Methods of automatically controlling the airplane are reviewed. Equations for the controlled motion including inertia effects of the control are developed and methods of investigating the stability of the resulting fifth and higher order equations are presented. The equations for longitudinal and lateral motion with both ideal and non-ideal controls are developed in dimensionless form in terms of control parameters based on simple dynamic tests of the isolated control unit.
Theory of automatic control of airplanes
01.04.1939
Sonstige
Keine Angabe
Englisch
Theory of automatic control of airplanes
SLUB | 1939
|Theory of automatic control of airplanes
TIBKAT | 1939
|Theory of automatic control of airplanes
Engineering Index Backfile | 1939
|Automatic control of airplanes
Engineering Index Backfile | 1937
|Automatic control of airplanes
Engineering Index Backfile | 1937
|