Disturbance observer-based quadrotor attitude tracking control for aggressive maneuvers

A Castillo, R Sanz, P Garcia, W Qiu, H Wang… - Control Engineering …, 2019 - Elsevier
In this paper, a disturbance observer-based quadrotor attitude controller for aggressive
maneuvering is presented. The controller is made up of the cascade connection between …

Nonlinear adaptive pose motion control of a servicer spacecraft in approximation with an accelerated tumbling target

A Kasiri, F Fani Saberi - Scientific Reports, 2024 - nature.com
Removing a limited number of large debris can significantly reduce space debris risks.
These bodies are generally exposed to extreme environmental disturbance torques or …

Dual-rate-loop control based on disturbance observer of angular acceleration for a three-axis aerial inertially stabilized platform

X Zhou, Y Jia, Q Zhao, T Cai - ISA transactions, 2016 - Elsevier
This paper presents a dual-rate-loop control method based on disturbance observer (DOB)
of angular acceleration for a three-axis ISP for aerial remote sensing applications, by which …

A hybrid control scheme for attitude and vibration suppression of a flexible spacecraft using energy-based actuators switching mechanism

M Azimi, G Sharifi - Aerospace Science and Technology, 2018 - Elsevier
A novel energy-based switching logic scenario to design a hybrid thruster/reaction wheel
(RW) system is investigated for active vibration suppression of a flexible spacecraft …

Velocity-free attitude coordinated tracking control for spacecraft formation flying

Q Hu, J Zhang, Y Zhang - ISA transactions, 2018 - Elsevier
This article investigates the velocity-free attitude coordinated tracking control scheme for a
group of spacecraft with the assumption that the angular velocities of the formation members …

Control of rotary inverted pendulum by using on–off type of cold gas thrusters

Y Silik, U Yaman - Actuators, 2020 - mdpi.com
This article describes the control of a rotary inverted pendulum utilizing on–off-type cold gas
thrusters as the actuators, which have high similarities with thruster actuated spacecrafts …

A study of spacecraft reaction thruster configurations for attitude control system

M Pasand, A Hassani… - IEEE Aerospace and …, 2017 - ieeexplore.ieee.org
Reaction thrusters (RTs) are used as an alternative to momentum exchange devices when
disturbance torques exceed the control authority of momentum exchange devices. The …

A novel body frame based approach to aerospacecraft attitude tracking

C Ma, MZQ Chen, J Lam, KC Cheung - ISA transactions, 2017 - Elsevier
In the common practice of designing an attitude tracker for an aerospacecraft, one
transforms the Newton-Euler rotation equations to obtain the dynamic equations of some …

Robust adaptive relative position and attitude control for spacecraft autonomous proximity

L Sun, W Huo, Z Jiao - ISA transactions, 2016 - Elsevier
This paper provides new results of the dynamical modeling and controller designing for
autonomous close proximity phase during rendezvous and docking in the presence of …

Design and evaluation of thruster control approach for micro-satellite ale-2

Y Sato, S Fujita, T Kuwahara, Y Shibuya… - 2020 IEEE/SICE …, 2020 - ieeexplore.ieee.org
This paper provides the thruster control approach for micro-satellites to realize autonomous
orbit and attitude control. The Space Robotics Laboratory (SRL) of Tohoku University and …