| | Windshear guidance system - Patent 5361065 (Site not responding. Last check: 2007-10-09) |
 | | Flight guidance in increasing performance windshear is based on the fact that the weather phenomenon of a microburst in the vicinity of the approach or departure area of an airport, where aircraft are operating at low altitude, may lead to hazardous conditions, and crashes have been documented as a direct result of this problem. |
 | | According to the present invention, a windshear guidance system is provided to adjust the performance of the aircraft during the initial increasing performance windshear encounter such that the kinetic energy of the aircraft will be increased, and this increase in energy will help to prevent a crash during a subsequent decreasing performance windshear. |
 | | In operation, a windshear detector (not shown) is utilized to determine that an increasing performance windshear is present, and when of a significant magnitude, the increasing performance windshear guidance is activated. |
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