| 摘要 |
<p>Disclosed are a system for verifying a satellite flight software and an operating method thereof, wherein the system is capable of supporting a command and a telemetry structure of a new satellite, and quickly verifying a satellite flight software in an initial step of a satellite development, and effectively changing designs of a command and a telemetry, while maintaining the core functions of the verification environment of which validity is confirmed through the previously performed satellite development processes. The system for verifying a satellite flight software comprises: a conventional verification environment; a command processing unit; a mounted computer; and a telemetry processing unit. In addition, the operating method of the system for verifying a satellite flight software comprises: a database mapping step; a CLTU conversion step; and a telemetry conversion step.</p> |
