2019
DOI: 10.1109/taes.2019.2906096
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Adaptive Finite-Time 6-DOF Tracking Control for Spacecraft Fly Around With Input Saturation and State Constraints

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Cited by 50 publications
(32 citation statements)
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“…whereˆi x is the observation states, and the fuzzy system function fitting the compound uncertainties can satisfy: xn is An j then θi j , where A1 j , A2 j ,..., An j are fuzzy variables and θi j is an element of adjustable parameter vector. By using product inference, center-average and singleton fuzzifier, the output of the fuzzy system can be expressed as (17) where fuzzy basis function ξi j satisfies…”
Section: State Observer Designmentioning
confidence: 99%
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“…whereˆi x is the observation states, and the fuzzy system function fitting the compound uncertainties can satisfy: xn is An j then θi j , where A1 j , A2 j ,..., An j are fuzzy variables and θi j is an element of adjustable parameter vector. By using product inference, center-average and singleton fuzzifier, the output of the fuzzy system can be expressed as (17) where fuzzy basis function ξi j satisfies…”
Section: State Observer Designmentioning
confidence: 99%
“…The deflection range of the rudder angle is ±20deg, and the magnitude of the harmonic interference torque on the pitch axis is: 2×106sin(2t). The traditional method (TM) in [17] shows strong robustness when only considering the presence of interference on the pitch axis. In this paper, the uncertainty of aerodynamic parameters is fully considered.…”
Section: Simulation Verification Experimentsmentioning
confidence: 99%
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“…For example, considering second-order multi-agent systems, Zhai [12] gives a discussion on this issue and designed the distributed controller under the input saturation constraint. And an adaptive finite-time control scheme is developed for noncooperative spacecraft fly-around subject to input saturation in [13]. However, to the best of our knowledge, there are few results considering the input saturation constraint for a wheeled mobile robot, whose dynamics is described by a rigid body on Lie group SE (2).…”
Section: Introductionmentioning
confidence: 99%