Lyapunov-Based Exponential Tracking Control of a Hypersonic Aircraft with Aerothermoelastic Effects

Z. D. Wilcox; W. MacKunis; S. Bhat; R. Lind; W. E. Dixon

doi:10.2514/1.46785

Lyapunov-Based Exponential Tracking Control of a Hypersonic Aircraft with Aerothermoelastic Effects

Z. D. Wilcox, W. MacKunis, S. Bhat, R. Lind, W. E. Dixon

Research output: Contribution to journal › Article › peer-review

Abstract

 Hypersonic flight conditions produce temperature variations that can alter both the structural dynamics and flight
 dynamics. These aerothermoelastic effects are modeled by a nonlinear, temperature-dependent, parameter-varying
 state-space representation. The model includes an uncertain parameter-varying state matrix, an uncertain
 parameter-varying nonsquare (column-deficient) input matrix, and a nonlinear additive bounded disturbance. A
 Lyapunov-based continuous robust controller is developed that yields exponential tracking of a reference model,
 despite the presence of bounded nonvanishing disturbances. Simulation results for a hypersonic aircraft are
 provided to demonstrate the robustness and efficacy of the proposed controller.

Original language	American English
Journal	Journal of Guidance, Control, and Dynamics
Volume	33
DOIs	https://doi.org/10.2514/1.46785
State	Published - Jul 2010
Externally published	Yes

Keywords

hypersonic flight control
aircraft structural dynamics
flight dynamics

Disciplines

Aerospace Engineering
Navigation, Guidance, Control and Dynamics
Aviation

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10.2514/1.46785License: Unspecified

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title = "Lyapunov-Based Exponential Tracking Control of a Hypersonic Aircraft with Aerothermoelastic Effects",

abstract = " Hypersonic flight conditions produce temperature variations that can alter both the structural dynamics and flight dynamics. These aerothermoelastic effects are modeled by a nonlinear, temperature-dependent, parameter-varying state-space representation. The model includes an uncertain parameter-varying state matrix, an uncertain parameter-varying nonsquare (column-deficient) input matrix, and a nonlinear additive bounded disturbance. A Lyapunov-based continuous robust controller is developed that yields exponential tracking of a reference model, despite the presence of bounded nonvanishing disturbances. Simulation results for a hypersonic aircraft are provided to demonstrate the robustness and efficacy of the proposed controller.",

keywords = "hypersonic flight control, aircraft structural dynamics, flight dynamics",

author = "Wilcox, {Z. D.} and W. MacKunis and S. Bhat and R. Lind and Dixon, {W. E.}",

year = "2010",

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doi = "10.2514/1.46785",

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AU - Wilcox, Z. D.

AU - MacKunis, W.

AU - Bhat, S.

AU - Lind, R.

AU - Dixon, W. E.

PY - 2010/7

Y1 - 2010/7

N2 - Hypersonic flight conditions produce temperature variations that can alter both the structural dynamics and flight dynamics. These aerothermoelastic effects are modeled by a nonlinear, temperature-dependent, parameter-varying state-space representation. The model includes an uncertain parameter-varying state matrix, an uncertain parameter-varying nonsquare (column-deficient) input matrix, and a nonlinear additive bounded disturbance. A Lyapunov-based continuous robust controller is developed that yields exponential tracking of a reference model, despite the presence of bounded nonvanishing disturbances. Simulation results for a hypersonic aircraft are provided to demonstrate the robustness and efficacy of the proposed controller.

AB - Hypersonic flight conditions produce temperature variations that can alter both the structural dynamics and flight dynamics. These aerothermoelastic effects are modeled by a nonlinear, temperature-dependent, parameter-varying state-space representation. The model includes an uncertain parameter-varying state matrix, an uncertain parameter-varying nonsquare (column-deficient) input matrix, and a nonlinear additive bounded disturbance. A Lyapunov-based continuous robust controller is developed that yields exponential tracking of a reference model, despite the presence of bounded nonvanishing disturbances. Simulation results for a hypersonic aircraft are provided to demonstrate the robustness and efficacy of the proposed controller.

KW - hypersonic flight control

KW - aircraft structural dynamics

KW - flight dynamics

UR - https://arc.aiaa.org/doi/pdf/10.2514/1.46785

U2 - 10.2514/1.46785

DO - 10.2514/1.46785

M3 - Article

SN - 1533-3884

VL - 33

JO - Journal of Guidance, Control, and Dynamics

JF - Journal of Guidance, Control, and Dynamics

ER -

Lyapunov-Based Exponential Tracking Control of a Hypersonic Aircraft with Aerothermoelastic Effects

Abstract

Keywords

Disciplines

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