It is well known that one critical step in a space project life cycle is to demonstrate the qualification of design and performance to meet the requirements at the specified levels.
In this context, the LODESTAR Small Sat Simulator division was created with the aim of providing infrastructure and methods for validation testing to measure product performance and functions under a representative environment. It is focused on safety-critical and mission-critical features in system, subsystem, and equipment levels.
The main application currently under development is dedicated to attitude determination and control of small satellites, take a moment to check it, and welcome to be part of it!