[HTML][HTML] Survey of orbital dynamics and control of space rendezvous

Y Luo, J Zhang, G Tang - Chinese Journal of Aeronautics, 2014 - Elsevier
Rendezvous orbital dynamics and control (RODC) is a key technology for operating space
rendezvous and docking missions. This paper surveys the studies on RODC. Firstly, the …

[HTML][HTML] 航天器动力学与控制的研究进展与展望

黄文虎, 曹登庆, 韩增尧 - 力学进展, 2012 - lxjz.cstam.org.cn
开展航天器动力学与控制的研究在航天技术的发展中起到举足轻重的作用,
其目的在于发展有效的方法促使航天器在各阶段平稳可靠地运行. 航天器技术发展迅速 …

A 6-DOF sliding mode fault tolerant control solution for in-orbit autonomous rendezvous

D Henry, J Zenteno-Torres, J Cieslak… - Aerospace Science and …, 2021 - Elsevier
The goal pursued by this article, is to evaluate the potential of sliding-mode control and
estimation techniques, to address fault tolerance against a large class of actuator faults …

Optimal impulsive control using adaptive dynamic programming and its application in spacecraft rendezvous

A Heydari - IEEE Transactions on Neural Networks and …, 2020 - ieeexplore.ieee.org
Optimal control of nonlinear impulsive systems with free impulse instants and the number of
impulses is investigated in this study. A scheme based on adaptive dynamic programming is …

Robust adaptive fixed‐time tracking control of 6‐DOF spacecraft fly‐around mission for noncooperative target

Y Huang, Y Jia - International Journal of Robust and Nonlinear …, 2018 - Wiley Online Library
The fixed‐time relative position tracking and attitude synchronization control problem of a
spacecraft fly‐around mission for a noncooperative target in the presence of parameter …

Active fault tolerant control design approach for the flexible spacecraft with sensor faults

Z Gao, B Han, G Jiang, J Lin, D Xu - Journal of the Franklin Institute, 2017 - Elsevier
In this paper, the problem of active fault tolerant control (FTC) is studied for a class of flexible
spacecraft attitude systems with Lipschitz nonlinearity and sensor fault. Firstly, a functional …

Bi-level game-based reconfigurable control for on-orbit assembly

Y Chai, J Luo, M Wang - Aerospace Science and Technology, 2022 - Elsevier
During on-orbit assembly, microsatellites are used to provide control ability for substructures
to be assembled. Every time a substructure is assembled to the combination composed of …

[HTML][HTML] Advances and trends in dynamics and control of spacecrafts

H Wenhu, C Dengqing, H Zengyao - 力学进展, 2012 - lxjz.cstam.org.cn
The research on dynamics and control of spacecrafts for the purpose of establishing
effective strategies to ensure reliable operation of spacecrafts at each stage plays a …

Optimization of control parameters based on genetic algorithms for spacecraft attitude tracking with input constraints

Y Jia, X Yang - Neurocomputing, 2016 - Elsevier
This paper studies the attitude tracking control problem for rigid spacecraft with input
constraint, parameter uncertainties and harmonic disturbances. By combining a nonlinear …

Autonomous impulsive rendezvous for spacecraft under orbital uncertainty and thruster faults

Z Li, X Yang, H Gao - Journal of the Franklin Institute, 2013 - Elsevier
This paper investigates the reliable impulsive control problem for autonomous spacecraft
rendezvous under the orbital uncertainty and possible thruster faults. The orbital uncertainty …