首页> 外文期刊>Journal of the Aeronautical Society of India >ROLL STABILISATION OF A FLEXIBLE SPACECRAFT USING QUANTITATIVE FEEDBACK THEORY
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ROLL STABILISATION OF A FLEXIBLE SPACECRAFT USING QUANTITATIVE FEEDBACK THEORY

机译:基于定量反馈理论的柔性桨叶的轧制稳定

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Quantitative Feedback Theory (QFT) has achieved the status as a powerful design technique for the achievement of assigned performance over the specified range of plant uncertainties. This is due to the relative simple algebra and the transparency of the design methodology. A QFT solution to a Single Input Single Output (SISO) problem of roll stabilization of a flexible satellite is presented in this paper. A simple controller is designed which ensures robustness against parameter variations and disturbances. The results of the study are compared with those obtained using an H_∞ controller.
机译:定量反馈理论(QFT)已成为一种强大的设计技术,可在指定的工厂不确定性范围内实现指定的性能。这是由于相对简单的代数和设计方法的透明性。本文提出了一种针对柔性卫星侧倾稳定的单输入单输出(SISO)问题的QFT解决方案。设计了一种简单的控制器,可确保其对参数变化和干扰的鲁棒性。将研究结果与使用H_∞控制器获得的结果进行比较。

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