A survey on active magnetic attitude control algorithms for small satellites
MY Ovchinnikov, DS Roldugin - Progress in Aerospace Sciences, 2019 - Elsevier
Control algorithms for the active magnetic attitude control systems are covered in the survey.
Three different situations in the magnetic system implementation are considered. First …
Three different situations in the magnetic system implementation are considered. First …
Fault-Tolerant Control of Time-Delay Markov Jump Systems With Stochastic Process and Output Disturbance Based on Sliding Mode Observer
This paper focuses on the fault-tolerant control problem of Markov jump systems (MJS) with
Itô stochastic process and output disturbances. Such a problem widely exists in practical …
Itô stochastic process and output disturbances. Such a problem widely exists in practical …
Developments of attitude determination and control system of microsats: A survey
L He, W Ma, P Guo, T Sheng - … Part I: Journal of Systems and …, 2021 - journals.sagepub.com
This study surveys the developments in satellite attitude determination and control system,
especially for microsats. This survey is not intended to be complete but is limited to the most …
especially for microsats. This survey is not intended to be complete but is limited to the most …
[BOOK][B] Spacecraft modeling, attitude determination, and control: quaternion-based approach
Y Yang - 2019 - taylorfrancis.com
This book discusses all spacecraft attitude control-related topics: spacecraft (including
attitude measurements, actuator, and disturbance torques), modeling, spacecraft attitude …
attitude measurements, actuator, and disturbance torques), modeling, spacecraft attitude …
Magnetorquers-based satellite attitude control using interval type-II fuzzy terminal sliding mode control with time delay estimation
H Yadegari, J Beyramzad, E Khanmirza - Advances in Space Research, 2022 - Elsevier
This paper presents a novel robust attitude controller for satellite applications with magnetic
actuation. First, at the kinematical level, a terminal sliding mode (TSM)-based sliding surface …
actuation. First, at the kinematical level, a terminal sliding mode (TSM)-based sliding surface …
Robust and global attitude stabilization of magnetically actuated spacecraft through sliding mode
The inertial pointing problem of a rigid satellite by solely magnetic torqueing is considered in
this paper. To ensure globally uniformly ultimately bounded motion about the reference in …
this paper. To ensure globally uniformly ultimately bounded motion about the reference in …
Novel approach to attitude stabilization of satellite using geomagnetic Lorentz forces
VI Kalenova, VM Morozov - Aerospace Science and Technology, 2020 - Elsevier
A satellite in a circular Earth orbit is under consideration. The three–axis stabilization of the
satellite in orbital coordinate system with the attitude control system using moments of …
satellite in orbital coordinate system with the attitude control system using moments of …
Application of the PSO for the construction of a 3-axis stable magnetically actuated satellite angular motion
A Okhitina, D Roldugin, S Tkachev - Acta Astronautica, 2022 - Elsevier
Particle swarm optimization (PSO) is a non-gradient biologically inspired global optimization
method. It utilizes direct calculation of the optimized cost function during the numerical …
method. It utilizes direct calculation of the optimized cost function during the numerical …
Controllability of spacecraft attitude using control moment gyroscopes
SP Bhat, PK Tiwari - IEEE transactions on Automatic Control, 2009 - ieeexplore.ieee.org
This technical note describes an application of nonlinear controllability theory to the problem
of spacecraft attitude control using control moment gyroscopes (CMGs). Nonlinear …
of spacecraft attitude control using control moment gyroscopes (CMGs). Nonlinear …
Satellite control using magnetic moments: controllability and stabilization algorithms
VM Morozov, VI Kalenova - Cosmic Research, 2020 - Springer
The stabilization of the relative equilibrium of a satellite moving in a circular orbit, which is
equipped with magnetic orientation system. It is shown that the linearized system of …
equipped with magnetic orientation system. It is shown that the linearized system of …