Coupled Dynamics and Integrated Control for position and attitude motions of spacecraft: a survey

F Zhang, G Duan - IEEE/CAA journal of Automatica sinica, 2023 - ieeexplore.ieee.org
Inspired by the integrated guidance and control design for endo-atmospheric aircraft, the
integrated position and attitude control of spacecraft has attracted increasing attention and …

Integrated relative position and attitude control of spacecraft in proximity operation missions

F Zhang, GR Duan - International Journal of Automation and Computing, 2012 - Springer
This paper addresses an integrated relative position and attitude control strategy for a
pursuer spacecraft flying to a space target in proximity operation missions. Relative …

Integrated translational and rotational control for the final approach phase of rendezvous and docking

H Yan, S Tan, Y Xie - Asian Journal of Control, 2018 - Wiley Online Library
This paper presents an approach of integrated translational and rotational control (ITRC)
design for the final approach phase of rendezvous and docking on an ellipse orbit. First …

Dynamics of a spacecraft with large flexible appendage constrained by multi-strut passive damper

YH Jia, SJ Xu, Q Hu - Acta Mechanica Sinica, 2013 - Springer
This paper is concerned with the dynamics of a spacecraft with multi-strut passive damper
for large flexible appendage. The damper platform is connected to the spacecraft by a …

Integrated translational and rotational control for rendezvous and docking on ellipse orbits

H Yan, S Tan, Y Xie - 2016 12th World Congress on Intelligent …, 2016 - ieeexplore.ieee.org
This paper presents an approach of integrated translational and rotational control (ITRC)
design for the final approach phase of rendezvous and docking on an ellipse orbit. First …

Guidance and robust control methods for the approach phase between two orbital vehicles with coupling between translational and rotational motions

LS Urbina - 2017 - theses.hal.science
The techniques related to formation flying and proximity operations of autonomous satellites
belong to the most significant and challenging operational space technologies of the last …

Flexible spacecraft optimal attitude maneuver with SMDO

M Cui, S Xu - 2011 International Conference on Electrical and …, 2011 - ieeexplore.ieee.org
The SMDO (Sliding Mode Disturbance Observer) is introduced in optimal attitude maneuver
control law for high-precision attitude control of flexible spacecraft which consists of rigid …

Integrated optimal and robust control of spacecraft in proximity operations

H Pan - 2011 - search.proquest.com
With the rapid growth of space activities and advancement of aerospace science and
technology, many autonomous space missions have been proliferating in recent decades …