Fundamental conditions for automatic control are discussed with description of automatic-control mechanism; first part is negative-pressure indicator, second and third part forming gyroscope consisting of two numerically equal gyroscopic tops coupled together but revolving in opposite directions; obtaining maximum steering economy; comments by Drexler, Bader and Diemer. From 1927 Yearbook of Wissenschaftliche Gesellschaft fuer Luftfahrt. (See also - discussion p 11-25)
Mechanical control of airplanes
Nat Advisory Committee Aeronautics -- Tech Memorandums
1929
11 pages
10 Figs.
Aufsatz (Zeitschrift)
Englisch
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Mechanical control of airplanes
NTRS | 1929
|Engineering Index Backfile | 1929
|Engineering Index Backfile | 1929
Engineering Index Backfile | 1929
|Engineering Index Backfile | 1927
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