In this paper, a low-cost, miniature spacecraft attitude control simulator is presented for testing miniature actuators such as Nano Control Moment Gyroscopes (CMGs) for simple maneuvers. The experimental setup is composed by an attitude control system (ACS) that mainly consists of a four-CMG cluster in a pyramid configuration and a custom-made air bearing. The one-degree-of-freedom (DoF) air bearing is fabricated to reproduce the frictionless conditions of a nano-satellite in orbit. The ACS is made exclusively using low-cost commercial-off-the-shelf (COTS) components, whilst the air bearing is made using 3D-printed parts. Both hardware and software implementations are described in detail and the performance of the developed simulator is ev...
This study presents two unique ideas in manoeuvring nano-satellites. Both ideas make use of the theo...
This paper presents the design as well as characterization of a practical control moment gyroscope (...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
With the surge of interest in nano-satellites, there is a concomitant need for high quality, yet aff...
Abstract: In this paper a new practical Attitude Control System is proposed, based on Control Momen...
The primary aim of this project is to design a Control Moment Gyroscope (CMG) prototype for single a...
The primary aim of this project is to design a Control Moment Gyroscope (CMG) prototype for single a...
© 2015 IEEE. Attitude control of a spacecraft is critical for its operations, but at the same time p...
A real time, three axis magnetic field simulator for nanosatellites, developed using only commercial...
The use of satellite simulators have enhanced in recent years. Each organization anduniversity uses ...
The use of satellite simulators have enhanced in recent years. Each organization anduniversity uses ...
The use of satellite simulators have enhanced in recent years. Each organization anduniversity uses ...
A spacecraft formation possesses several benefits over a single-satellite mission. How-ever, launchi...
Utah State University has developed an air bearing table to simulate the attitude dynamics of a smal...
To simulate the conditions of the space environment at ground, the Laboratory of Application and Inn...
This study presents two unique ideas in manoeuvring nano-satellites. Both ideas make use of the theo...
This paper presents the design as well as characterization of a practical control moment gyroscope (...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
With the surge of interest in nano-satellites, there is a concomitant need for high quality, yet aff...
Abstract: In this paper a new practical Attitude Control System is proposed, based on Control Momen...
The primary aim of this project is to design a Control Moment Gyroscope (CMG) prototype for single a...
The primary aim of this project is to design a Control Moment Gyroscope (CMG) prototype for single a...
© 2015 IEEE. Attitude control of a spacecraft is critical for its operations, but at the same time p...
A real time, three axis magnetic field simulator for nanosatellites, developed using only commercial...
The use of satellite simulators have enhanced in recent years. Each organization anduniversity uses ...
The use of satellite simulators have enhanced in recent years. Each organization anduniversity uses ...
The use of satellite simulators have enhanced in recent years. Each organization anduniversity uses ...
A spacecraft formation possesses several benefits over a single-satellite mission. How-ever, launchi...
Utah State University has developed an air bearing table to simulate the attitude dynamics of a smal...
To simulate the conditions of the space environment at ground, the Laboratory of Application and Inn...
This study presents two unique ideas in manoeuvring nano-satellites. Both ideas make use of the theo...
This paper presents the design as well as characterization of a practical control moment gyroscope (...
Attitude control of a satellite is required for the pointing of communications antennas and other in...