Novel analysis of limit cycle for PWM signal of PD control system
Author:
Affiliation:
1. Control Dept., Korea Aerospace Research Institute
2. Mechatronics Dept., Chungnam National University
Publisher
Institute of Electronics, Information and Communications Engineers (IEICE)
Subject
Electrical and Electronic Engineering,Condensed Matter Physics,Electronic, Optical and Magnetic Materials
Link
http://www.jstage.jst.go.jp/article/elex/6/11/6_11_787/_pdf
Reference8 articles.
1. Multilevel PWM methods at low modulation indices
2. Nonlinear Model-Based Control of Pulse Width Modulated Pneumatic Servo Systems
3. [3] T. Ieko, Y. Ochi, K. Kanai, N. Hori, and P. N. Nikiforuk, “Design of a pulse-width-modulation spacecraft attitude control system via digital redesign, ” IFAC 14 Triennial World Congress, pp. 355-360, 1999.
4. [4] B.-F. Wu, J.-W. Perng, and H.-I. Chin, “Limit cycle analysis of nonlinear sampled-data system by gain-phase margin approach, ” Journal of the Franklin Institute, pp. 175-192, 2005.
5. [5] V. E. Haloulakos, “Thrust and impulse requirements for jet attitude-control systems, ” Journal of Spacecraft, pp. 84-90, 1964.
Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Hardware-in-the-Loop Simulation for the Reaction Control System Using PWM-Based Limit Cycle Analysis;IEEE Transactions on Control Systems Technology;2012-03
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