This work considers the presentation of equations for the perturbed motion of an airplane in the form of single-loop block diagrams. A brief analysis is given of the characteristics of the individual links and of their change with changing flight speed and altitude. A derivation of transfer functions for control with elevator, rudder, and aileron is presented, as well as simplified expressions for the transfer functions, depending on the frequency range, which correspond to break- ing up the perturbed motion into simple types. The representation of the equations of perturbed airplane motion in the form of single-loop block diagrams permits a simple and easy application of contemporary methods of control theory to the analysis of airplane motion, and also allows rapid formulation of simplified equations of motion and transfer functions applicable during control with the control elements.
Airplane as an Object of Control: Block Diagrams of the Equations of Perturbed Airplane Motion
1959
48 pages
Report
No indication
English
Airplane as object of control (Block Diagrams of Equations of Perturbed Airplane Motion)
Engineering Index Backfile | 1959
|Diagrams of airplane stability
Engineering Index Backfile | 1920
|Diagrams of airplane stability
NTRS | 1921
|