Robust Guidance Law via Integral-Sliding-Mode Scheme

Abstract

No AccessEngineering NoteRobust Guidance Law via Integral-Sliding-Mode SchemeYew-Wen Liang, Chih-Chiang Chen, Der-Cherng Liaw, Yang-Ching Feng, Chiz-Chung Cheng and Chun-Hone ChenYew-Wen LiangInstitute of Electrical Control Engineering, National Chiao Tung University, Hsinchu 300, Taiwan, Republic of China, Chih-Chiang ChenInstitute of Electrical Control Engineering, National Chiao Tung University, Hsinchu 300, Taiwan, Republic of China, Der-Cherng LiawInstitute of Electrical Control Engineering, National Chiao Tung University, Hsinchu 300, Taiwan, Republic of China, Yang-Ching FengInstitute of Electrical Control Engineering, National Chiao Tung University, Hsinchu 300, Taiwan, Republic of China, Chiz-Chung ChengDepartment of Electrical Engineering, Lee-Ming Institute of Technology, Taipei 243, Taiwan, Republic of China and Chun-Hone ChenChung-Shan Institute of Science and Technology, Taoyuan 325, Taiwan, Republic of ChinaPublished Online:25 Apr 2014https://doi.org/10.2514/1.60669SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Yuan P. J. and Chern J. S., "Ideal Proportional Navigation," Journal of Guidance, Control, and Dynamics, Vol. 15, No. 5, 1992, pp. 1161–1165. doi:https://doi.org/10.2514/3.20964 JGCDDT 0162-3192 LinkGoogle Scholar[2] Yang C.-D. and Yang C.-C., "Analytical Solution of Three-Dimensional Realistic True Proportional Navigation," Journal of Guidance, Control, and Dynamics, Vol. 19, No. 3, 1996, pp. 569–577. doi:https://doi.org/10.2514/3.21659 JGCDDT 0162-3192 LinkGoogle Scholar[3] Palumbo N. F., Blauwkamp R. A. and Lloyd J. M., "Modern Homing Missile Guidance Theory and Techniques," Johns Hopkins APL Technical Digest, Vol. 29, No. 1, 2010, pp. 42–59. JHADDQ 0270-5214 Google Scholar[4] Zarchan P., Tactical and Strategic Missile Guidance, 5th ed., AIAA, Reston, VA, 2007, pp. 95–118. Google Scholar[5] Liaw D.-C., Liang Y.-W. and Cheng C.-C., "Nonlinear Control for Missile Terminal Guidance," Journal of Dynamic Systems, Measurement, and Control, Vol. 122, No. 4, 2000, pp. 663–668. doi:https://doi.org/10.1115/1.1316796 JDSMAA 0022-0434 CrossrefGoogle Scholar[6] Brierley S. D. and Longchamp R., "Application of Sliding-Mode Control to Air–Air Interception Problem," IEEE Transactions on Aerospace and Electronic Systems, Vol. 26, No. 2, 1990, pp. 306–325. doi:https://doi.org/10.1109/7.53460 IEARAX 0018-9251 CrossrefGoogle Scholar[7] Zhou C., Zhang Y.-A. and Duan G.-R., "Multiple Model Adaptive Two-Step Filter and Motion Tracking Sliding-Mode Guidance for Missiles with Time Lag in Acceleration," Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 47, No. 156, 2005, pp. 81–89. doi:https://doi.org/10.2322/tjsass.47.81 TJASAM 0549-3811 CrossrefGoogle Scholar[8] Ratnoo A. and Ghose D., "State-Dependent Riccati-Equation-Based Guidance Law for Impact-Angle-Constrained Trajectories," Journal of Guidance, Control, and Dynamics, Vol. 32, No. 1, 2009, pp. 320–326. doi:https://doi.org/10.2514/1.37876 JGCDDT 0162-3192 LinkGoogle Scholar[9] Khalil H. K., Nonlinear Systems, 3rd ed., Pearson Education, Upper Saddle River, NJ, 2000, pp. 552–575. Google Scholar[10] Liang Y.-W., Ting L.-W. and Lin L.-G., "Study of Reliable Control via an Integral-Type Sliding Mode Control Scheme," IEEE Transactions on Industrial Electronics, Vol. 59, No. 8, 2012, pp. 3062–3068. doi:https://doi.org/10.1109/TIE.2011.2162211 ITIED6 0278-0046 CrossrefGoogle Scholar[11] Castanos F. and Fridman L., "Analysis and Design of Integral Sliding Manifolds for System with Unmatched Perturbations," IEEE Transactions on Automatic Control, Vol. 51, No. 5, 2006, pp. 853–858. doi:https://doi.org/10.1109/TAC.2006.875008 IETAA9 0018-9286 CrossrefGoogle Scholar Previous article Next article