2021
DOI: 10.1007/s40998-021-00424-x
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Fault-Tolerant Adaptive Asymptotic Attitude Tracking Control for a Rigid Spacecraft

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Cited by 5 publications
(5 citation statements)
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“…Recently, there has been a great deal of attention on the analysis of a class of systems known as predefined-time stable systems [21][22][23][24][25][26], since the settling time boundary of such systems is an exactly known design parameter. In the view of the advantage of predefinedtime stability, predefined-time system identification should be also investigated for the sake of estimation time presetting.…”
Section: Introductionmentioning
confidence: 99%
“…Recently, there has been a great deal of attention on the analysis of a class of systems known as predefined-time stable systems [21][22][23][24][25][26], since the settling time boundary of such systems is an exactly known design parameter. In the view of the advantage of predefinedtime stability, predefined-time system identification should be also investigated for the sake of estimation time presetting.…”
Section: Introductionmentioning
confidence: 99%
“…On the one hand, the on‐orbit spacecrafts are inevitably influenced by uncertain inertia properties (caused by fuel consumption, appendage variation, etc.) [5], unknown unstructured disturbance (e.g., J2$$ {J}_2 $$ perturbation, atmospheric resistance and electromagnetic field force) [6, 7], and actuator failure (owing to harsh space environment, e.g., high and low temperature, high energy particle impact, friction, and corrosion) [8]. On the other hand, physical limitations are due to the finite on‐board energy and computational resource, which requires the control algorithm should be as simple as possible [9].…”
Section: Introductionmentioning
confidence: 99%
“…Wang et al. [18] proposed an adaptive asymptotic fault‐tolerant attitude tracking control approach for a rigid spacecraft, and by applying an adaptive control method to approximate system uncertainties, the attitude tracking error converged to zero asymptotically. Additional results in this issue can be found in [19–21].…”
Section: Introductionmentioning
confidence: 99%
“…For example, Zhai et al [17] investigated the problem of adaptive fault-tolerant control for a class of non-linear systems, and a constructive design method for the problem was set up by exploiting a parameter separation and regrouping technique. Wang et al [18] proposed an adaptive asymptotic fault-tolerant attitude tracking control approach for a rigid spacecraft, and by applying an adaptive control method to approximate system uncertainties, the attitude tracking error converged to zero asymptotically. Additional results in this issue can be found in [19][20][21].…”
Section: Introductionmentioning
confidence: 99%