Add to ORKGThe problem of longitudinal stability and control of an airframe, having nonlinearity in its principal aerodynamic characteristics, is considered. It is shown that the equation describing the response in w, and thus the incidence, is a nonlinear differential equation of the fourth order. This equation, and its degenerate forms, is used as an example to demonstrate various nonlinear techniques and their shortcomings. This paper is to be presented at the AGARD Flight Mechanics Panel Specialists&apos
Determining suitable controllers for the process of evaluating dynamic per-formance of multiple vers...
Aircraft control normally relies on gain-scheduling of linear control laws, an approach that has bee...
The F/A-18 Hornet aircraft with the original flight control law exhibited a nonlinear out-of-control...
The problem of longitudinal stability and control of an airframe, having nonlinearity in its princi...
In this work, we analyzed a bifurcational behavior of a longitudinal flight nonlinear dynamics, taki...
This paper shows simple method to simulate nonlinear longitudinal flight dynamic of an aircraft in t...
Through theoretical and analog results the effects of two nonlinear stability derivatives on the lon...
This paper investigates geometrically-nonlinear aeroelastic effects on an industry-level aircraft co...
Abstract—Without horizontal and vertical stabilizers, a combat flying wing with high aspect-ratio ha...
Fluid-structure interactions (FSI) that involve nonlinear aerodynamic forces are described which aff...
Nonlinear model-following control design is applied to the problem of control of the six degrees of ...
AbstractTo investigate the longitudinal motion stability of aircraft maneuvers conveniently, a new s...
AbstractA review on the recent advance in nonlinear aeroelasticity of the aircraft is presented in t...
Abstract: In this paper, a stabilization problem for an aircraft at a high angle of attack is consid...
Automatic flight control systems have become increasingly vital ever since the emergence of airplan...
Determining suitable controllers for the process of evaluating dynamic per-formance of multiple vers...
Aircraft control normally relies on gain-scheduling of linear control laws, an approach that has bee...
The F/A-18 Hornet aircraft with the original flight control law exhibited a nonlinear out-of-control...
The problem of longitudinal stability and control of an airframe, having nonlinearity in its princi...
In this work, we analyzed a bifurcational behavior of a longitudinal flight nonlinear dynamics, taki...
This paper shows simple method to simulate nonlinear longitudinal flight dynamic of an aircraft in t...
Through theoretical and analog results the effects of two nonlinear stability derivatives on the lon...
This paper investigates geometrically-nonlinear aeroelastic effects on an industry-level aircraft co...
Abstract—Without horizontal and vertical stabilizers, a combat flying wing with high aspect-ratio ha...
Fluid-structure interactions (FSI) that involve nonlinear aerodynamic forces are described which aff...
Nonlinear model-following control design is applied to the problem of control of the six degrees of ...
AbstractTo investigate the longitudinal motion stability of aircraft maneuvers conveniently, a new s...
AbstractA review on the recent advance in nonlinear aeroelasticity of the aircraft is presented in t...
Abstract: In this paper, a stabilization problem for an aircraft at a high angle of attack is consid...
Automatic flight control systems have become increasingly vital ever since the emergence of airplan...
Determining suitable controllers for the process of evaluating dynamic per-formance of multiple vers...
Aircraft control normally relies on gain-scheduling of linear control laws, an approach that has bee...
The F/A-18 Hornet aircraft with the original flight control law exhibited a nonlinear out-of-control...