Review of advanced guidance and control algorithms for space/aerospace vehicles

R Chai, A Tsourdos, A Savvaris, S Chai, Y **a… - Progress in Aerospace …, 2021 - Elsevier
The design of advanced guidance and control (G&C) systems for space/aerospace vehicles
has received a large amount of attention worldwide during the last few decades and will …

Magnetic bearing: structure, model, and control strategy

Z Huang, C Li, Z Zhou, B Liu, Y Zhang, M Yang… - … International Journal of …, 2024 - Springer
Bearings are pivotal components in mechanical systems, providing crucial support to
rotating bodies. However, traditional bearings are susceptible to failure caused by friction …

Faster fixed-time control of flexible spacecraft attitude stabilization

L Cao, B **ao, M Golestani… - IEEE Transactions on …, 2019 - ieeexplore.ieee.org
The rapid attitude stabilization problem of flexible spacecraft with uncertain inertia and
disturbances is investigated. In this article, a sliding mode-based fixed-time control approach …

Quadrotor fault tolerant incremental sliding mode control driven by sliding mode disturbance observers

X Wang, S Sun, EJ van Kampen, Q Chu - Aerospace Science and …, 2019 - Elsevier
This paper proposes an Incremental Sliding Mode Control driven by Sliding Mode
Disturbance Observers (INDI-SMC/SMDO), with application to a quadrotor fault tolerant …

Appointed-time prescribed performance attitude tracking control via double performance functions

Z Yin, A Suleman, J Luo, C Wei - Aerospace science and technology, 2019 - Elsevier
This work investigates the attitude tracking control problem of spacecraft under strong
external disturbances and parameter uncertainties. A novel appointed-time stable control …

Active adaptive continuous nonsingular terminal sliding mode controller for hypersonic vehicle

R Guo, Y Ding, X Yue - Aerospace Science and Technology, 2023 - Elsevier
An active adaptive continuous nonsingular terminal sliding mode algorithm (ACNTSM) is
designed for hypersonic boost glide vehicle to achieve higher control accuracy and faster …

Finite-time fault tolerant attitude tracking control of spacecraft using robust nonlinear disturbance observer with anti-unwinding approach

SM Amrr, M Nabi - Advances in Space Research, 2020 - Elsevier
This paper investigates the composite control scheme of robust nonlinear disturbance
observer (RNDO) with adaptive non-singular fast terminal sliding mode control (NSFTSMC) …

Anti-unwinding sliding mode attitude maneuver control for rigid spacecraft

RQ Dong, AG Wu, Y Zhang - IEEE Transactions on Automatic …, 2021 - ieeexplore.ieee.org
In this article, anti-unwinding attitude maneuver control for rigid spacecraft is considered.
First, in order to avoid the unwinding phenomenon when the system states are restricted to …

Low-complexity prescribed performance control for spacecraft attitude stabilization and tracking

J Luo, Z Yin, C Wei, J Yuan - Aerospace Science and Technology, 2018 - Elsevier
In this paper, the attitude stabilization and tracking control problem is investigated for
spacecraft with consideration of unknown dynamics and external disturbance. A low …

Finite-time sliding mode attitude control for rigid spacecraft without angular velocity measurement

S Shao, Q Zong, B Tian, F Wang - Journal of the Franklin Institute, 2017 - Elsevier
The continuous finite-time nonsingular terminal sliding mode (NTSM) attitude tracking
control for rigid spacecraft is investigated. Firstly, a finite-time attitude controller combined …