Adaptive sliding mode fault tolerant attitude tracking control for flexible spacecraft under actuator saturation

B Xiao, Q Hu, Y Zhang - IEEE Transactions on Control Systems …, 2011 - ieeexplore.ieee.org
A novel fault tolerant attitude tracking control scheme is developed for flexible spacecraft
with partial loss of actuator effectiveness fault. Neural networks are first introduced to …

Fixed-time attitude tracking control for spacecraft with input quantization

H Sun, L Hou, G Zong, X Yu - IEEE Transactions on Aerospace …, 2018 - ieeexplore.ieee.org
This paper investigates the fixed-time attitude tracking control problem for rigid spacecraft
with input quantization and external disturbances. A novel fixed-time disturbance observer is …

Fault-tolerant tracking control of spacecraft with attitude-only measurement under actuator failures

B Xiao, Q Hu, Y Zhang, X Huo - Journal of Guidance, Control, and …, 2014 - arc.aiaa.org
This paper investigates the velocity-measurement-free feedback control problem associated
with attitude tracking for a rigid spacecraft in the presence of both actuator failures and …

Fault-tolerant attitude control for rigid spacecraft without angular velocity measurements

X Wang, CP Tan, F Wu, J Wang - IEEE Transactions on …, 2019 - ieeexplore.ieee.org
In this paper, a fault-tolerant control scheme is proposed for the rigid spacecraft attitude
control system subject to external disturbances, multiple system uncertainties, and actuator …

A structure simple controller for satellite attitude tracking maneuver

B Xiao, S Yin, L Wu - IEEE Transactions on Industrial …, 2016 - ieeexplore.ieee.org
This paper addresses a difficult problem of designing a control approach with simple
structure to perform attitude tracking maneuver for rigid satellites. The satellite is subject to …

Fuzzy adaptive fault-tolerant output feedback attitude-tracking control of rigid spacecraft

B Huo, Y Xia, L Yin, M Fu - IEEE Transactions on Systems, Man …, 2016 - ieeexplore.ieee.org
This paper proposes a stable adaptive fuzzy fault-tolerant attitude-tracking controller for a
rigid spacecraft in the presence of unavailable velocities, external disturbance, actuator …

Generalized multi-kernel maximum correntropy Kalman filter for disturbance estimation

S Li, D Shi, Y Lou, W Zou, L Shi - IEEE Transactions on …, 2023 - ieeexplore.ieee.org
Disturbance observers have been attracting continuing research efforts and are widely used
in many applications. Among them, the Kalman filter-based disturbance observer is an …

Finite-time output feedback attitude control for spacecraft using “Adding a power integrator” technique

B Jiang, C Li, G Ma - Aerospace Science and Technology, 2017 - Elsevier
This paper investigates the problem of finite-time output feedback control for spacecraft
attitude stabilization with attitude-only measurement. First, a finite-time filter is proposed to …

Robust attitude control design for spacecraft under assigned velocity and control constraints

Q Hu, B Li, Y Zhang - ISA transactions, 2013 - Elsevier
A novel robust nonlinear control design under the constraints of assigned velocity and
actuator torque is investigated for attitude stabilization of a rigid spacecraft. More specifically …

Attitude stabilization control of flexible satellites with high accuracy: An estimator-based approach

B Xiao, S Yin, O Kaynak - IEEE/ASME Transactions on …, 2016 - ieeexplore.ieee.org
This paper presents a novel nonlinear control approach for attitude stabilization of flexible
satellites. It is developed by using a nonlinear estimator technique. An estimator is proposed …