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Wind Advisory SystemThe present invention is a two-part wind advisory system comprising a ground station at an airfield and an airborne unit placed inside an aircraft. The ground station monitors wind conditions (wind speed, wind direction, and wind gust) at the airfield and transmits the wind conditions and an airfield ID to the airborne unit. The airborne unit identifies the airfield by comparing the received airfield ID with airfield IDs stored in a database. The airborne unit also calculates the headwind and crosswind for each runway in both directions at the airfield using the received wind conditions and runway information stored in the database. The airborne unit then determines a recommended runway for takeoff and landing operations of the aircraft based on th~ runway having the greatest headwind value and displays the airfield ID, wind conditions, and recommended runway to the pilot. Another embodiment of the present invention includes a wireless internet based airborne unit in which the airborne unit can receive the wind conditions from the ground station over the internet.
Document ID
20010125600
Acquisition Source
Armstrong Flight Research Center
Document Type
Other - Patent
Authors
Curto, Paul A.
(NASA Dryden Flight Research Center Edwards, CA United States)
Brown, Gerald E.
(NASA Dryden Flight Research Center Edwards, CA United States)
Zysko, Jan A.
(NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
August 20, 2013
Publication Date
October 30, 2001
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-606102
Patent Number: NASA-Case-DRC-09901-6
Patent Number: US-Patent-6,311,107
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-Case-DRC-09901-6|US-Patent-6,311,107
Patent Application
US-Patent-Appl-SN-606102
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