In this paper, we present a test bench intended to test attitude control of 1U Cubesats. This platform, based in air bearing principle, is intended for educational purposes. It is designed according to the principles of modularity, low costs and usability. We have built the frame and the cubesat model using additive manufacturing techniques. Our design is affordable, easy to reproduce and based in COTS. We also present a basic 1U cubesat frame that fits inside a sphere, allowing a full 360º movement around all axis. The cubesat model is equipped with reaction wheels and manetorquers.</div
This paper describes the design and the manufacturing of a Cubesat realized within the activities of...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...
In this paper, the development of a performant and accurate Attitude Determination and Control Syste...
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 current process to learn CubeSat controls is vastly conceptual for students from the high school...
The purpose of this research project is to build an educational spacecraft platform to enable anyone...
The performance of the Attitude Determination and Control Subsystem (ADCS) of a CubeSat relies on co...
A cubesat attitude control system (ACS) was designed at the NASA Marshall Space Flight Center (MSFC)...
This paper describes the design, testing & performance characterization of a Reaction Wheel-based at...
This work describes the development of a three degrees of freedom CubeSat attitude simulator testbed...
With the surge of interest in nano-satellites, there is a concomitant need for high quality, yet aff...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...
© COPYRIGHT SPIE. Downloading of the abstract is permitted for personal use only. CubeSat technology...
We present a satellite attitude control system design using low-cost hardware and software for a 1U ...
This paper describes the design and the manufacturing of a Cubesat realized within the activities of...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...
In this paper, the development of a performant and accurate Attitude Determination and Control Syste...
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 current process to learn CubeSat controls is vastly conceptual for students from the high school...
The purpose of this research project is to build an educational spacecraft platform to enable anyone...
The performance of the Attitude Determination and Control Subsystem (ADCS) of a CubeSat relies on co...
A cubesat attitude control system (ACS) was designed at the NASA Marshall Space Flight Center (MSFC)...
This paper describes the design, testing & performance characterization of a Reaction Wheel-based at...
This work describes the development of a three degrees of freedom CubeSat attitude simulator testbed...
With the surge of interest in nano-satellites, there is a concomitant need for high quality, yet aff...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...
© COPYRIGHT SPIE. Downloading of the abstract is permitted for personal use only. CubeSat technology...
We present a satellite attitude control system design using low-cost hardware and software for a 1U ...
This paper describes the design and the manufacturing of a Cubesat realized within the activities of...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...
In this paper, the development of a performant and accurate Attitude Determination and Control Syste...