Finite‐time attitude tracking control for rigid spacecraft with control input constraints

Zou, An‐Min; Ruiter, Anton H. J. de; Kumar, Krishna Dev

doi:10.1049/iet-cta.2016.1097

Cited by 48 publications

(24 citation statements)

References 36 publications

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“…However, considering disturbances, the tracking errors only converge to a small neighborhoods of zero. In [13]- [15], finite-time controllers using the homogeneous method were investigated for rigid spacecraft. Although they guarantee the closed-loop system finite-time stable, they don't consider the disturbances and uncertainties.…”

Section: Introductionmentioning

confidence: 99%

Adaptive Nonsingular Terminal Sliding Mode Control for Attitude Tracking of Spacecraft With Actuator Faults

Jing

Niu

et al. 2019

IEEE Access

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In this paper, an adaptive nonsingular terminal sliding mode control (ANTSMC) is investigated for attitude tracking of spacecraft with actuator faults. First, a nonsingular fast terminal sliding mode surface is designed to avoid the singularity. Finite-time attitude control is developed using the nonsingular terminal sliding mode technique, which can make the attitude and angular velocity tracking errors converge to zero in finite time in the presence of uncertainties and external disturbances. Second, the total uncertainty is deduced to be bounded. The adaptive laws are incorporated to develop the ANTSMC, removing the restriction on the upper bound of the lumped uncertainty. The finite-time convergence of the closed-loop system with ANTSMC is proved using the Lyapunov stability theory. Finally, the simulation results are presented to demonstrate the performance of the proposed controllers. INDEX TERMS Spacecraft, nonsingular terminal sliding mode, adaptive, finite time, attitude control, actuator faults.

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Section: Introductionmentioning

confidence: 99%

Adaptive Nonsingular Terminal Sliding Mode Control for Attitude Tracking of Spacecraft With Actuator Faults

Jing

Niu

et al. 2019

IEEE Access

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“…Based on a non‐linear angular velocity observer, a saturated finite‐time velocity‐free attitude contorl is proposed in [26]. With a new smooth model for input saturation, Zou et al [27] address the problem of velocity‐free attitude tracking control with input constraints.…”

Section: Introductionmentioning

confidence: 99%

Global saturated velocity‐free finite‐time control for attitude tracking of spacecraft

Xia

2019

IET Control Theory & Applications

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“…[23] used the adaptive method to estimate the resulting approximation error between constrained control input and smooth function. An input saturated model was built and considered as the part of the control law [24, 25]. In [26–28], the effect of input saturation was compensated by the disturbance observer.…”

Section: Introductionmentioning

confidence: 99%

Dynamic infinity‐norm constrained control allocation for attitude tracking control of overactuated combined spacecraft

Huang

Duan

2019

IET Control Theory & Applications

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Finite‐time attitude tracking control for rigid spacecraft with control input constraints

Cited by 48 publications

References 36 publications

Adaptive Nonsingular Terminal Sliding Mode Control for Attitude Tracking of Spacecraft With Actuator Faults

Adaptive Nonsingular Terminal Sliding Mode Control for Attitude Tracking of Spacecraft With Actuator Faults

Global saturated velocity‐free finite‐time control for attitude tracking of spacecraft

Dynamic infinity‐norm constrained control allocation for attitude tracking control of overactuated combined spacecraft

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