2017
DOI: 10.1177/1687814017696413
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Extended state observer–based finite-time controller design for coupled spacecraft formation with actuator saturation

Abstract: This article investigates the consensus tracking control problem of the leader-follower spacecraft formation system in the presence of model uncertainties, external disturbances, and actuator saturation, where the relative motion of the leader and the follower need to track a desired time-varying trajectory given in advance. First, the six-degree-of-freedom relative-coupled translational and rotational dynamics models are derived using the exponential coordinates on the Lie group SE(3). Then, a fast terminal s… Show more

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Cited by 25 publications
(20 citation statements)
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References 29 publications
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“…after performing the congruence transformation with matrix diag{Z 1 , I, I, Z 1 , I} on condition (35), and matrix diag{I, Z 1 } on condition (36), we obtain the same results as those of (29) and (30). This verifies equivalency between condition (32) and condition (35), as well as condition (33) and condition (36).…”
Section: Convex Synthesis Of Dynamic Relative Output-feedback Satusupporting
confidence: 69%
See 2 more Smart Citations
“…after performing the congruence transformation with matrix diag{Z 1 , I, I, Z 1 , I} on condition (35), and matrix diag{I, Z 1 } on condition (36), we obtain the same results as those of (29) and (30). This verifies equivalency between condition (32) and condition (35), as well as condition (33) and condition (36).…”
Section: Convex Synthesis Of Dynamic Relative Output-feedback Satusupporting
confidence: 69%
“…This verifies equivalency between condition (32) and condition (35), as well as condition (33) and condition (36). The controller reconstruction formula (26) can also be verified by inverting the relations in (30). This ends the proof.…”
Section: Convex Synthesis Of Dynamic Relative Output-feedback Satusupporting
confidence: 60%
See 1 more Smart Citation
“…A composite control law that employs extended state observer (ESO) and an additive controller was developed to remove external disturbance in Chen et al (2018). Another ESO-based control laws were presented in Ye et al (2017) and Li et al (2016) for formation flying of spacecraft. Back-stepping was combined with the observer to formulate a stabilization control scheme in Sun and Zheng (2017).…”
Section: Introductionmentioning
confidence: 99%
“…In the paper by Zhi et al, 10 the spectral radius of extremal graphs for the unicyclic graphs is investigated using graft transformation and matching, and the upper bounds of the spectral radius of unicyclic graphs are obtained using the relations between degree and the second degree. The second group starts with a paper on finite-time controller design for coupled spacecraft formation with actuator saturation by Ye et al 11 This article investigates the consensus tracking control issue for a class of leader-follower spacecraft formation system, considering the occurrence of model uncertainties, external disturbances, and actuator saturation. A 6degree-of-freedom (DOF) relative-coupled translational and rotational dynamics model is derived with the aid of exponential coordinates on the Lie group SE(3).…”
mentioning
confidence: 99%