Feasibility study of a procedure to detect and warn of low-level wind shear
Barry S. Turkel, Philip A. Kessel, Walter Frost, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, George C. Marshall Space Flight Center
National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981 - Technology & Engineering - 70 pages
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1-Cosine S-Shape 20.6 m/s amplitude aircraft trajectory program airspeed deviation parameters airspeed ranged airspeed varied amplitude and l/2 angle of attack attack varied B727 Aircraft Performed B727 Using Control combination longitudinal S-shape computer model computer simulation Computer-Simulated Approach Trajectory cosine downbursts Cosine Wave Wind derivative rad Doppler radar Eastern 66 elevator angle Figure fixed gains flight path angle flight path deterioration flight path deviation flight simulator FPDP ft/s full forward glide slope ground speed head wind l5.45 m/s amplitude Longitudinal Longitudinal Longitudinal longitudinal S-shape wave longitudinal sine wave longitudinal wave model pilot NASA Ames simulator path deterioration parameters phugoid frequency Pilot Pilot Pilot pilot simulator runs pitch angle S-shape and vertical S-Shape Wave Wind shear wave simulated pilot Simulated trajectory Sine Sine Sine Sine Wave Wind tail wind shear thrust rate vertical velocity Vref wave amplitude wave of 5.l5 wind field wind gradient wind to tail