This study surveys the developments in the gyroless attitude determination system,
especially for small satellites. Two kinds of gyroless satellite attitude determination …

Attitude motion of a satellite equipped with magnetic control system is considered. System
comprises of three magnetorquers and one three-axis magnetometer. Satellite is stabilized …

An algorithm of satellite formation flying control in the Low-Earth Orbit using the
aerodynamic force is considered. A simple model of the aerodynamic force that takes into …

Precise attitude tracking control of small satellites is a demanding task due to the limited
hardware resources of sensors, actuators, and processors equipped on board. Moreover …

Искусственные спутники Земли практически всегда оснащены системой ориентации
для обеспечения требуемого углового движения вокруг своего центра масс. В связи с …

This paper deals with the design, realization, and testing of an earth magnetic field
simulator, which allows us to validate hardware-in-the-loop algorithms, as well as to test new …

This paper proposed a new attitude determination method for low-orbit spacecraft. The
attitude prediction accuracy is greatly improved by adding the unmodeled environmental …

Advanced missions of satellites are increasingly demanding more accurate and robust
attitude maneuvering capabilities. However, it is difficult to achieve especially for small …

An analytical approach to study of attitude determination algorithms is considered. The
approach is applicable for quasi-stationary motion determination. It is based on filter post …

This paper is dedicated to the attitude control law synthesis for GRACE-like missions.
Namely, two satellites move along the same orbit at a distance of several hundred …