FLIGHT/THRUST INTEGRATED CONTROL USINGH∞SYNTHESIS IN AUTOMATIC CARRIER LANDING |
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作者姓名: | YuYong YangYidong DaiShijun |
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作者单位: | CollegelfAutomationEngineering,NUAA29YudaoStreet,Nanjing210016,P.R.China |
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摘 要: | The landing task of an aircraft under low aerodynamic pressure on carrier requires precise airplane control,A flight/thrust integrated control system(FTICS)with constant ad,actual angle of attack,is developed using LMI-based H∞synthesis.The typical single input/outputspecifications are translated into the weighting functions of an H∞output-feedback synthesis problem.The motiva-tion of the work is to improve the key performance of dy-namic tracking and air disturbance attenuation.The FTICS can keep the attitude andgle and the path angle un-changeable as the airplane is passing through the ramp at which the tracking radar doesnot work and the guidance signal is terminated.For engineering application,an or-der-reduction method of the H∞controller is also pro-posed,Simulational results indicate that the system satis-fies the design requirements quite well.
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关 键 词: | flight/thrust integrated control H∞synthe-sis linear matrix inequality flight control system carrier-based aircraft 飞行控制 鲁棒控制 自动驾驶着陆系统 线性矩阵不等式 舰载飞机 推力控制 设计 |
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