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NASA Operational Simulator for Small Satellites (NOS3): the STF-1 CubeSat case study

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 Added by Max Spolaor
 Publication date 2019
  fields Physics
and research's language is English




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One of the primary objectives of small satellites is to reduce the costs associated with spacecraft development and operations as compared to traditional spacecraft missions. Small satellite missions are generally able to reduce mission planning, hardware, integration, and operational costs; however, small satellite missions struggle with reducing software development and testing costs. This paper presents the case study of the NASA Operational Simulator for Small Satellites (NOS3), a software-only simulation framework that was developed for the Simulation-to-Flight 1 (STF-1) 3U CubeSat mission. The general approach is to develop software simulators for the various hardware flight components (e.g., electrical power system, antenna deployment system, etc.) to create a completely virtual representation of the actual spacecraft system. In addition, NOS3 conveniently packages together a set of open-source software packages including the 42 dynamics simulator, the spacecraft software development framework (core Flight System), and a command and control system (COSMOS). This results in a flexible and easily deployable simulation environment that can be utilized to support software development, testing, training, and mission operations. The NOS3 environment contributed to the success of STF-1 mission in several ways, such as reducing the missions reliance on hardware, increasing available test resources, and supporting training and risk reduction targeted testing of critical software behaviors on the simulated platform. The NOS3 has been released as open-source and is available at www.nos3.org.



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