Attitude and Momentum Management of Inertial Oriented Spacecraft

Zhu, Minglei; Xin-long, Chen; Li, Zhi

doi:10.1061/(asce)as.1943-5525.0000471

Cited by 7 publications

(1 citation statement)

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“…For the three‐axis coupled dynamics in the local‐vertical local‐horizon frame, Harduvel constructed a control architecture with the same approach, which has been successfully applied to the International Space Station. In the inertial frame, Zhang et al and Zhu et al also used the integrated LQR and DRF controller to manage momentum. However, the works only focused on plants with fixed moment of inertia.…”

Section: Introductionmentioning

confidence: 99%

An integrated solution to ACMM problem of spacecraft with inertia uncertainty

Liu

Xue

Chen

et al. 2018

Intl J Robust & Nonlinear

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Summary In this work, an integrated solution to the attitude control and momentum management problem is studied for the velocity‐free large spacecraft subject to both inertia uncertainty and strong disturbances. A multiple‐input–multiple‐output‐type linear extended state observer is constructed to estimate the uncertain information, and a novel disturbance compensator and a linear quadratic regulator controller are proposed. The stability of the proposed scheme is rigorously proved, and the quantitative relationship between the closed‐loop tracking error and the uncertainty size is thoroughly analyzed. Comparison studies are carried out to verify the effectiveness and robustness of the proposed approach.

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Section: Introductionmentioning

confidence: 99%