Box 13
Container
Contains 76 Results:
Control investigations: Investigations on the dependency of the stability range on changes in the coefficients in the control equation when assigning rudder speed. (Carried out for stand c1 = d = 0)., 1940-12-19
File — Box: 13, Folder: 86/60
Dates:
1940-12-19
Control investigations: Stability of aggregate vibrations in the orbital plane, 1941-01-15
File — Box: 13, Folder: 86/65
Dates:
1941-01-15
Guide beam activation: Investigations on the lateral guide beam guidance of the unit V2., 1941-01-28
File — Box: 13, Folder: 86/67
Dates:
1941-01-28
Contribution to the theory of aircraft control Dissertation of the Department of Mathematics and Natural Sciences of the Technical University of Darmstadt, 1941-02-05
File — Box: 13, Folder: 86/69
Dates:
1941-02-05
Control investigations: Stability ranges of the unit vibrations with guide beam guidance perpendicular to the plane of the steam, 1941-03-16
File — Box: 13, Folder: 86/75
Dates:
1941-03-16
Control investigations: Favorable choice of the coefficients of a characteristic equation
File — Box: 13, Folder: 86/81
Dates:
1920 - 1970
Guide beam activation: Determination of the guide beam activations for the unit A4 with S A M control
File — Box: 13, Folder: 86/87
Dates:
1920 - 1970
Beacon activation: To illustrate the stability theory of lateral beacon guidance, 1941-05-15
File — Box: 13, Folder: 86/82
Dates:
1941-05-15
Control investigations: investigation of the influence of liquid oscillations in the fuel tanks on the stability of the unit, 1941-04-09
File — Box: 13, Folder: 86/84
Dates:
1941-04-09
Guide beam activation: Guide beam side guidance of unit 52 without gyro control, 1941-09-02
File — Box: 13, Folder: 86/90
Dates:
1941-09-02