2006 1st International Symposium on Systems and Control in Aerospace and Astronautics
DOI: 10.1109/isscaa.2006.1627502
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Flexible Satellite Attitude Maneuver Control Using Pulse-Width Pulse-Frequency Modulated Input Shaper

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(1 citation statement)
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“…Staehlin designed closed-loop delay filter to eliminate residual vibration of flexible systems [4]. Yuan designed feedforward compensator and PD controller to suppress the vibration of large flexible structural parts, and the simulation results proved that this control strategy has strong robustness for the system parameter uncertainty and the impulsive delay is optimal [5]. Zhongyi Chu used linear servo motor as the robot main driver, to achieve high-speed accurate position control and delay filtering techniques to reduce residual vibration on the end of the mechanical [6].…”
Section: Introductionmentioning
confidence: 99%
“…Staehlin designed closed-loop delay filter to eliminate residual vibration of flexible systems [4]. Yuan designed feedforward compensator and PD controller to suppress the vibration of large flexible structural parts, and the simulation results proved that this control strategy has strong robustness for the system parameter uncertainty and the impulsive delay is optimal [5]. Zhongyi Chu used linear servo motor as the robot main driver, to achieve high-speed accurate position control and delay filtering techniques to reduce residual vibration on the end of the mechanical [6].…”
Section: Introductionmentioning
confidence: 99%