Presentation of equations for perturbed motion of aircraft in form of single loop diagrams; analysis of characteristics of individual links and their change with changing flight speed and altitude; derivation of transfer functions for control with elevator, rudder, and aileron. English translation of paper in Russian from Report, Ministry of Aviation Industry.
Airplane as object of control (Block Diagrams of Equations of Perturbed Airplane Motion)
NASA -- Tech Translation
1959
52 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Diagrams of airplane stability
Engineering Index Backfile | 1920
|Diagrams of airplane stability
NTRS | 1921
|