2014•Unpublished venueRequires access

Ground test platform for attitude and orbit control system of small satellite

Huayi Li

Abstract

Ground test platform for attitude and orbit control system of small satellite is designed. Hardware interfaces between the real sensors / actuators and the onboard computer is simulated. Satellite dynamic and space environment is calculated in order to form a close-loop control system. Finally, the ground test system is validated by comparing the simulation result and in-orbit flying data.

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Available abstract

Key concepts: Attitude control, Satellite, Orbit (dynamics), Aerospace engineering, Ground track, Actuator, Computer science, Control system