| 摘要 |
<p>The invention relates to a method for managing the air data of an aircraft. The invention further relates to a method for managing the altitude data of an aircraft, in which a main baro-inertial calculation loop is used, which uses signals from an inertial unit and standard altitude information provided by a main air data source, and at least one secondary baro-inertial loop for calculating gaps, which uses signals from said inertial unit of the main loop and standard altitude information from a secondary air data source, respectively; and in which a baro-inertial altitude gap, a vertical velocity gap and a accelerometer bias gap visible on the satellite subpoint between the main loop and said at least one secondary baro-inertial loop are calculated.</p> |
