| 摘要 |
The purpose of the present invention is to provide a launcher device integrated test facility system capable of a flying software test, a functional test of a guide control electronic unit which is being developed or completed, and a system integration test of a launcher of an actuator product and a completed guide control electronic for flying in the same condition as the actual flight condition. The launcher device integrated test facility system according to the present invention comprises: a launcher simulator to produce and output a launcher posture and a tracking simulation output by receiving an electronic unit signal or an actuator signal; a launcher emulator to produce and output an emulation signal for operating a launcher guide navigation control system by receiving the electronic unit signal; an electronic unit simulator to copy a launcher loaded electronic unit, to receive the launcher posture, the tracking simulation output, and the emulation signal, and to output the electronic unit signal including a launcher loaded actuator driving command; an actuator simulator to copy the static/dynamic characteristics of the actuator in response to the launcher loaded actuator driving command included in the electronic unit signal; and an interface control module to perform signal switching between the launcher simulator, the launcher emulator, the electronic unit simulator, and the actuator simulator upon the launcher device integrated test condition. |
