Proceedings ArticleDOI
Fuzzy Sliding Mode Attitude Control of Satellite
TLDR
The adaptive fuzzy sliding mode control is applied to the attitude stabilization of flexible satellite and the hitting control, which guarantees the stability of the control system, is developed.Abstract:
The adaptive fuzzy sliding mode control is applied to the attitude stabilization of flexible satellite. The detailed design procedure of the fuzzy sliding mode control system is presented. The adaptive fuzzy control is utilized to approach the equivalent control of sliding mode control and the adaptive law is derived. The hitting control, which guarantees the stability of the control system, is developed. In order to attenuate the chattering phenomena, fuzzy rules are employed to smooth the hitting control. Simulation results show precise attitude control is accomplished based on the proposed method.read more
Citations
More filters
Journal ArticleDOI
Self-tuning PID controller to three-axis stabilization of a satellite with unknown parameters
TL;DR: The three-axis stabilization of a satellite system in the presence of the gravity gradient and orbital eccentricity is addressed by using Lyapunov approach and a self-tuning PID controller is designed to produce control signals for three reaction wheels in three axes.
Book ChapterDOI
Integral Sliding-Based Robust Control
TL;DR: In this paper, the robust performance control based on integral sliding-mode for system with nonlinearities and perturbations that consist of external disturbances and model uncertainties of great possibility time-varying manner is studied.
Proceedings ArticleDOI
A survey of control strategies for spacecraft attitude and orientation
TL;DR: A survey of different control methods deployed for spacecraft attitude control with a focus on strengths, weaknesses and opportunities for improvement is presented in this paper, where the authors highlight the need for low cost, robustness, precision, high efficiency and low computational load.
Proceedings ArticleDOI
Application of decaying boundary layer and switching function method thorough error feedback for sliding mode control on spacecraft's attitude
TL;DR: The proposed technique is shown to reduce chattering permanently and also retain control output accuracy and the novel decaying boundary layer and switching function to improve the earlier version is proposed.
Proceedings ArticleDOI
Fuzzy sliding mode controller design for spacecraft attitude tracking in terms of quaternion
A. Mohammad,S.S. Ehsan +1 more
TL;DR: In this paper, a fuzzy sliding mode control (FSMC) for spacecraft attitude tracking in terms of quaternion is designed, and the proposed controller design is simulated on an assumed case study with uncertain parameters and external disturbances.
References
More filters
Journal ArticleDOI
A stability approach to fuzzy control design for nonlinear systems
Guang-Chyan Hwang,Shih-Chang Lin +1 more
TL;DR: The fuzzy sliding mode control method, developed by the application of fuzzy set theory, provides a simple way to achieve asymptotic stability of the systems and is capable of handling the chattering problem inherent to sliding Mode control simply and effectively.
Journal ArticleDOI
Robust Adaptive Variable Structure Control of Spacecraft Under Control Input Saturation
TL;DR: In this article, two globally stable control algorithms for robust stabilization of spacecraft in the presence of control input saturation, parametric uncertainty, and external disturbances are proposed and a detailed stability analysis for the resulting closed-loop system is provided.
Journal ArticleDOI
Robust control by fuzzy sliding mode
TL;DR: The performance and the robustness of this kind of FC stems from their property of driving the system into the sliding mode (SM), in which the controlled system is invariant to parameter fluctuations and disturbances.
Journal ArticleDOI
Sliding-mode controller design for spacecraft attitude tracking maneuvers
Yon-Ping Chen,Shih-Che Lo +1 more
TL;DR: A robust sliding-mode control law is presented to deal with the spacecraft attitude tracking problems by using the second method of Lyapunov thoery to achieve system stability in the sliding mode.
Journal ArticleDOI
On the pointing robustness issue of a class of new generation spacecraft
F. Karray,V. Modi +1 more
TL;DR: A control design procedure for dealing with the robust slewing and pointing manoeuvres of a class of new generation spacecraft is proposed, based on the application of the optimal interpolation technique to the sliding control approach.