Add to ORKGThrough theoretical and analog results the effects of two nonlinear stability derivatives on the longitudinal motions of an aircraft have been investigated. Nonlinear functions of pitching-moment and lift coefficients with angle of attack were considered. Analog results of aircraft motions in response to step elevator deflections and to the action of the proportional control systems are presented. The occurrence of continuous hunting oscillations was predicted and demonstrated for the attitude stabilization system with proportional control for certain nonlinear pitching-moment variations and autopilot adjustments
A theoretical investigation has been made to determine the effect of nonlinear stability derivatives...
A longitudinal stability and control characteristics of a Boeing B-29 airplane have been measured wi...
Dynamical systems theory has been used to study the nonlinear dynamics of the F-14. An eight degre...
A theoretical investigation has been made to determine the effect of nonlinear stability derivatives...
This report presents the results of an investigation conducted in the Langley free-flight tunnel to ...
Dynamical systems theory has been used to study nonlinear aircraft dynamics. A six degree of freedom...
The influence of automatic operation of the aileron and rudder controls on the lateral stability of ...
Methods of automatically controlling the airplane are reviewed. Equations for the controlled motion ...
The problem of longitudinal stability and control of an airframe, having nonlinearity in its princi...
The results of an experimental and theoretical investigation of the effects of large artificial vari...
The present investigation may be considered as preliminary to the study of automatic stabilizers. We...
An investigation was made to determine the accuracy with which the lateral flight motions of a swept...
Analytical-techniques are developed for deriving approximate solutions to a class of problems that ...
Nonlinear rotary stability derivatives - dynamic stability investigation - aerodynamic
A predictive method of nonlinear system analysis is used to investigate airplane stability and dynam...
A theoretical investigation has been made to determine the effect of nonlinear stability derivatives...
A longitudinal stability and control characteristics of a Boeing B-29 airplane have been measured wi...
Dynamical systems theory has been used to study the nonlinear dynamics of the F-14. An eight degre...
A theoretical investigation has been made to determine the effect of nonlinear stability derivatives...
This report presents the results of an investigation conducted in the Langley free-flight tunnel to ...
Dynamical systems theory has been used to study nonlinear aircraft dynamics. A six degree of freedom...
The influence of automatic operation of the aileron and rudder controls on the lateral stability of ...
Methods of automatically controlling the airplane are reviewed. Equations for the controlled motion ...
The problem of longitudinal stability and control of an airframe, having nonlinearity in its princi...
The results of an experimental and theoretical investigation of the effects of large artificial vari...
The present investigation may be considered as preliminary to the study of automatic stabilizers. We...
An investigation was made to determine the accuracy with which the lateral flight motions of a swept...
Analytical-techniques are developed for deriving approximate solutions to a class of problems that ...
Nonlinear rotary stability derivatives - dynamic stability investigation - aerodynamic
A predictive method of nonlinear system analysis is used to investigate airplane stability and dynam...
A theoretical investigation has been made to determine the effect of nonlinear stability derivatives...
A longitudinal stability and control characteristics of a Boeing B-29 airplane have been measured wi...
Dynamical systems theory has been used to study the nonlinear dynamics of the F-14. An eight degre...