Small satellite missions are becoming increasingly complex as scientists and engineers propose to utilize them to accomplish more ambitious science and technology goals. Small satellites such as CubeSats are challenging to design because they have limited resources, coupled subsystems, and must operate in dynamic environments.
Integrated model-based systems engineering (MBSE) applied to the Simulation of a CubeSat mission
2014-03-01
5008609 byte
Conference paper
Electronic Resource
English