Continuous finite-time attitude control for rigid spacecraft based on angular velocity observer

Q Hu, B Jiang - IEEE Transactions on Aerospace and Electronic …, 2017 - ieeexplore.ieee.org
This paper addresses the problem of designing an angular velocity observer and an output
feedback attitude controller with finite-time convergence and disturbances for spacecraft …

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 …

Observer-based output feedback attitude stabilization for spacecraft with finite-time convergence

Q Hu, B Jiang, Y Zhang - IEEE Transactions on Control …, 2017 - ieeexplore.ieee.org
This brief investigates the problem of finite-time output feedback control for spacecraft
attitude stabilization without angular velocity measurement. First, two new sufficient …

Actuator fault tolerant control using adaptive RBFNN fuzzy sliding mode controller for coaxial octorotor UAV

S Zeghlache, H Mekki, A Bouguerra, A Djerioui - ISA transactions, 2018 - Elsevier
In this paper, a robust controller for a Six Degrees of Freedom (6 DOF) coaxial octorotor
helicopter control is proposed in presence of actuator faults. Radial Base Function Neural …

Finite-time fault-tolerant trajectory tracking control of an autonomous surface vehicle

N Wang, X Pan, SF Su - Journal of the Franklin Institute, 2020 - Elsevier
In this paper, finite-time fault-tolerant control (FTC) for trajectory tracking of an autonomous
surface vehicle (ASV) is solved. Main contributions are summarized as follows:(1) a finite …

Auxiliary fault tolerant control with actuator amplitude saturation and limited rate

X Jin, J Qin, Y Shi, WX Zheng - IEEE Transactions on Systems …, 2017 - ieeexplore.ieee.org
In this paper, the problem of fault tolerant tracking control for a linear time-invariant system
subject to actuator faults and saturations is addressed. An auxiliary system is developed to …

Adaptive fixed-time attitude tracking control for rigid spacecraft with actuator faults

J Gao, Z Fu, S Zhang - IEEE Transactions on Industrial …, 2018 - ieeexplore.ieee.org
This paper investigates fixed-time attitude tracking maneuver of rigid spacecraft in the
presence of actuator faults, external disturbances, and inertia uncertainties. First, a fast finite …

Fault-tolerant attitude tracking control of combined spacecraft with reaction wheels under prescribed performance

X Huang, G Duan - ISA transactions, 2020 - Elsevier
Capture and control of a failed spacecraft can be achieved by a space manipulator installed
in a service spacecraft. After this target has been captured, the combined spacecraft must be …

Adaptive fixed‐time fault‐tolerant control for rigid spacecraft using a double power reaching law

M Tao, Q Chen, X He, M Sun - International Journal of Robust …, 2019 - Wiley Online Library
In this paper, an adaptive fixed‐time fault‐tolerant control scheme is presented for rigid
spacecraft with inertia uncertainties and external disturbances. By using an inverse …

Adaptive fuzzy fault-tolerant control of high-order nonlinear systems: A fully actuated system approach

Y Cui, G Duan, X Liu, H Zheng - International Journal of Fuzzy Systems, 2023 - Springer
An adaptive tracking control problem of high-order nonlinear strict-feedback system (SFS)
with non-affine nonlinear faults is considered in this paper. Based on high-order fully …