Client-Server Implementation in Solving the Problem of Modeling the Small Spacecraft Flight at Low-Earth Orbit

The possibility of implementing a modeling of the flight of a small spacecraft in low earth orbit based on a client-server architecture was researched. Issues such as transmitting and displaying the system state, aggregating states at different points in time, and executing user code were discussed. The conducted studies demonstrate the benefits of using a client-server implementation in solving the problem of simulating the flight of a small spacecraft in near-earth orbit in a world of increasing interest in satellite developments.