| 摘要 |
<p>The system has a detection circuit (1) having a measuring channel (10) which includes static air pressure measuring devices (13, 14) and an aircraft`s side-slip angle measuring device. A measuring device (15) measures a dynamic pressure, a total temperature and an angle of attack of the aircraft, and a data processing device (12) determines anemobaroclinometric parameters based on the measurements. A laser anemometer (50) anemometer is placed in a housing proximal to an external skin of the aircraft and measures a true air speed parameter of the aircraft.</p> |
