小型直升机自主软着陆的时变LQ控制

2009 International Conference on Information and Automation Pub Date : 2009-06-22 DOI:10.1109/ICINFA.2009.5204925

X. Xia, Min Zhu, Xiaotao Zhang, Y. Ge

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引用次数: 0

摘要

本文研究了微型直升机的软着陆问题，并针对典型的软着陆问题，提出了一种具有适当设计参数的优化策略。对微型直升机自主软着陆的时变增益和时变二次性能指标LQ控制进行了仿真研究。仿真结果证明了所设计控制器的有效性。

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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Time-varying LQ control for autonomous soft landing of small-scale helicopter

This paper addresses soft landing of miniature helicopter issue and suggests an optimal strategy with appropriate design parameters for a typical soft landing. The time-varying gains and time-varying quadratic performance index LQ control for autonomous soft landing of miniature helicopter examines and simulate. Simulation results have proved that the designed controller is suitable.

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来源期刊

2009 International Conference on Information and Automation

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