| 摘要 |
<p>The invention relates to a display device (14) including a means (15) for selectively displaying the flight characteristics of an aircraft on the basis of a credibility state ascribed to the measurements from static-pressure, total-pressure, and incidence sensors, including a means for selectively displaying: a main set of flight characteristics including at least one flight characteristic from a measurement from one of said sensors when the measurements from said sensors are considered to be reliable; and a secondary set of flight characteristics different than those of said main set and including at least one secondary flight characteristic (M* n, Z** p, EV* n) which is to replace a homologous flight characteristic in the main set when the measurements from at least one of said sensors are considered to be unreliable, and which is separate from any measurement from each sensor considered to be unreliable which was performed when the measurements from said sensor were considered to be unreliable.</p> |
