Add to ORKGThis project handled the design and analysis of the attitude determination and control, command and data handling, and structural subsystems of CubeSats designed for two distinct missions. One mission was to fly a CubeSat in extreme low earth orbit, while the other was to fly two CubeSats in formation. Attitude sensors and an onboard computer selected in previous years designs were reviewed and updated. Structural analysis simulations were conducted in ANSYS. Additionally, the test bed for an attitude determination and control system experiment designed and constructed by the students in MAD-1701 was improved upon, and an attitude control system was designed. Finally, recommendations were provided for future teams looking to further develop...
This project presents design and analysis for a 6-unit CubeSat carrying a miniaturized mass spectrom...
The possibility of a low-cost alternative to conventional micro-gravity testbeds used to design, tes...
The primary purpose of an Earth observing spacecraft constellation is to obtain global measurements ...
A cubesat attitude control system (ACS) was designed at the NASA Marshall Space Flight Center (MSFC)...
Guidance, navigation, and control (GNC) systems are commonly found in vehicles, whether they be spac...
The attitude determination and control system (ADCS) for a satellite is responsible for multiple key...
Over the last year, Cal Poly Pomona has made a significant push to become a consistent space-faring ...
In the fall of 2016, the NASA Science Mission Directorate, working with the Virginia Space Grant Con...
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 importance of small satellites, and in particular of nano-satellites (e.g. CubeSats) has increas...
textA guidance, navigation, and control (GN&C) module is being designed and fabricated as part of a ...
textA guidance, navigation, and control (GN&C) module is being designed and fabricated as part of a ...
This project describes the development of the attitude determination and control, on board computing...
A cubesat attitude control system (ACS) was designed at the NASA Marshall Space Flight Center (MSFC)...
This project presents design and analysis for a 6-unit CubeSat carrying a miniaturized mass spectrom...
The possibility of a low-cost alternative to conventional micro-gravity testbeds used to design, tes...
The primary purpose of an Earth observing spacecraft constellation is to obtain global measurements ...
A cubesat attitude control system (ACS) was designed at the NASA Marshall Space Flight Center (MSFC)...
Guidance, navigation, and control (GNC) systems are commonly found in vehicles, whether they be spac...
The attitude determination and control system (ADCS) for a satellite is responsible for multiple key...
Over the last year, Cal Poly Pomona has made a significant push to become a consistent space-faring ...
In the fall of 2016, the NASA Science Mission Directorate, working with the Virginia Space Grant Con...
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 importance of small satellites, and in particular of nano-satellites (e.g. CubeSats) has increas...
textA guidance, navigation, and control (GN&C) module is being designed and fabricated as part of a ...
textA guidance, navigation, and control (GN&C) module is being designed and fabricated as part of a ...
This project describes the development of the attitude determination and control, on board computing...
A cubesat attitude control system (ACS) was designed at the NASA Marshall Space Flight Center (MSFC)...
This project presents design and analysis for a 6-unit CubeSat carrying a miniaturized mass spectrom...
The possibility of a low-cost alternative to conventional micro-gravity testbeds used to design, tes...
The primary purpose of an Earth observing spacecraft constellation is to obtain global measurements ...