A real time, three axis magnetic field simulator for nanosatellites, developed using only commercial off the shelf components, is described in the paper. It is a complete and independent system to be used for the ground testing of nanosatellites, allowing automated magnetic attitude control systems to be verified. The main aim of this simulator is to reproduce magnetic field conditions in orbit with low cost mechanical and electronic designs. The system is capable of creating an arbitrarily-oriented magnetic field on request for ground testing of 1U CubeSats or 3U CubeSats
With the surge of interest in nano-satellites, there is a concomitant need for high quality, yet aff...
The validation of the Attitude Determination and Control System (ADCS) of a satellite is essential f...
This paper presents the design of an attitude controller for a magnetically actuated nanosatellite. ...
A real time, three axis space magnetic field simulator, developed using only commercial, off-the-she...
This paper presents the design and development of a nanosatellite-scale spacecraft three-axis simula...
This work describes the development of a three degrees of freedom CubeSat attitude simulator testbed...
This work describes the development of a three degrees of freedom CubeSat attitude simulator testbed...
This work describes the development of a three degrees of freedom CubeSat attitude simulator testbed...
A miniaturized attitude control system suitable for nanosatellites, developed using only commercial ...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
The validation of the Attitude Determination and Control System (ADCS) of a satellite is essential f...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
Abstract: A description of the passive magnetic attitude control system of the TNS-0 №2 na...
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...
The validation of the Attitude Determination and Control System (ADCS) of a satellite is essential f...
This paper presents the design of an attitude controller for a magnetically actuated nanosatellite. ...
A real time, three axis space magnetic field simulator, developed using only commercial, off-the-she...
This paper presents the design and development of a nanosatellite-scale spacecraft three-axis simula...
This work describes the development of a three degrees of freedom CubeSat attitude simulator testbed...
This work describes the development of a three degrees of freedom CubeSat attitude simulator testbed...
This work describes the development of a three degrees of freedom CubeSat attitude simulator testbed...
A miniaturized attitude control system suitable for nanosatellites, developed using only commercial ...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
The validation of the Attitude Determination and Control System (ADCS) of a satellite is essential f...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
Abstract: A description of the passive magnetic attitude control system of the TNS-0 №2 na...
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...
The validation of the Attitude Determination and Control System (ADCS) of a satellite is essential f...
This paper presents the design of an attitude controller for a magnetically actuated nanosatellite. ...