F' and establishing a connection between ground and satellite on orbit. #735
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Per the cubesat spec no power is allowed to flow on the satellite before deployment from the launch vehicle. Most cubesats have deployment switches on the rails that cause the flight computer to boot on seperation from the deployer. There also may be launch vehicle requirements that prevent radio transmissions until some time after deployment.
For a cubesat you usually replace the TCP/IP communication driver with a radio driver and route all ground interface traffic out over the radio. The F' GDS is mostly intended for development and testing and not so much for actual operations. The assumption is that users select and integrate a full scale GDS solution for actual operations. However, the F' GDS could be used potentially be used if you wrote an plugin to interface with your ground station. |
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This might be a stupid question and might not be 100% related to F'. Let's say I want to launch a generic cubesat with flight software developed on F' framework to LEO.
1.) Should the flight software start running before the launch or once it separate from the launch vehicle or any moment in between?
2.) was I correct to assume that once I have the ground station set up, I should know the ip address of that satellite on orbit and the machine running GDS itself? (Probably by assigning a static ip beforehand). If so, all I need to do is setting up the autostart sequence at specific time or trigger for the flight software code with a pre-set ip address and port right?
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