/10.14429/dsj.55.1996 CrossrefGoogle Scholar[8] Nesline F. W. and Zarchan P., "Missile Guidance for Low Altitude Air Defense," Journal of Guidance, Control, and Dynamics, Vol. 2, No. 4, 1979, pp. 283–289. doi:https://doi.org/10.2514/3.55876 JGCODS 0162-3192 LinkGoogle Scholar[9] Yueh W. R. and Lin C. F., "Guidance Performance Analysis with In-Flight Radome Error Compensation," Journal of Guidance, Control, and Dynamics, Vol. 8, No. 5, 1985, pp. 666–669. doi:https://doi.org/10.2514/3.20039 LinkGoogle Scholar[10] Lin J. M. and Chau Y. F., "Radome Slope Compensation Using Multiple-Model Kalman Filters," Journal of Guidance, Control, and Dynamics, Vol. 18, No. 3, 1995, pp. 637–640. doi:https://doi.org/10.2514/3.21438 LinkGoogle Scholar[11] Han S. S., Jang S. K. and Lee S. J., "Radome Compensation Using Adaptive Particle Filter," IFAC Proceedings Volumes, IFAC, Vol. 40, No. 7, 2007, pp. 43–48. doi:https://doi.org/10.3182/20070625-5-fr-2916.00009 Google Scholar[12] Han S. K., Ahn S., Ra W. S. and Park J. B., "Missile Radome Error Compensation Using Modified Interacting Multiple Model Kalman Filter," International Conference on Control, Automation and Systems (ICCAS), IEEE, Piscataway, NJ, 2014, pp. 391–395. doi:https://doi.org/10.1109/iccas.2014.6988028 Google Scholar[13] Lin C. H., "Stability Analysis of Radome Error and Calibration Using Neural Networks," IEEE Transactions on Aerospace and Electronic Systems, Vol. 37, No. 4, 2001, pp. 1442–1450. doi:https://doi.org/10.1109/7.976979 IEARAX 0018-9251 CrossrefGoogle Scholar[14] Willman W., "Radome Compensation Using Adaptive Dither," AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA Paper 1998-4415, 1998. doi:https://doi.org/10.2514/6.1998-4415 LinkGoogle Scholar[15] Zarchan P. and Gratt H., "Adaptive Radome Compensation Using Dither," Journal of Guidance, Control, and Dynamics, Vol. 22, No. 1, 1999, pp. 51–57. doi:https://doi.org/10.2514/2.4370 LinkGoogle Scholar[16] Gurfil P. and Kasdin J., "Improving Missile Guidance Performance by In Flight Two-Step Nonlinear Estimation of Radome Aberration," AIAA Guidance and Control Conference, AIAA Paper 2003-5723, 2003. doi:https://doi.org/10.2514/6.2003-5723 LinkGoogle Scholar[17] Song L. T. and Shin J. S., "Active Homing Performance Enhancement with Multiple Model Radome Slope Estimation," AIAA Guidance and Control Conference, AIAA Paper 2004-4899, 2004. doi:https://doi.org/10.2514/6.2004-4899 LinkGoogle Scholar[18] Gurfil P., Jodorkovsky M. and Guelman M., "Neoclassical Guidance for Homing Missiles," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 3, 2001, pp. 452–459. doi:https://doi.org/10.2514/2.4765 LinkGoogle Scholar[19] Baba Y., Inoue K. and Howe R. M., "Suboptimal Guidance with Line of Sight Rate Only Measurements," AIAA Guidance, Navigation and Control, AIAA Paper 1988-4066, 1988, pp. 122–129. doi:10.2514/6.1988-4066 LinkGoogle Scholar[20] Murray T., "Correlation of Linear and Nonlinear Radome Error Induced Miss Distance Predictions," American Control Conference, IEEE, Piscataway, NJ, 1984, pp. 743–750. Google Scholar[21] Nesline F. W. and Zarchan P., "Missile Guidance Design Tradeoffs for High Altitude Air Defence," Journal of Guidance, Control, and Dynamics, Vol. 6, No. 3, 1983, pp. 207–212. doi:https://doi.org/10.2514/3.19817 LinkGoogle Scholar[22] Mohler R. R., "Nonlinear Stability Time Domain Analysis," Nonlinear Systems, Vol. I, Dynamics and Control, Prentice–Hall, Upper Saddle River, NJ, 1991, Chap. 7. Google Scholar[23] Kahlil H. K., "Fundamental Properties," Nonlinear Systems, Prentice–Hall, Upper Saddle River, NJ, 1996, Chap. 3. Google Scholar[24] Franklin G. F., Powell J. D. and Emami-Naeini A., "Root-Locus Design Method," Feedback Control of Dynamic Systems, Pearson Education Ltd., London, 2015, Chap. 5. Google Scholar[25] Ogata K., "Transient and Steady-State Response Analysis," Modern Control Engineering, Prentice–Hall, Upper Saddle River, NJ, 2010, Chap. 7. 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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. TopicsAntennasArtificial Neural NetworkAvionics ComputersCommunication SystemCommunication Technology and EquipmentComputing SystemComputing and InformaticsComputing, Information, and CommunicationGuidance, Navigation, and Control SystemsMissile Guidance and ControlMissile Systems, Dynamics and TechnologyMissilesNavigational GuidanceSignal ProcessingTracking and Positioning Systems KeywordsRadomesHoming MissileClosed Loop Transfer FunctionGuidance SystemPower Spectral DensityProportional NavigationFlight Path AngleAerodynamic PropertiesInteracting Multiple ModelFlight Control SystemPDF Received28 August 2016Accepted13 December 2016Published online28 February 2017
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