Добірка наукової літератури з теми "Singular Perturbation based guidance design"
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Статті в журналах з теми "Singular Perturbation based guidance design"
Manickavasagam, M., A. K. Sarkar, and V. Vaithiyanathan. "A Singular Perturbation Based Midcourse Guidance Law for Realistic Air-to-Air Engagement." Defence Science Journal 67, no. 1 (December 23, 2016): 108. http://dx.doi.org/10.14429/dsj.1.9236.
Повний текст джерелаYefei, Yin, Li Xu, and Li Qiaoqi. "Design of Guidance Law for Smart Missile Based on Direct Mode Configuration with Implicit Dynamic-Inverse." Journal of Physics: Conference Series 2478, no. 11 (June 1, 2023): 112036. http://dx.doi.org/10.1088/1742-6596/2478/11/112036.
Повний текст джерелаZhao, Penglei, Wanchun Chen, and Wenbin Yu. "Optimal perturbation guidance with constraints on terminal flight-path angle and angle of attack." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 12 (January 13, 2019): 4436–46. http://dx.doi.org/10.1177/0954410018823472.
Повний текст джерелаFan, Yunsheng, Bowen Liu, Guofeng Wang, and Dongdong Mu. "Adaptive Fast Non-Singular Terminal Sliding Mode Path Following Control for an Underactuated Unmanned Surface Vehicle with Uncertainties and Unknown Disturbances." Sensors 21, no. 22 (November 10, 2021): 7454. http://dx.doi.org/10.3390/s21227454.
Повний текст джерелаHa, Cheol-Keun, and Hyoung-Sik Choi. "Design of Autolanding Guidance and Control Algorithm Using Singular Perturbation." Journal of Control, Automation and Systems Engineering 11, no. 8 (August 1, 2005): 726–32. http://dx.doi.org/10.5302/j.icros.2005.11.8.726.
Повний текст джерелаAnnam, Chandrakanth, Ashwini Ratnoo, and Debasish Ghose. "Singular-Perturbation-Based Guidance of Pulse Motor Interceptors with Look Angle Constraints." Journal of Guidance, Control, and Dynamics 44, no. 7 (July 2021): 1356–70. http://dx.doi.org/10.2514/1.g005508.
Повний текст джерелаLandolsi, F., and F. H. Ghorbel. "Design and singular perturbation control of a piezotube-based nanomanipulator." Nonlinear Dynamics 83, no. 1-2 (September 8, 2015): 971–81. http://dx.doi.org/10.1007/s11071-015-2381-x.
Повний текст джерелаSong, Seong Ho, Chang Seop Kim, and Jeom Keun Kim. "Stability Analysis of Internal Model Based Gain Control System for Three-Level EDFA Model." Applied Mechanics and Materials 339 (July 2013): 33–37. http://dx.doi.org/10.4028/www.scientific.net/amm.339.33.
Повний текст джерелаWardi, Mohamed Lazhar, Messaoud Amairi, and Mohamed Naceur Abdelkrim. "Fractional PID controller design for nonlinear systems based on singular perturbation technique." International Journal of Digital Signals and Smart Systems 2, no. 2 (2018): 95. http://dx.doi.org/10.1504/ijdsss.2018.093172.
Повний текст джерелаWardi, Mohamed Lazhar, Mohamed Naceur Abdelkrim, and Messaoud Amairi. "Fractional PID controller design for nonlinear systems based on singular perturbation technique." International Journal of Digital Signals and Smart Systems 2, no. 2 (2018): 95. http://dx.doi.org/10.1504/ijdsss.2018.10014373.
Повний текст джерелаДисертації з теми "Singular Perturbation based guidance design"
Wu, Chia-Pin, and 吳佳斌. "Using Singular Perturbation Methods in Observer-based Controller Design." Thesis, 2012. http://ndltd.ncl.edu.tw/handle/88637893484414157491.
Повний текст джерела國立臺灣科技大學
電機工程系
100
The thesis is mainly to design the controller by applying the theory of singular perturbation. First of all, using the singular perturbation technique to design the output feedback controller of mechanic systems, it is similar to the design of a proportional-derivative control law. We can precede the speed control by only measuring the displacement. The controller algorithm is the rule of low-order dynamic output feedback control. It is simple and easily accomplished. Besides, when the mechanical system contains uncertain items, this thesis presents robust stability of the closed-loop system. It also offers the analysis of Lyapunov theory by solving a Riccati algebra equation and a linear matrix inequality. Furthermore, for the mismatched parameter uncertainties and matched nonlinear perturbations in a linear MIMO system, the thesis proposes a disturbance-observer based controller in which the input disturbance can be effectively estimated by using a high-gain integration observer. Finally, it is verified the practicability by numerical examples.
