Spacecraft adaptive nonlinear attitude tracking with harmonic disturbances and inertia uncertainties

In this paper, an adaptive controller is proposed for spacecraft attitude tracking problem subject to inertia uncertainties and harmonic disturbances. A class of sinusoidal disturbances with known frequencies but unknown amplitudes and phase angles are considered. The proposed controller is composed...

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Published inChinese Control Conference pp. 8753 - 8758
Main Authors Li, Chuanjiang, Guo, Yanning, Ma, Guangfu, Du, Shaohe
Format Conference Proceeding
LanguageEnglish
Published TCCT, CAA 01.07.2014
Subjects
Adaptive control
Attitude tracking
Decision support systems
Global asymptotic stability
Harmonic disturbances
Transient performance
Online AccessGet full text
ISSN1934-1768
DOI10.1109/ChiCC.2014.6896471

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Abstract In this paper, an adaptive controller is proposed for spacecraft attitude tracking problem subject to inertia uncertainties and harmonic disturbances. A class of sinusoidal disturbances with known frequencies but unknown amplitudes and phase angles are considered. The proposed controller is composed of a nonlinear proportional-derivative (PD) control part and an adaptive control part. The internal model control is utilized to identify the harmonic disturbances. The nonlinear PD control term is designed to achieve better tracking performance with shorter settling time and smaller/no overshoot. The overall closed-loop tracking error system is shown to be globally asymptotically stable via Lyapunov stability theory. Finally, numerical simulations are carried out to illustrate the effectiveness of the proposed methodology.
AbstractList In this paper, an adaptive controller is proposed for spacecraft attitude tracking problem subject to inertia uncertainties and harmonic disturbances. A class of sinusoidal disturbances with known frequencies but unknown amplitudes and phase angles are considered. The proposed controller is composed of a nonlinear proportional-derivative (PD) control part and an adaptive control part. The internal model control is utilized to identify the harmonic disturbances. The nonlinear PD control term is designed to achieve better tracking performance with shorter settling time and smaller/no overshoot. The overall closed-loop tracking error system is shown to be globally asymptotically stable via Lyapunov stability theory. Finally, numerical simulations are carried out to illustrate the effectiveness of the proposed methodology.
Author Guo, Yanning
Du, Shaohe
Ma, Guangfu
Li, Chuanjiang
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  givenname: Shaohe
  surname: Du
  fullname: Du, Shaohe
  organization: Dept. of Control Sci. & Eng., Harbin Inst. of Technology, Harbin, China
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Snippet In this paper, an adaptive controller is proposed for spacecraft attitude tracking problem subject to inertia uncertainties and harmonic disturbances. A class...
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StartPage 8753
SubjectTerms Adaptive control
Attitude tracking
Decision support systems
Global asymptotic stability
Harmonic disturbances
Transient performance
Title Spacecraft adaptive nonlinear attitude tracking with harmonic disturbances and inertia uncertainties
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