2015
DOI: 10.1080/00207179.2014.996854
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Finite-time attitude tracking control for a rigid spacecraft using time-varying terminal sliding mode techniques

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Cited by 106 publications
(60 citation statements)
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“…Figure 7 shows the response curves of control law for followers 1 to 3, and the chattering is eliminated. The above simulation results show that the proposed control laws (8) and (20) can both provide good robustness against the unknown external disturbances.…”
Section: Simulation Resultsmentioning
confidence: 87%
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“…Figure 7 shows the response curves of control law for followers 1 to 3, and the chattering is eliminated. The above simulation results show that the proposed control laws (8) and (20) can both provide good robustness against the unknown external disturbances.…”
Section: Simulation Resultsmentioning
confidence: 87%
“…Figure 5 gives the trajectories of agents 1 to 7 by using control law (20), which shows that followers 1 to 3 move into the convex hull formed by leaders 4 to 7. Figure 6 shows the response curves of errors Figure 5: Trajectories of agents 1 to 7 using control law (20). The circles and squares represent the leaders and the followers, respectively.…”
Section: Simulation Resultsmentioning
confidence: 99%
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“…Conversely, SMC (Ahmad, & Zhu, 2015;Utikin, 1992), because of its various attractive features such as quick response, good transient performance, particularly, the valuable invariance against matched uncertainties, has been well known as an effective robust control strategy and also has found to be widely applied to various complex systems (Basin, Ferreira, & Fridman, 2007;Liu, & Gao, 2016;Wu, & Lam, 2008;Zhao, & Zhu, 2014) as well in many technical problems (Zhao, & Jia, 2015). As for the neutral systems, some excellent works have been reported.…”
Section: ∆B(χ T) = B∆b(χ T) G(x χ T) = B∆g(x χ T)mentioning
confidence: 99%