Continuous finite-time extended state observer based fault tolerant control for attitude stabilization

B Li, Q Hu, Y Yang - Aerospace Science and Technology, 2019 - Elsevier
This work investigates the challenging problem of fast robust fault tolerant attitude control for
spacecraft to handle external disturbances, actuator failures and misalignments. More …

Adaptive backstepping control of spacecraft rendezvous and proximity operations with input saturation and full-state constraint

L Sun, W Huo, Z Jiao - IEEE Transactions on Industrial …, 2016 - ieeexplore.ieee.org
This paper presents a six-degree-of-freedom relative motion control method for autonomous
spacecraft rendezvous and proximity operations subject to input saturation, full-state …

Observer-based fault-tolerant attitude control for rigid spacecraft

B Li, Q Hu, Y Yu, G Ma - IEEE Transactions on Aerospace and …, 2017 - ieeexplore.ieee.org
This paper addresses the problem of robust fault-tolerant control of spacecraft attitude
stabilization in the presence of model uncertainties, actuator failures, and external …

Robust adaptive relative position tracking and attitude synchronization for spacecraft rendezvous

L Sun, W Huo - Aerospace Science and Technology, 2015 - Elsevier
This paper studies the relative position tracking and attitude synchronization of non-
cooperative spacecraft rendezvous with model uncertainty and external disturbance. The …

Feedback control for spacecraft reorientation under attitude constraints via convex potentials

U Lee, M Mesbahi - IEEE Transactions on Aerospace and …, 2014 - ieeexplore.ieee.org
A novel guidance algorithm is proposed for the attitude reorientation of a rigid body
spacecraft in the presence of multiple types of attitude-constrained zones. In this direction …

Neural network-based control for the on-orbit assembly of heterogeneous spacecraft cluster based on Vicsek fractal

X Pan, Z Wei, T Chen - Aerospace Science and Technology, 2024 - Elsevier
On-orbit assembly is a highly effective technique for building large space structures. This
paper presents the dynamics and control of an on-orbit assembly of a large space structure …

6-DOF integrated adaptive backstepping control for spacecraft proximity operations

L Sun, W Huo - IEEE Transactions on Aerospace and Electronic …, 2015 - ieeexplore.ieee.org
Relative motion control with 6 degrees of freedom (6 DOF) is investigated for a chaser
spacecraft with parametric uncertainties to approach an unknown tumbling space target …

Adaptive finite-time 6-DOF tracking control for spacecraft fly around with input saturation and state constraints

Y Huang, Y Jia - IEEE Transactions on Aerospace and …, 2019 - ieeexplore.ieee.org
An adaptive finite-time control scheme is developed for noncooperative spacecraft fly-
around subject to input saturation, full-state constraints, dynamic couplings, parameter …

Disturbance-observer-based robust relative pose control for spacecraft rendezvous and proximity operations under input saturation

L Sun, W Huo, Z Jiao - IEEE Transactions on Aerospace and …, 2018 - ieeexplore.ieee.org
This paper investigates the robust relative pose control for spacecraft rendezvous and
proximity operations subject to input saturation, kinematic couplings, parametric …

Finite‐time disturbance observer based integral sliding mode control for attitude stabilisation under actuator failure

B Li, Q Hu, Y Yang… - IET control theory & …, 2019 - Wiley Online Library
This work develops a novel disturbance observer and integral sliding mode technique
based fault tolerant attitude control scheme for spacecraft, which is subject to external …