The performance of the Attitude Determination and Control Subsystem (ADCS) of a CubeSat relies on consistent and robust inputs from sensors to provide the actuation to manoeuvre and stabilise the satellite orientation in space. This paper details the design and manufacture of a 1-axis motorised testbed to perform pre-flight ADCS functional testing of a nanosatellite based on the CubeSat Standard. This testbed has been developed to support the Educational Irish Research Satellite, EIRSAT-1, a 2U CubeSat being developed in University College Dublin (UCD) as part of the European Space Agency (ESA) Fly Your Satellite! (FYS!) Programme. EIRSAT-1 is a student led project to develop, build, test and launch Ireland's first satellite...
This paper describes the design, testing & performance characterization of a Reaction Wheel-based at...
The Velox-I, developed by Nanyang Technological University, is the first Singapore build nano-satell...
This paper describes the design, testing & performance characterization of a Reaction Wheel-based at...
The design and test of a 6U CubeSat Attitude Determination and Control System (ADCS) are explored to...
The 16th International Conference on Space Operations, Cape Town, South Africa, 3-5 May 2021The Cube...
The NTNU Test Satellite, NUTS, is a satellite being build in a student CubeSat project at the Norweg...
The compact, standardised form factor of CubeSats allows for the use of commercial off-the-shelf com...
In this paper, we present a test bench intended to test attitude control of 1U Cubesat...
In this paper, we present a test bench intended to test attitude control of 1U Cubesat...
In this paper, we present a test bench intended to test attitude control of 1U Cubesat...
One of the main difficulties in studying and testing cubesat attitude control systems is the lack of...
The Educational Irish Research Satellite, EIRSAT-1, is a project developed by students at University...
The validation of the Attitude Determination and Control System (ADCS) of a satellite is essential f...
The Educational Irish Research Satellite, EIRSAT-1, is a project developed by students at University...
The validation of the Attitude Determination and Control System (ADCS) of a satellite is essential f...
This paper describes the design, testing & performance characterization of a Reaction Wheel-based at...
The Velox-I, developed by Nanyang Technological University, is the first Singapore build nano-satell...
This paper describes the design, testing & performance characterization of a Reaction Wheel-based at...
The design and test of a 6U CubeSat Attitude Determination and Control System (ADCS) are explored to...
The 16th International Conference on Space Operations, Cape Town, South Africa, 3-5 May 2021The Cube...
The NTNU Test Satellite, NUTS, is a satellite being build in a student CubeSat project at the Norweg...
The compact, standardised form factor of CubeSats allows for the use of commercial off-the-shelf com...
In this paper, we present a test bench intended to test attitude control of 1U Cubesat...
In this paper, we present a test bench intended to test attitude control of 1U Cubesat...
In this paper, we present a test bench intended to test attitude control of 1U Cubesat...
One of the main difficulties in studying and testing cubesat attitude control systems is the lack of...
The Educational Irish Research Satellite, EIRSAT-1, is a project developed by students at University...
The validation of the Attitude Determination and Control System (ADCS) of a satellite is essential f...
The Educational Irish Research Satellite, EIRSAT-1, is a project developed by students at University...
The validation of the Attitude Determination and Control System (ADCS) of a satellite is essential f...
This paper describes the design, testing & performance characterization of a Reaction Wheel-based at...
The Velox-I, developed by Nanyang Technological University, is the first Singapore build nano-satell...
This paper describes the design, testing & performance characterization of a Reaction Wheel-based at...