![]() ![]() This paper details the design and the structural analysis of a Control Moment Gyroscope (CMG) actuator for agile CubeSats with a physical size up to 12U, which require high torque actuators. CubeSats are standardized small size satellites based on 10 × 10 × 10 cm cube modules (1U) and are becoming sophisticated platforms despite their very small size. Following a global trend towards miniaturization, the population of nano- and micro-satellite continues to increase.
0 Comments
Leave a Reply. |