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 …

UAV vision aided INS/odometer integration for land vehicle autonomous navigation

J Dong, X Ren, S Han, S Luo - IEEE Transactions on Vehicular …, 2022 - ieeexplore.ieee.org
Autonomous navigation without external GNSS aiding is crucial for some kinds of land
vehicle applications, such as military vehicles and unmanned vehicles navigation under …

[图书][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 …

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 …

[HTML][HTML] Robust optimal adaptive trajectory tracking control of quadrotor helicopter

M Navabi, H Mirzaei - Latin American Journal of solids and structures, 2017 - SciELO Brasil
This paper focuses on robust optimal adaptive control strategy to deal with tracking problem
of a quadrotor unmanned aerial vehicle (UAV) in presence of parametric uncertainties …

Robust attitude control using a double-gimbal variable-speed control moment gyroscope

T Sasaki, T Shimomura, H Schaub - Journal of Spacecraft and Rockets, 2018 - arc.aiaa.org
This paper derives a linear parameter-varying (LPV) model for three-axis attitude control of a
spacecraft with a single double-gimbal variable-speed control moment gyroscope …

Spacecraft quaternion based attitude input-output feedback linearization control using reaction wheels

M Navabi, MR Hosseini - 2017 8th International conference on …, 2017 - ieeexplore.ieee.org
The aim of this paper is attitude control of spacecraft utilizing nonlinear control feedback
linearization. Input-output linearization is a technique of feedback linearization theory. In this …

An orientation estimation strategy for low cost IMU using a nonlinear Luenberger observer

DA Aligia, BA Roccia, CH De Angelo, GA Magallan… - Measurement, 2021 - Elsevier
In this work a new orientation estimation strategy for a non-accelerated platform is
presented. The proposed strategy is based on a low-cost inertial measurement unit (IMU) …

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 …

Biplanar coils design for spatial nonlinear magnetic fields using an enhanced target field method

S Yuan, P Cui, M Shi, X Zhang, J Yang… - Journal of Physics D …, 2024 - iopscience.iop.org
The demand for spatial nonlinear magnetic fields (SNMF) spans diverse domains,
encompassing medical applications like drug transportation and aerospace applications …