In this paper a new Attitude Control System is proposed, based on Control Moment
Gyroscopes (CMG). These actuators can provide unique torque, angular momentum and …

The satellite communication is embellished constantly by providing information, ensuring
security, and enables the communication among huge at a particular time efficiently. The …

A generic model of a nanosatellite attitude control and stabilization system was developed
on the basis of magnetorquers and reaction wheels, which are controlled by PID controllers …

The attitude-control problem of a rigid spacecraft containing a redundant set of reaction
wheels is investigated. Particularly with small spacecraft the available power is very limited …

Attitude estimation is a critical component of the Attitude Determination and Control System
(ADCS) of any satellite. It is used to convert the sensor observation data to an estimated …

Abstract SNAP-1 is the first 3-axis stabilised nanosatellite in orbit. The satellite is stabilised
by a single Ymomentum wheel and 3-axis magnetorquer rods, used for nutation damping …

The paper investigates the dynamic behavior of a spacecraft when a single magnetic torque-
rod is used for achieving a pure spin condition by means of the so-called Y-dot control law …

Purpose–The purpose of this paper is to present the development results of the overhaul
melioration plan for the following aircraft types: MiG‐21Bis, G‐4 Galeb and SA‐341 …

This paper presents the development of the attitude determination and control system
design of the Cyclone Global Navigation Satellite System spacecraft. The CYGNSS …

Magnetic attitude control methods for the REIMEI microsatellite are studied. The REIMEI
satellite is a 70 (kg) microsatellite and was launched in 2005. This satellite achieved …