| 摘要 |
<p>The method involves determining a current phase of flight of an aircraft, and determining an altitude corresponding to current altitude of the aircraft. Another altitude corresponds to an average value of a section of the trajectory of the flight. The section starts from a current position of the aircraft and corresponds to a maximum section which is displayed in a select indicator (3) with respect to the size of the indicator and indicator`s scale. The current phase of the flight and the altitudes are determined. Independent claims are also included for the following: (1) a device for assisting a pilot of an aircraft (2) an aircraft has a device for assisting a pilot of an aircraft.</p> |
