旋翼状态反馈在直升机飞行控制中的鲁棒性和容错性

2014 IEEE Conference on Control Applications (CCA) Pub Date : 2014-12-11 DOI:10.1109/CCA.2014.6981387

S. Panza, M. Lovera

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引用次数: 14

摘要

考虑旋翼状态反馈的直升机飞控律设计，提出了一种既能保证稳定性又能保证性能鲁棒性的结构化H∞控制方法。该框架还包括对转子状态传感器故障的容错。给出了仿真结果，并与文献结果进行了比较。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Rotor state feedback in helicopter flight control: Robustness and fault tolerance

Helicopter flight control law design including rotor state feedback is considered and an approach based on structured H∞ control, capable of guaranteeing stability and performance robustness, is proposed. The framework also encompasses fault tolerance with respect to failures of the rotor state sensors. Simulation results comparing the proposed approach to results from the literature are presented and discussed.

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2014 IEEE Conference on Control Applications (CCA)

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