| 摘要 |
<p>Windshear warning apparatus which separately compares a plurality of inertial derived (34-36) and air data derived (47) acceleration signals which under normal wind conditions are substantially equal but under windshear conditions will be significantly different and used to indicate incipient windshear. Also, a signal proportional to the product of the magnitude and rate of change of the total or resultant inertial acceleration of the aircraft is used to provide a warning (52) of a significant windshear condition. </p> |
