Turnitin
降AI改写
早检测系统
早降重系统
Turnitin-UK版
万方检测-期刊版
维普编辑部版
Grammarly检测
Paperpass检测
checkpass检测
PaperYY检测
Review of advanced guidance and control algorithms for space/aerospace vehicles
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 …
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 …
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 …
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
This paper proposes an Incremental Sliding Mode Control driven by Sliding Mode
Disturbance Observers (INDI-SMC/SMDO), with application to a quadrotor fault tolerant …
Disturbance Observers (INDI-SMC/SMDO), with application to a quadrotor fault tolerant …
Appointed-time prescribed performance attitude tracking control via double performance functions
This work investigates the attitude tracking control problem of spacecraft under strong
external disturbances and parameter uncertainties. A novel appointed-time stable control …
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 …
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
This paper investigates the composite control scheme of robust nonlinear disturbance
observer (RNDO) with adaptive non-singular fast terminal sliding mode control (NSFTSMC) …
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 …
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
In this paper, the attitude stabilization and tracking control problem is investigated for
spacecraft with consideration of unknown dynamics and external disturbance. A low …
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 …
control for rigid spacecraft is investigated. Firstly, a finite-time attitude controller combined …