Model-free active input–output feedback linearization of a single-link flexible joint manipulator: An improved active disturbance rejection control approach
WR Abdul-Adheem, IK Ibraheem… - Measurement and …, 2021 - journals.sagepub.com
Traditional input–output feedback linearization requires full knowledge of system dynamics
and assumes no disturbance at the input channel and no system's uncertainties. In this …
and assumes no disturbance at the input channel and no system's uncertainties. In this …
Disturbance observer-based control for small nonlinear UAV systems with transient performance constraint
J Chen, R Sun, B Zhu - Aerospace Science and Technology, 2020 - Elsevier
Small UAVs are a class of nonlinear systems with unknown dynamics and uncertainties.
This paper proposes a disturbance observer-based (DOB) control scheme with transient …
This paper proposes a disturbance observer-based (DOB) control scheme with transient …
Attitude stabilization of spacecraft simulator based on modified constrained feedback linearization model predictive control
M Khodaverdian, M Malekzadeh - IET Control Theory & …, 2023 - Wiley Online Library
This paper aims to discuss the approach of constrained modified feedback linearization
model predictive control for the spacecraft simulator. By utilizing the high accuracy and …
model predictive control for the spacecraft simulator. By utilizing the high accuracy and …
Applied nonlinear control of spacecraft simulator with constraints on torque and momentum of reaction wheels
In this paper, the attitude of a spacecraft simulator is controlled in the presence of
nonlinearities, uncertainties and constraints of the system. An optimization-based controller …
nonlinearities, uncertainties and constraints of the system. An optimization-based controller …
Super‐Twisting Sliding Mode Control Law Design for Attitude Tracking Task of a Spacecraft via Reaction Wheels
The attitude control has been recognized as one of the most important research topics for
spacecraft. If the desired attitude trajectory cannot be tracked precisely, it may cause mission …
spacecraft. If the desired attitude trajectory cannot be tracked precisely, it may cause mission …
A multi-index feedback linearization control for a buck-boost converter
X Li, X Chen - Energies, 2021 - mdpi.com
Due to the nonlinear and nonminimum phase characteristics of the buck-boost converter, the
design of its controller has always been a challenging problem. In this paper, a multi-index …
design of its controller has always been a challenging problem. In this paper, a multi-index …
Modeling and control of a nonlinear coupled spacecraft-fuel system
M Navabi, A Davoodi, M Reyhanoglu - Acta Astronautica, 2019 - Elsevier
This paper considers the nonlinear interaction of the rigid body dynamics of a spacecraft
with the sloshing dynamics of the liquid propellant in its partially filled spherical tank during …
with the sloshing dynamics of the liquid propellant in its partially filled spherical tank during …
A Multiobjective Feedback Linearization Control of a Cuk Converter
D Chen, X Hu - IEEE Journal of Emerging and Selected Topics …, 2023 - ieeexplore.ieee.org
Cuk converter is one of the most common power electronic converters, but its controller
design has always been a challenging problem due to its fourth-order nonlinear and …
design has always been a challenging problem due to its fourth-order nonlinear and …
Feedback linearization-based satellite attitude control with a life-support device without communications
A Giuseppi, A Pietrabissa, S Cilione… - control engineering …, 2019 - Elsevier
This paper develops a control strategy for a life-support device to be attached to an orbiting
satellite to extend its operational life. The objective is met in such a way that the original …
satellite to extend its operational life. The objective is met in such a way that the original …
Comparison of various control techniques applied to a quadcopter
M Merzban, AAM Khalaf, HFA Hamed - Journal of Advanced …, 2023 - journals.ekb.eg
A quadcopter is considered one of the most well-known examples of unmanned aerial
vehicles (UAVS), because it has more advantages than standard helicopter in terms of size …
vehicles (UAVS), because it has more advantages than standard helicopter in terms of size …