Suppression of Helicopter's Disturbances in a Hovering Flight by Static Output Feedback

O. D. Gorbatyuk; V. B. Larin; A. A. Tunik

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Suppression of Helicopter's Disturbances in a Hovering Flight by Static Output Feedback

机译：通过静态输出反馈抑制悬停飞行中的直升机干扰

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The problem of stabilizing the helicopter in a hovering flight when subjected to external atmospheric disturbances, taking into account the influence of the dynamics of the actuators and incorporation of accelerometers in the measurement unit of the control system. The suppression of external disturbances is carried out by the static feedback by output variables, which is synthesized by the method of linear matrix inequalities. The results of the synthesis are estimated both analytically and by simulation.

机译：考虑到执行器动力学的影响以及在控制系统的测量单元中并入了加速度计，在受到外部大气干扰时稳定直升机在悬停飞行中的问题。外部干扰的抑制是通过输出变量的静态反馈来实现的，该变量通过线性矩阵不等式的方法进行合成。合成的结果可以通过分析和仿真来估计。

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来源
《Journal of automation and information sciences》 |2009年第5期|29-40|共12页
作者
O. D. Gorbatyuk; V. B. Larin; A. A. Tunik;
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作者单位

Control Systems Institute of National Aviation University, Kiev;

Department of S.P. Timoshenko Institute of Mechanics of National Academy of Sciences of Ukraine, Kiev;

National Aviation University, Kiev;

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收录信息美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类
关键词
stabilizing the helicopter in a hovering flight; atmospheric disturbances; suppression; static feedback by output variables; method of linear matrix inequalities;

机译：在盘旋飞行中稳定直升机;大气干扰;抑制;输出变量的静态反馈;线性矩阵不等式的方法;

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4. FLIGHT STABILIZATION AND EXOGENOUS UNCERTAIN DISTURBANCE SUPPRESSION VIA STATIC AND DYNAMIC OUTPUT FEEDBACK [C] . V.B.Larin, A.A.Tunik Saint Petersburg International Conference on Integrated Navigation Systems . 2006

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5. Disturbance decoupling with stability for nonlinear systems using static/output feedback: A geometric approach. [D] . Elshihabi, Azzam M. 1998

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6. Sequential and Automatic Image-Sequence Registration of Road Areas Monitored from a Hovering Helicopter [O] . Fatemeh Karimi. Nejadasl, Roderik. Lindenbergh 2014

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7. Disturbance decoupling of multi-input multi-output discrete-time nonlinear systems by static measurement feedback [O] . A Kaldmäe, Ü Kotta 2012

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8. Extensions to PIFCGT: Multirate Output Feedback and Optimal Disturbance Suppression [R] . Broussard, J. R. 1986

机译：pIFCGT的扩展：多速率输出反馈和最佳干扰抑制

Suppression of Helicopter's Disturbances in a Hovering Flight by Static Output Feedback

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