Forward-look wind-shear detection for microburst recovery
David A. Hinton
Abstract
David A. Hinton
Abstract
An effort is in progress by NASA, the Federal Aviation Administration, and the industry to reduce the threat of convective microburst wind-shear phenomena to aircraft. This paper describes an effort to quantify the benefits of forward-look sensing and to develop and test a candidate set of strategies for recovery from inadvertent microburst encounters during the landing approach. Initial development of recovery strategies was performed in batch simulation prior to piloted simulation evaluation using a full dynamic airplane model. The results of this effort indicate that the factor that most strongly effects a microburst recovery is the time at which the recovery is initiated. Improving the alert time by 5 s generally provided a greater recovery performance increase than could be achieved by changing the recovery strategy. Forward-look alerts given 10 s prior to microburst entry permitted recoveries to be made with negligible altitude loss. Nomenclature F = wind-shear hazard index g = gravitational acceleration //ref = reference altitude for recovery strategies V = airplane airspeed Wh = vertical wind component, updraft positive Wx = horizontal wind component, along the airplane ground track
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An effort is in progress by NASA, the Federal Aviation Administration, and the industry to reduce the threat of convective microburst wind-shear phenomena to aircraft. This paper describes an effort to quantify the benefits of forward-look sensing and to develop and test a candidate set of strategies for recovery from inadvertent microburst encounters during the landing approach. Initial development of recovery strategies was performed in batch simulation prior to piloted simulation evaluation using a full dynamic airplane model. The results of this effort indicate that the factor that most strongly effects a microburst recovery is the time at which the recovery is initiated. Improving the alert time by 5 s generally provided a greater recovery performance increase than could be achieved by changing the recovery strategy. Forward-look alerts given 10 s prior to microburst entry permitted recoveries to be made with negligible altitude loss. Nomenclature F = wind-shear hazard index g = gravitational acceleration //ref = reference altitude for recovery strategies V = airplane airspeed Wh = vertical wind component, updraft positive Wx = horizontal wind component, along the airplane ground track
Key concepts: Microburst, Wind shear, Aerospace engineering, Shear (geology), Geology, Environmental science, Meteorology, Engineering