Design and Implementation of UAV's Flight Control System Test Platform

Abstract

For the test requirements of UAV flight control system, using the virtual instrument, dynamic configuration of software and hardware and database technology, a flight control system test platform with more flexible manual and automated testing platform was designed. This paper describes composition and working principle of the system. Some key technology such as ICD data management, flight instrument simulation displaying, and flight control actuator loading is analyzed and discussed. Through actual use, the platform can satisfy comprehensive testing requirements for the development and production.