Nonlinear Fault-Tolerant Control for Hypersonic Flight Vehicle With Multi-Sensor Faults

This paper presents a nonlinear fault-tolerant control (FTC) and sensor fault diagnosis for longitudinal dynamics of hypersonic flight vehicle. A nominal sliding mode control is developed to track the reference command of velocity and altitude on the basis of an affine nonlinear dynamic model. A non...

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Veröffentlicht in:	IEEE access 2018-01, Vol.6, p.25427-25436
Hauptverfasser:	Chen, Fuyang, Niu, Juan, Jiang, Gengqian
Format:	Artikel
Sprache:	eng
Schlagworte:	Adaptive systems Aerodynamics Altitude backstepping Control stability Controllers Dynamic models Dynamical systems Fault diagnosis Fault tolerance Fault tolerant systems Flight vehicles Hypersonic flight hypersonic flight vehicle Multi-sensor faults Nonlinear control Nonlinear dynamics Observers Robust control Rocket launches Sensors Sliding mode control Stability analysis Vehicle dynamics
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