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The Airborne wind shear detection and alert system, fitted in an aircraft, detects and alerts the pilot both visually and aurally of a wind shear condition. In case of reactive wind shear detection system, the detection takes place when the aircraft penetrates a wind shear condition of sufficient force, which can pose a hazard to the aircraft. In case of predictive wind shear detection system, the detection takes place, if such wind shear condition is ahead of the aircraft. In 1988 the U.S. Federal Aviation Administration (FAA) mandated that all turbine-powered commercial aircraft must have on-board windshear detection systems by 1993. Airlines successfully lobbied to have commercial turbo-prop aircraft exempted from this requirement. In the predictive wind shear detection mode, the weather radar processor of the aircraft detects the presence of the microburst, a type of vertical wind shear condition by detecting the Doppler frequency shift of the microwave pulses caused by the microburst ahead of the aircraft and displays the area where it is present in the Navigation Display Unit (of the Electronic Flight Instrument System) along with an aural warning. ==History of development== On July 24, 1986, the FAA of United States and NASA signed a memorandum of agreement to formally begin the Airborne Wind-Shear Detection and Avoidance Program (AWDAP). As a result, a wind-shear program was created in the Flight Systems Directorate of NASA's Langley Research Center. After five years of intensely studying various weather phenomena and sensor technologies, the researchers decided to validate their findings in actual flight conditions. They chose an extensively modified Boeing 737, which was equipped with a rear research cockpit in place of the forward section of the passenger cabin.〔(【引用サイトリンク】title=Making the Skies Safer, p.1 ) in Electronic Design, May 24, 2004〕 A modified Rockwell Collins model 708 X-band ground-based radar unit was used in the AWDAP experiments. The real-time radar processor system used during 1992 flight experiments was a VME bus-based system with a Motorola 68030 host processor and three DSP boards. On September 1, 1994, the weather radar model RDR-4B of the Allied-Signal/Bendix (now Honeywell) became the first predictive wind-shear system to be certified for commercial airline operation. In the same year, Continental Airlines became the first commercial carrier to install an airborne predictive wind-shear detection system on its aircraft. By June 1996, Rockwell Collins and Westinghouse's Defense and Electronics Group (now Grumman/Martin) also came up with FAA-certified predictive wind-shear detection systems.〔(【引用サイトリンク】title=Making the Skies Safer, p.2 ) in Electronic Design, May 24, 2004〕 The IEEE Intelligent Transportation Systems Society is conducting researches for further developments of this system. 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Airborne wind shear detection and alert system」の詳細全文を読む スポンサード リンク
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