Simulation platform for the attitude and orbit control system design of small satellites
Ning Liu
Abstract
Ning Liu
Abstract
A platform was developed to simulate attitude and orbit control system design of small satellites graphical output. The software calculates the orbital dynamics, interfaces with the satellite attitude determination and control system (ADCS) program and produces 3D output of the simulation result. The software was developed to design orbits for formation flying and to test the ADCS program. The 3D realtime display demonstrates orbit and attitude motion during launch, telemetry and telecommand operations and applications of the satellites.
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A platform was developed to simulate attitude and orbit control system design of small satellites graphical output. The software calculates the orbital dynamics, interfaces with the satellite attitude determination and control system (ADCS) program and produces 3D output of the simulation result. The software was developed to design orbits for formation flying and to test the ADCS program. The 3D realtime display demonstrates orbit and attitude motion during launch, telemetry and telecommand operations and applications of the satellites.
Key concepts: Attitude control, Orbit (dynamics), Satellite, Software, Computer science, Simulation, Aerospace engineering, Engineering