2017
DOI: 10.1155/2017/6034786
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A Novel SHLNN Based Robust Control and Tracking Method for Hypersonic Vehicle under Parameter Uncertainty

Abstract: Hypersonic vehicle is a typical parameter uncertain system with significant characteristics of strong coupling, nonlinearity, and external disturbance. In this paper, a combined system modeling approach is proposed to approximate the actual vehicle system. The state feedback control strategy is adopted based on the robust guaranteed cost control (RGCC) theory, where the Lyapunov function is applied to get control law for nonlinear system and the problem is transformed into a feasible solution by linear matrix … Show more

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Cited by 4 publications
(4 citation statements)
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“…NN is a simple abstraction of biological NN that stores function in the neurons and in the connections between them [50]. It learns to perform useful functions by training on data.…”
Section: B Neural Networkmentioning
confidence: 99%
“…NN is a simple abstraction of biological NN that stores function in the neurons and in the connections between them [50]. It learns to perform useful functions by training on data.…”
Section: B Neural Networkmentioning
confidence: 99%
“…where k b2 is a positive constant. Differentiating equation (14) and according to equation 7, we have…”
Section: Control Of the Pitch Channelmentioning
confidence: 99%
“…Meanwhile, the intelligence-based control method has become an active research topic. In the literature, 14,15 the main idea is to use a fuzzy logic system FLS/NN for nonlinearity approximation, which can provide the feedback information. In this way, the controller design can be simplified since the nonlinearity is not required to be known exactly.…”
Section: Introductionmentioning
confidence: 99%
“…To this end, a comprehensive analytical model of waverider was developed in [3] using Newtonian impact theory to estimate the pressures that act on the vehicle. Based on the integration of computational fluid dynamics (CFD) and analytical techniques, the stability and control derivatives were determined in [4] to build a model of the longitudinal dynamics of the waverider and investigate the propulsion/airframe integration. A first principlebased dynamic model of the waverider was provided in [5] to incorporate aero-thermo-elastic-propulsion interactions: this model applied inviscid compressible oblique shock-expansion theory to estimate aerodynamic forces and moments, as well as a 1D Rayleigh flow model and an Euler-Bernoulli beam model determined scramjet propulsion and structural flexibility, respectively.…”
Section: Introductionmentioning
confidence: 99%