| 摘要 |
<p>The system has fiber laser anemometers (401-404) distributed in locations of a fuselage of an aircraft. Each anemometer includes a measuring channel to measure a local component of true airspeed of the aircraft. The anemometers assure local measurements distributed by the fuselage. A calculating unit calculates a module and direction of a vector of the true airspeed from the measurements of the component. The unit implements a correlation table allowing the correlation among the local measurements, the airspeed vector, and the disturbances related to the presence of the fuselage.</p> |
