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This paper discusses the design and verification of the operating procedure of the Attitude Determination and Control Subsystem (ADCS) of PHOENIX nanosatellite. As one of the satellites which joins the QB50 project, the main objective of PHOENIX is to perform in-situ measurements in the lower thermosphere. In order to meet the mission requirements, the attitude control system is required to stabilize...
PHOENIX satellite is a 2kg CubeSat that is being developed as a part of the FP7 international QB50 project. QB50 is an international network of 50 CubeSats for multi-point, in-situ measurements in the largely-unexplored lower thermosphere and for re-entry research. The CubeSat constellation will be launched in the first half of 2015 into a circular orbit at 320 km altitude, inclination 79°. A unique...
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