2023
DOI: 10.1109/tnnls.2022.3144493
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Neural-Network-Based Adaptive Finite-Time Output Feedback Control for Spacecraft Attitude Tracking

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Cited by 22 publications
(9 citation statements)
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“…Input: The parameters τ 1 , τ i , and b in intermediate variables (16); the parameters ℓ > 0, ψ > 0, and β > 1 in virtual control laws (21), (31), and (45) and actual controller (53); the parameters γ i > 0, ℓ > 0, µ > 0, and ψ > 0 in adaptive laws (22), (32), ( 46), (54), and (55); the parameter δ i in disturbance observers (23), (33), (44)…”
Section: Algorithm 1 Algorithm To Design Fixed-time Fuzzy Controllermentioning
confidence: 99%
See 1 more Smart Citation
“…Input: The parameters τ 1 , τ i , and b in intermediate variables (16); the parameters ℓ > 0, ψ > 0, and β > 1 in virtual control laws (21), (31), and (45) and actual controller (53); the parameters γ i > 0, ℓ > 0, µ > 0, and ψ > 0 in adaptive laws (22), (32), ( 46), (54), and (55); the parameter δ i in disturbance observers (23), (33), (44)…”
Section: Algorithm 1 Algorithm To Design Fixed-time Fuzzy Controllermentioning
confidence: 99%
“…It is worth noting that a limitation of finite-time control is its dependence on the initial states for convergence time [20][21][22][23]. The applicability of finite-time control is impeded by the necessity to have information about initial states for determining convergent time, a requirement that may not always be met due to uncertainties in the initial conditions in real-world applications [24][25][26].…”
Section: Introductionmentioning
confidence: 99%
“…To improve the robustness, an adaptive constrained controller using FLS was proposed for the flight vehicles [27]. A NN-based adaptive attitude controller was designed for the spacecraft [28]. Moreover, an adaptive switching control method using NN was proposed for a nonlinear system [29].…”
Section: Introductionmentioning
confidence: 99%
“…[17] designed a finite-time extended-state observer-based output feedback control for attitude maneuvering and the disturbance rejection of a rigid spacecraft in the presence of the actuator fault. A saturated neural-network-based adaptive output feedback attitude control with finite-time convergence has been developed in [18]. The unknown angular velocity is first estimated by a neural-state observer, and a command-filtered back-stepping control is then designed, such that the computation complexity problem is effectively resolved.…”
Section: Introductionmentioning
confidence: 99%