Agile attitude maneuver with active vibration-suppression for flexible spacecraft-Reference-Cited by-同舟云学术

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Agile attitude maneuver with active vibration-suppression for flexible spacecraft

Published:2022-02 Issue:3 Volume:359 Page:1172-1195
ISSN:0016-0032
Container-title:Journal of the Franklin Institute
language:en
Short-container-title:Journal of the Franklin Institute

Author:

Zhang Jianqiao,Kong Xianglong,Liu Chuang,Deng Qing,Shi Keke

Publisher

Elsevier BV

Subject

Applied Mathematics,Computer Networks and Communications,Signal Processing,Control and Systems Engineering

Reference40 articles.

1. On the attitude stabilization of a rigid spacecraft using two skew control moment gyros;Gui;Nonlinear Dyn.,2015

2. Singularity escape/avoidance steering logic for control moment gyro systems;Wei;J. Guid. Control Dyn.,2005

3. Nonlinear analysis of discrete-time sliding mode prediction deployment of tethered space robot;Ma;IEEE Trans. Ind. Electron.,2021

4. Implementation of shortest-time maneuvers for generic CMG steering laws;Karpenko,2012

5. Inertia-free attitude stabilization for flexible spacecraft with active vibration suppression;Liu;Int. J. Robust Nonlinear Control,2019

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1. Multi-objective design of parametric equivalent-input-disturbance approaches with application to vehicle suspension systems;Journal of the Franklin Institute;2024-07

2. Design of anti-unwinding attitude coupling controller for flexible spacecraft using positive position feedback control;Acta Astronautica;2024-05

3. Hybrid control of attitude maneuver and structural vibration for a large phased array antenna satellite;Journal of the Franklin Institute;2024-01

4. Non-fragile negative imaginary output feedback control for attitude stabilization of flexible spacecraft;Acta Astronautica;2023-07

5. Dynamics and Control of Flexible Satellite Using Reaction Sphere Actuators;Space: Science & Technology;2023-01

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