| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a simplified user interface for an aircraft. <P>SOLUTION: The user interface 30 for an integrated autopilot and flight management system for an aircraft 10 includes a plurality of tactical parameter controls for operation of the autopilot and a plurality of strategic parameter controls for operation of the flight management system. <P>COPYRIGHT: (C)2013,JPO&INPIT |
