Paper
27 May 1996 Lidar wind sensing at cruise altitudes for flight-level optimization
Russell Targ, Lawrence L. Ames
Author Affiliations +
Abstract
It has been apparent for more than a decade that the weather-forecast wind speed reaching flight crews in commercial aircraft differs by an average of +/- 15 knots from the wind speed actually experienced during the flight at cruise altitude. We recently analyzed wind-versus-altitude forecasts and found that the forecast altitude of maximum wind is also in error, by an average of +/- 4800 feet. In this era of increasing free-flight operations, we propose the use of airborne laser radar to measure winds above and below the aircraft in real time, so that a pilot can optimize the flight altitude with respect to prevailing winds. Analysis shows that such a lidar system would generate fuel savings of $LR100,000 to $LR200,000 per aircraft per year, especially for transoceanic routes. THis saving would pay for the instrument in one to two years.
© (1996) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Russell Targ and Lawrence L. Ames "Lidar wind sensing at cruise altitudes for flight-level optimization", Proc. SPIE 2737, Air Traffic Control Technologies II, (27 May 1996); https://doi.org/10.1117/12.241057
Advertisement
Advertisement
RIGHTS & PERMISSIONS
Get copyright permission  Get copyright permission on Copyright Marketplace
KEYWORDS
LIDAR

Fourier transforms

Meteorology

Wind measurement

Error analysis

Atmospheric modeling

Chlorine

Back to Top