Adaptive Output Control of Uncertain Nonlinear Systems with Unknown Backlash

Zhou, Jing; Chen, Wen; Zhang, Chengjin; Xiao-zhong, Shen

doi:10.1109/acc.2007.4282311

Cited by 12 publications

(14 citation statements)

References 11 publications

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“…To derive the fault-tolerant controller, the following two filters are employed [11]: T , and the matrix…”

Section: A State Estimation Filters Designmentioning

confidence: 99%

“…where i N i e i t is a virtual control law [11], and i is a positive constant, satisfies _ z i;1 i , and…”

Section: A State Estimation Filters Designmentioning

confidence: 99%

“…Therefore, z i;1 , z i;2 , e i , , andx a i are bounded on 0; t f for all t f > 0; in view of Eqs. (11) and (24), it can be known that all the signals in the closed-loop system are bounded on 0; t f for all t f > 0. Thus, according to [10], all the signals in the closed-loop system are bounded for t f 1.…”

Section: A State Estimation Filters Designmentioning

confidence: 99%

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Fault-Tolerant Attitude Control for Spacecraft Under Loss of Actuator Effectiveness

Xiao

Zhang

2011

Journal of Guidance, Control, and Dynamics

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“…To derive the fault-tolerant controller, the following two filters are employed [11]: T , and the matrix…”

Section: A State Estimation Filters Designmentioning

confidence: 99%

“…where i N i e i t is a virtual control law [11], and i is a positive constant, satisfies _ z i;1 i , and…”

Section: A State Estimation Filters Designmentioning

confidence: 99%

See 1 more Smart Citation

Fault-Tolerant Attitude Control for Spacecraft Under Loss of Actuator Effectiveness

Xiao

Zhang

2011

Journal of Guidance, Control, and Dynamics

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“…To overcome these restrictions, recursive and systematic backstepping design was developed by Kanellakopoulos (1991). In the past decade, backstepping has become one of the most popular design methods for adaptive nonlinear control and synchronization [5][6][7], because it can guarantee global stabilities, tracking and transient performance for the broad class of strict-feedback systems [7][8][9].…”

Section: Introductionmentioning

confidence: 99%

Adaptive Backstepping Control for a Class of Nonlinear Systems

Jiang

Gao

2011

2011 Third International Conference on Measuring Technology and Mechatronics Automation

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Tracking control of nonlinear uncertain Chua's chaotic systems is studied. Based on coordinate transform, the paper deduced the principle with which Chua's chaotic system can be translated into the so-called general strict-feedback form. Combining the backstepping method with robust control technology, an adaptive parameter control law is developed and thus the output tracking is successfully accomplished for the system with unknown parameters and dynamic uncertainties. It is proved that the derived robust adaptive controller based on Lyapunov stability theory can guarantee that all states of the closed-loop system are globally uniformly ultimately bounded, and lead the system tracking error to a small neighborhood. Finally simulation results are provided to show the effectiveness of the proposed approach.

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“…However, the unstructured plant parameter variations are required to have small speed. A new control scheme incorporating with adaptive backstepping technique is considered in [22], in which the control objectives are achieved by introducing estimator to estimate the bound of the variation rate of parameters with Nussbaum type function. However, these aforementioned methods cannot be directly applied to the spacecraft attitude system with time-varying fault, and to the best of our knowledge, there are few works dealing with MIMO time-varying issue at present stage.…”

Section: Introductionmentioning

confidence: 99%

Adaptive Backstepping Based Fault Tolerant Spacecraft Attitude Control under Loss of Actuator Effectiveness

Xiao

Zhang³

2010

AIAA Guidance, Navigation, and Control Conference

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In this paper, an adaptive backstepping technique based fault tolerant control scheme is developed for a spacecraft attitude stabilization system, in which the external disturbances and partial loss of actuator effectiveness fault are considered. More specifically, using the adaptive backstepping control method, a baseline control law is first proposed for the normal system without actuator fault; then this is extended to the faulty system by adding an auxiliary system, which is used to compensate the actuator fault by designing the control input of the auxiliary system such that the output of the auxiliary system can follow the specified commands of the normal system. As motivated from practical spacecraft control applications, synthesis of controller in the presence of faults with no knowledge of fault time, pattern and value. Complete stability and performance analysis are presented and illustrative simulation results of an application to spacecraft attitude control show that the high precise attitude control is successfully achieved using various scenarios of partial loss of control effectiveness induced by actuator failures.

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Adaptive Output Control of Uncertain Nonlinear Systems with Unknown Backlash

Cited by 12 publications

References 11 publications

Fault-Tolerant Attitude Control for Spacecraft Under Loss of Actuator Effectiveness

Fault-Tolerant Attitude Control for Spacecraft Under Loss of Actuator Effectiveness

Adaptive Backstepping Control for a Class of Nonlinear Systems

Adaptive Backstepping Based Fault Tolerant Spacecraft Attitude Control under Loss of Actuator Effectiveness

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