Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization

Du, Haibo; Li, Shengbo Eben; Qian, Chunjiang

doi:10.1109/tac.2011.2159419

Cited by 693 publications

(353 citation statements)

References 18 publications

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“…Recently, some researchers have paid their attentions to synchronization of chaotic systems in finite-time. Finite-time control techniques have been proposed for synchronization of some pratical chaotic systems by Sun, Wu, Bai, Wei, and Sun (2016) ;Liu, Li, and Feng (2016) and Du, Li, and Qian (2011). Moreover, Mobayen (2016) studied finite-time synchronization of chaotic systems with matched and unmatched uncertainties via LMI technique.…”

Section: Introductionmentioning

confidence: 99%

Robust finite-time synchronization of uncertain chaotic systems: application on Duffing-Holmes system and chaos gyros

Mohammadpour

Binazadeh

2018

Systems Science & Control Engineering

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This paper considers the finite-time synchronization of chaotic systems in the presence of model uncertainties and/or external disturbances. The synchronization happens between the two nonlinear master and slave systems. Control law is designed in such a way that the state variables of the slave system follow the state variables of the master system in the presence of uncertainties and external disturbances. In order to design a robust finite-time controller, first, a novel terminal sliding surface is proposed and its finite-time convergence to zero is analytically proved. Then a terminal sliding mode controller is designed which can conquer the uncertainties and guarantees the finitetime stability of the sliding motion equations. In this regard, a theorem is proposed and according to the Lyapunov approach it is proved that the synchronization happenes in finite-time. Additionally, in order to show the applicability of the proposed controller, it is applied on two practical systems, the Duffing-Holmes system and chaotic gyroscope system. Computer simulations verify the theoretical results and also display the effective performance of the proposed controller. ARTICLE HISTORY

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Section: Introductionmentioning

confidence: 99%

Robust finite-time synchronization of uncertain chaotic systems: application on Duffing-Holmes system and chaos gyros

Mohammadpour

Binazadeh

2018

Systems Science & Control Engineering

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“…Based on geometric homogeneity and separation principles, global attitude controllers are proposed in [11][12]. Du and Li [13] adopt adding a power integrator and finite time theory to design attitude tracking controller and distributed attitude control law. Furthermore, fixed-time attitude control schemes [14] are initially proposed to steer attitude tracking errors to the origin.…”

Section: Introductionmentioning

confidence: 99%

Robust Finite Time Control for Stabilization of Rigid Spacecraft

Tang¹,

Cai²,

Gao³

et al. 2018

Proceedings of the 2017 2nd International Conference on Electrical, Control and Automation Engineering (ECAE 2017)

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“…[1][2][3][4][5][6][7] There have been numerous valuable research studies on attitude control of spacecraft, such as adaptive attitude synchronization control, [8][9][10][11][12] finite-time attitude coordination control, [13][14][15][16] and fast terminal sliding-mode control. [17][18][19][20] Because of fuel consumption and onboard payload working such as rotation of solar arrays, the inertia of spacecraft is time-varying.…”

Section: Introductionmentioning

confidence: 99%

“…8,13,15,20 Yang et al 8 studied the problem of attitude tracking control for spacecraft formation with external disturbances and designed an adaptive control method to fulfill attitude synchronization under a directed communication topology. Du et al 13 studied the finite-time attitude control problems for multiple spacecraft and proposed a distributed finite-time attitude control law to guarantee the tracking errors to reach a region around the origin with leader-follower architecture. Hu et al 15 coped with a bounded finite-time attitude coordinated control problem for SFF under a connected graph.…”

Section: Introductionmentioning

confidence: 99%

Adaptive fault‐tolerant attitude tracking control for spacecraft formation with unknown inertia

Zhu

Guo

2017

Adaptive Control & Signal

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SummaryIn this paper, an adaptive fault-tolerant attitude coordinated tracking problem for spacecraft formation is investigated under a directed communication topology containing a spanning tree with the leader as the root, where inertia matrices and external disturbances are unknown time-varying. With no prior knowledge of faults and inertia, an adaptive approach is proposed to reject the influence of disturbances and uncertainties. Meanwhile, combining with a consensus algorithm and graph theory, an adaptive fault-tolerant attitude synchronization tracking control law is presented to regulate the attitude to a common time-varying reference state. Aiming at optimizing the control law, a dynamic adjustment function is introduced to adjust the control gain according to the attitude tracking error. The effectiveness of the proposed control approach is demonstrated through simulation results.

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Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization

Cited by 693 publications

References 18 publications

Robust finite-time synchronization of uncertain chaotic systems: application on Duffing-Holmes system and chaos gyros

Robust finite-time synchronization of uncertain chaotic systems: application on Duffing-Holmes system and chaos gyros

Robust Finite Time Control for Stabilization of Rigid Spacecraft

Adaptive fault‐tolerant attitude tracking control for spacecraft formation with unknown inertia

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