DOB-Based Neural Control of Flexible Hypersonic Flight Vehicle Considering Wind Effects

This paper investigates the disturbance observer (DOB)-based neural adaptive control on the longitudinal dynamics of a flexible hypersonic flight vehicle (HFV) in the presence of wind effects. The coupling effect between flexible states and rigid body, and the accessional angle of attack (AOA) due t...

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Veröffentlicht in:	IEEE transactions on industrial electronics (1982) 2017-11, Vol.64 (11), p.8676-8685
Hauptverfasser:	Xu, Bin, Wang, Danwei, Zhang, Youmin, Shi, Zhongke
Format:	Artikel
Sprache:	eng
Schlagworte:	Accessional attack angle Adaptation models Adaptive control Aerodynamics Angle of attack Approximation Artificial neural networks Compounds Computer simulation Control systems design disturbance observer (DOB) Disturbance observers Electronic mail Estimation flexible hypersonic flight dynamics Flight vehicles Fuel consumption Hypersonic flight Mathematical analysis Neural networks neural networks (NNs) Rigid structures Uncertainty Weight wind effect Wind effects
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