2023
DOI: 10.1109/tsmc.2022.3174845
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Constrained Attitude Control of Uncertain Spacecraft With Appointed-Time Control Performance

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Cited by 7 publications
(2 citation statements)
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“…On this basis, this paper will continue to carry out the research on the attitude of FTC of space tumbling target fly-around. In addition, there have been many mature research results on spacecraft attitude, such as SO (3) [32], quaternion [33], Rodriguez [34], etc. In this study, the error quaternion attitude dynamics equations will be established in the RLOS coordinate system.…”
Section: Introductionmentioning
confidence: 99%
“…On this basis, this paper will continue to carry out the research on the attitude of FTC of space tumbling target fly-around. In addition, there have been many mature research results on spacecraft attitude, such as SO (3) [32], quaternion [33], Rodriguez [34], etc. In this study, the error quaternion attitude dynamics equations will be established in the RLOS coordinate system.…”
Section: Introductionmentioning
confidence: 99%
“…In Reference 18 a vector-based adaptive control scheme was proposed for the constrained attitude tracking problem in the presence of parameter uncertainties and external disturbances. Note that the aforementioned results [16][17][18] are mainly concerned with epistemic uncertainties, which caused by lack of knowledge of flexible spacecraft properties or space environment during the attitude control system modeling and simulation. 19 Besides epistemic uncertainties, stochastic uncertainties caused by the randomness of the external environment or spacecraft properties also degrade the performance of the control system.…”
Section: Introductionmentioning
confidence: 99%