飞行控制,非线性控制,鲁棒自适应控制,高超声速飞行器," /> 飞行控制,非线性控制,鲁棒自适应控制,高超声速飞行器,"/> flight control,nonlinear system control,robust adaptive control,hypersonic vehicle,"/> <span style="font-size:10.5pt;font-family:宋体;">Robust Adaptive Control for Near Space Vehicle Based on Trajectory Linearization Method</span><span style="font-size:medium;"></span>

Aerospace Contrd and Application ›› 2008, Vol. 34 ›› Issue (1): 38-43.

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Robust Adaptive Control for Near Space Vehicle Based on Trajectory Linearization Method

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  1. Institute of Aerospace Science&Technology,Shanghai Jiao Tong University,Shanghai 200240,China
  • Online:2008-02-25 Published:2021-12-11

Abstract: A robust adaptive flight control scheme is presented for a near—space vehicle(NSV)A novel estimator design technique called the single Hidden layer neural network disturbance observer(SDO)is developedThe SDO utilizes both the universal approximation property of neural networkand more useful information on the controlled systemA new robust adaptive control algorithm is proposed by Integrating the existing trajectory linearization control(TLC)method with the SD0 techniqueConditions are derived which guarantee ultimate boundedness of all the errors in the closed--loop systemFinallythe flight control system of the NSV is implemented by using the proposed methodExcellent disturbance attenuation ability and strong robustness of the Proposed method are demonstrated

Key words: font-family:宋体, flight control">flight controlfont-family:宋体, ')">">, nonlinear system control, robust adaptive control, hypersonic vehicle')">">

CLC Number: 

  • TPl83