Optimization and guidance of abort landing trajectories in a windshear

Author:

MIELE A.1,WANG T.1,MELVIN W.2

Affiliation:

1. Rice University, Houston, TX

2. Delta Airlines, Inc., Atlanta, GA

Publisher

American Institute of Aeronautics and Astronautics

Reference52 articles.

1. Chicago, Illinois, 1985.

2. Boeing 727-235, N4737, New Orleans

3. July 9, 1982, Report No. NTSB-AAR-8302,1933.

4. Delta Air Lines, Lockheed L-1011-3851,

5. Airport, Texas, August 2, 1985, Report No.

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1. Target pitch angle for the microburst escape maneuver;Journal of Aircraft;1993-11

2. Adaptive control of aircraft in windshear;International Journal of Robust and Nonlinear Control;1993

3. Optimal recovery from microburst wind shear;Guidance, Navigation and Control Conference;1992-08-10

4. Target pitch angle for the microburst escape maneuver;30th Aerospace Sciences Meeting and Exhibit;1992-01-06

5. Forward-look wind-shear detection for microburst recovery;Journal of Aircraft;1992-01

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