Chang, Yuan-Jen, and 張元震. "Application of the Singular Perturbation Method in the Design of Real-Time Guidance Law for an Air-to-Surface Missile." Thesis, 1998. http://ndltd.ncl.edu.tw/handle/66639207625545361372.
Повний текст джерела國立成功大學
航空太空工程學系
86
How a missile flying along the optimal trajectory which leads to a hit to a target in the minimum time is a major topic for the investigation of the design of guidance law. This is essentially a two-point boundary value problem. In the past, however, the optimal trajectories obtained by using the rigorous optimal control theory associated with the gradient method for numerical computations are too difficult to be implemented as the procedure of computation is so complicated that the iterations often do not converge. The purpose of this thesis is to investigate a real-time guidance law by using the singular perturbation method(SPM). As a result, the trajectory of the missile is near optimal but not rigorously optimal. In the beginning, the altitude is much lower than the optimal value, the guidance law derived by using the SPM is employed. When the missile climbs to the near optimal altitude, the guidance law derived by using the classical control theory is used to accomplish the mission. According to the results of computer simulations, the guidance law designed can indeed guide the missile to fly a near optimal trajectory which characterize the essential part of the rigorous optimal trajectory, and is, therefore, very practical.
Тези доповідей конференцій з теми "Singular Perturbation based guidance design"
Zheng, Tianyu, Fenghua He, Yu Yao, Hongsheng Qi, and Xiaoming Hu. "A singular perturbation-based design for the integrated guidance and control." In 2016 American Control Conference (ACC). IEEE, 2016. http://dx.doi.org/10.1109/acc.2016.7525596.
Повний текст джерелаChen, Yuanyan, and J. Jim Zhu. "Car-Like Ground Vehicle Trajectory Tracking by Using Trajectory Linearization Control." In ASME 2017 Dynamic Systems and Control Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/dscc2017-5372.
Повний текст джерелаYOO, S., and T. BULLOCK. "Missile guidance based on weight adjusted singular perturbation." In Guidance, Navigation and Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-3482.
Повний текст джерелаPark, S., and G. Nagati. "Singular perturbation method in the design of decoupling flight control systems with output feedback." In Guidance, Navigation, and Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-3261.
Повний текст джерелаZhu, J., Brad Banker, and Charles Hall. "X-33 ascent flight control design by trajectory linearization - A singular perturbation approach." In AIAA Guidance, Navigation, and Control Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-4159.
Повний текст джерелаSMITH, P., D. HOPPER, and A. BRADSHAW. "Comparison of eigenstructure assignment and the Salford singular perturbation methods in VSTOL aircraft control law design." In Guidance, Navigation and Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-3451.
Повний текст джерелаXiao, Jiaping, and Zuojun Shen. "Stability analysis of Trajectory Tracking Entry Guidance based on singular perturbation theory." In 2016 35th Chinese Control Conference (CCC). IEEE, 2016. http://dx.doi.org/10.1109/chicc.2016.7553323.
Повний текст джерелаManhartsgruber, Bernhard. "Singular Perturbation Analysis of an Electrohydraulic Servo-Drive With Discontinuous Reduced Dynamics." In ASME 1999 Design Engineering Technical Conferences. American Society of Mechanical Engineers, 1999. http://dx.doi.org/10.1115/detc99/vib-8178.
Повний текст джерелаFakharian, A., F. Jamshidi, and M. Taghi Hamidi Beheshti. "Logic based switching H2/H∞ controller design for linear singular perturbation systems: A fuzzy supervisor approach." In 2010 8th IEEE International Conference on Control and Automation (ICCA 2010). IEEE, 2010. http://dx.doi.org/10.1109/icca.2010.5524299.
Повний текст джерелаAksenov, Efim A., and Valery D. Yurkevich. "Control system design based on sliding mode control and singular perturbation technique for a Cuk converter." In 2016 13th International Scientific-Technical Conference on Actual Problems of Electronics Instrument Engineering (APEIE). IEEE, 2016. http://dx.doi.org/10.1109/apeie.2016.7806933.
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