A Flight-test and Simulation Evaluation of the Longitudinal Final Approach and Landing Performance of an Automatic System for a Light Wing Loading STOL Aircraft Equipped with Wing Spoilers

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National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1984 - Instrument landing systems - 41 pages
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Contents

Section 1
24
Section 2
25
Section 3
26

4 other sections not shown

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