Effects of cable geometry and aircraft attitude on the accuracy of a magnetic leader cable system for aircraft guidance during rollout and turnoff / W. Thomas Bundick.
|Main Author:||Bundick, W. Thomas.|
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1982.
> Control systems.
Microwave landing systems.
Subject Category 04.
"Langley Research Center."
29 p. :
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