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An efficient method to control the amplitude of the limit cycle in satellite attitude control system | ||
| AUT Journal of Modeling and Simulation | ||
| مقاله 2، دوره 48، شماره 1، شهریور 2016، صفحه 13-27 اصل مقاله (1.1 M) | ||
| نوع مقاله: Research Article | ||
| شناسه دیجیتال (DOI): 10.22060/miscj.2016.634 | ||
| نویسندگان | ||
| Mahdi Sabet Rasekh1؛ seyed kamaleddin yadavar nikravesh* 2؛ nematollah ghahramani3 | ||
| 1Electrical engineering faculty Amirkabir university of technology | ||
| 2Amirkabir University of technology | ||
| 3Malek Ashtar University of technology | ||
| چکیده | ||
| In this paper, an efficient method is presented to control the attitude of a satellite with ON-OFF actuator. The main objective of this novel method is to control the amplitude of the limit cycle which commonly appears in the steady state of such systems; and at the same time by consideration of real actuator constraints, reduce the fuel consumption of system. The Proposed method is a combination of a command modifier (which based on the set point and the required accuracy of pointing, by means of optimization, calculate the desired limit cycle), a phase plane controller (PPC) and a compensator (to compensate for the real constraints of the actuator). The effectiveness and outperformance of the proposed method is approved in comparison with the previous methods of attitude control problem through the closed loop simulation and the stability and robustness of the closed loop system is fully analyzed and illustrated by simulations. | ||
| کلیدواژه‌ها | ||
| Limit Cycle؛ On/Off Actuator؛ Phase Plane Controller؛ Attitude control؛ Robustness | ||
| عنوان مقاله [English] | ||
| An efficient method to control the amplitude of the limit cycle in satellite attitude control system | ||
| نویسندگان [English] | ||
| Mahdi Sabet Rasekh1؛ seyed kamaleddin yadavar nikravesh2؛ nematollah ghahramani3 | ||
| 1Electrical engineering faculty Amirkabir university of technology | ||
| چکیده [English] | ||
| In this paper, an efficient method is presented to control the attitude of a satellite with ON-OFF actuator. The main objective of this method is to control the amplitude of the limit cycle which commonly appears in the steady state of such systems, while simultaneously by consideration of real actuator constraints, it reduces the fuel consumption of system. The proposed method is a combination of a command modifier (which is based on the set point and the required accuracy of pointing, by means of optimization, it calculates the desired limit cycle), a phase plane controller (PPC) and a compensator (to compensate for the real constraints of the actuator). The effectiveness and outperformance of the proposed method is approved in comparison with the previous methods of attitude control problem through the closed loop simulation and the stability and robustness of the closed loop system is fully analyzed and illustrated by simulations. | ||
| کلیدواژه‌ها [English] | ||
| Limit Cycle, On/Off Actuator, Phase Plane Controller, Attitude control, Robustness | ||
| مراجع | ||
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[1] H. Olsson and K. J. Astron, “Friction Generated Limit Cycles,” IEEE Transaction on Control Systems and Technology, Vol. 9, No. 4, 2001. [2] Y. J. Huang and Y. J. Wang, “Limit Cycle Analysis of Electro-Hydraulic Control Systems with Friction and Transport Delay,” in World Congress on Intelligent Control and Automation,2000. [3] M. Tanelli, et al, “Limit Cycles Analysis in Hybrid Anti-Lock Braking Systems,” in IEEE Conference on Decision and Control, 2007. [4] S. Adler, A. Warshavsky and A. Peretz, “Low-Cost Cold-Gas Reaction Control System For Slohsat FLEVO Small Satellite,” journal of Spacecraft Rocket, Vol.42, No.2, 2005. [5] Robert N. Clark, “Limit Cycle Oscillation in Pulse-Modulated Systems,” Journal of Spacecraft, Vol. 6, No. 7, 1969. [6] T. D. Krovel, “Optimal Tuning of PWPF Modulator for Attitude Control,” M.S. Thesis,Department of Engineering Cybernetics,Norwegian University of Science and Technology,2005. [7] Philip C. Calhoun and Eric M. Queen, “Entry Vehicle Control System Design for the Mars Smart Lander,” in AIAA Atmospheric Flight Mechanics Conference, Monterey, California, 2002. [8] Marcel J. Sidi, “Spacecraft Dynamics and Control,” Cambridge University Press,1997. [9] B. F. Wu and J. W. Perng, “Limit Cycle Analysis of PID Controller Design,” American Control Conference, 2003. [10] J. W. Perng, B. F. Wu, H. I. Chin, and T. T. Lee,“Limit Cycle Analysis of Uncertain Fuzzy Vehicle Control Systems,” in IEEE Conference on Networking, Sensing and Control, 2005. [11] J. Mendel, “On-Off Limit-Cycle Controllers for Reaction-Jet-Controlled Systems,” IEEE Transactions on Automatic Control, Vol. 15, No. 3,1970. [12] B. F.Wu, J.W. Perng, and J. I. Chin, “Limit Cycle Analysis of Nonlinear Sampled-Data Systems by Gain-Phase Margin Approach,” J. Franklin Inst.,Vol. 342, 2005. [13] C. C. Cheng and C. H. Huang, “On the Limit Cycle of The Underwater Vehicle Control System,” in Int. Symposium Underwater Technol., 1998. [14] V. E. Haloulakos, “Thrust and Impulse Requirements for Jet Attitude Control Systems,” J.Spacecraft, 1964. [15] M. H. Kaplan, “Modern Spacecraft Dynamics and Control,” Wiley press, New York, 1976. [16] H. B. Hablani, “Target Acquisition, Tracking,Spacecraft Attitude Control, and Vibration Suppression with IPFM Reaction Jet Controllers,”in AIAA Guidance, Navigation and Control Conference, 1992. [17] R.N. Clark, “Limit Cycle Oscillation in a Satellite Attitude Control System,” Automatica, Vol. 6,1970. [18] M. J. Abzug, el al., “A Time Optimal Attitude Control System Designed to Overcome Certain Sensor Imperfection,” Guidance and Control II,edited by R. Langford, Elsevier, 1964. [19] Sang W. Jeon and Seul Jung, “Hardware-in-the-Loop Simulation for The Reaction Control System Using PWM-Based Limit Cycle Analysis,” IEEE Transactions on Control Systems Technology, Vol. 20, No. 2, Mar. 2012. [20] A. R. Mesquita, K. H. Kienitz and E. L. Rempel,“Robust Limit Cycle Control in an Attitude Control System with Switching-Constrained Actuators,” in The 47th IEEE Conference on Decision and Control, Cancun, Mexico, Dec. 9-11,2008. [21] A. Mesquita, E. L. Rempel and K. H. Kienitz,“Bifurcation Analysis of Attitude Control Systems with Switching-Constrained Actuators,,” Springer,Vol. 51, Issue 1, pp. 207-216, 2008. | ||
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