Add to ORKGA mathematical model for a real time simulation of a tilt rotor aircraft was developed. The mathematical model is used for evaluating aircraft performance and handling qualities. The model is based on an eleven degree of freedom total force representation. The rotor is treated as a point source of forces and moments with appropriate response time lags and actuator dynamics. The aerodynamics of the wing, tail, rotors, landing gear, and fuselage are included
An investigation was conducted in the Langley V/STOL tunnel to determine the performance, stability ...
A high order rotorcraft mathematical model is developed and validated against the XV-15 and a Large ...
An overview of an experimental and analytical research program underway for studying the aeroelastic...
The results of a real time piloted simulation to investigate the handling qualities and performance ...
A mathematical model for real-time flight simulation of a tilt rotor research aircraft was developed...
A mathematical model of a tilt-wing aircraft that was used in a piloted, six-degree-of-freedom fligh...
This paper aims at describing the effort performed by the joint research group of Politecnico di Tor...
A computer model of a tilt-rotor has been developed for calculating perfor-mance, simulating flight ...
This paper introduces a novel gimballed rotor mathematical model for real-time flight simulation of ...
This paper aims at describing the effort performed by the joint research group of Politecnico di Tor...
A preliminary design study was conducted to establish a minimum sized, low cost V/STOL tilt-rotor re...
The aim of this work is to describe the development of a tilt-rotor model for real-time flight simu...
The results of a study of folding tilt rotor (stowed rotor) aircraft are presented. The effects of d...
The introduction of tilt-rotor aircraft into the existing civilian air transportation system will pr...
The design features and general characteristics of the NASA/Army XV-15 tilt rotor research aircraft ...
An investigation was conducted in the Langley V/STOL tunnel to determine the performance, stability ...
A high order rotorcraft mathematical model is developed and validated against the XV-15 and a Large ...
An overview of an experimental and analytical research program underway for studying the aeroelastic...
The results of a real time piloted simulation to investigate the handling qualities and performance ...
A mathematical model for real-time flight simulation of a tilt rotor research aircraft was developed...
A mathematical model of a tilt-wing aircraft that was used in a piloted, six-degree-of-freedom fligh...
This paper aims at describing the effort performed by the joint research group of Politecnico di Tor...
A computer model of a tilt-rotor has been developed for calculating perfor-mance, simulating flight ...
This paper introduces a novel gimballed rotor mathematical model for real-time flight simulation of ...
This paper aims at describing the effort performed by the joint research group of Politecnico di Tor...
A preliminary design study was conducted to establish a minimum sized, low cost V/STOL tilt-rotor re...
The aim of this work is to describe the development of a tilt-rotor model for real-time flight simu...
The results of a study of folding tilt rotor (stowed rotor) aircraft are presented. The effects of d...
The introduction of tilt-rotor aircraft into the existing civilian air transportation system will pr...
The design features and general characteristics of the NASA/Army XV-15 tilt rotor research aircraft ...
An investigation was conducted in the Langley V/STOL tunnel to determine the performance, stability ...
A high order rotorcraft mathematical model is developed and validated against the XV-15 and a Large ...
An overview of an experimental and analytical research program underway for studying the aeroelastic...