Add to ORKGThe aim of the project was to design a CubeSat control unit. The board is composed of commercial parts yet reliable in the space environment. Because of its benefits, an FPGA was selected as the core of the board. The FPGA is periodically checked for errors and reset if an error is found. The unit has various sensors to monitor its condition and can do necessary measures. Two MRAMs allow to store a golden bitstream and upload new bitstream in flight
The CUBES (CUbesat x-ray Background Explorer using Scintillators) is a payload on the KTH student sa...
El objetivo final de este proyecto es diseñar una PCB orientada al control de estabilidad de un Cub...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...
CubeSat missions needs components that are tolerant against the radiation in space. The hardware com...
This thesis discusses the integration of the subsystems in a CubeSat satellite and the implementatio...
This thesis describes the development of the Attitude Determination and Control System (ADCS) for Cu...
Cílem práce je návrh univerzální řídicí jednotky pro CubeSat založené na obvodu FPGA. Taková jednotk...
BeaverCube is a 3U CubeSat in development by the Space Systems Development capstone class and STARLa...
Over the past decade, the satellite industry has witnessed the birth and evolution of the CubeSat st...
One of the challenges to date for operational spacecrafts is to satisfy high attitude pointing accur...
CubeSat attitude control systems must be compact, fast, and accurate to achieve success in space mis...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...
The definition of the CubeSat standard boosted the research and development of the pico and nano sate...
his document reports the process of design, implementation, and testing of an On-Board Computer for ...
CubeSats enable low-cost experiment and missions to be performed by universities and research instit...
The CUBES (CUbesat x-ray Background Explorer using Scintillators) is a payload on the KTH student sa...
El objetivo final de este proyecto es diseñar una PCB orientada al control de estabilidad de un Cub...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...
CubeSat missions needs components that are tolerant against the radiation in space. The hardware com...
This thesis discusses the integration of the subsystems in a CubeSat satellite and the implementatio...
This thesis describes the development of the Attitude Determination and Control System (ADCS) for Cu...
Cílem práce je návrh univerzální řídicí jednotky pro CubeSat založené na obvodu FPGA. Taková jednotk...
BeaverCube is a 3U CubeSat in development by the Space Systems Development capstone class and STARLa...
Over the past decade, the satellite industry has witnessed the birth and evolution of the CubeSat st...
One of the challenges to date for operational spacecrafts is to satisfy high attitude pointing accur...
CubeSat attitude control systems must be compact, fast, and accurate to achieve success in space mis...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...
The definition of the CubeSat standard boosted the research and development of the pico and nano sate...
his document reports the process of design, implementation, and testing of an On-Board Computer for ...
CubeSats enable low-cost experiment and missions to be performed by universities and research instit...
The CUBES (CUbesat x-ray Background Explorer using Scintillators) is a payload on the KTH student sa...
El objetivo final de este proyecto es diseñar una PCB orientada al control de estabilidad de un Cub...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...