Add to ORKGA mathematical model suitable for real time simulation of the CH-53 helicopter is presented. This model, which is based on modified nonlinear classical rotor theory and nonlinear fuselage aerodynamics, will be used to support terminal-area guidance and navigation studies on a fixed-base simulator. Validation is achieved by comparing the model response with that of a similar aircraft and by a qualitative comparison of the handling characteristics made by experienced pilots
A linear time-varying helicopter simulation program (TVHIS) is described. The program is designed as...
A math model was formulated to represent some of the aerodynamic effects of low speed, low altitude,...
A study on the kinematic relationship of the variables of helicopter motion in steady, coordinated t...
A mathematical model, suitable for piloted simulation of the flying qualities of helicopters, is a n...
A generalized, real time, piloted, visual simulation of a single rotor helicopter, suspension system...
A nonlinear simulation model of the CH-47B helicopter was adapted for use in the NASA Ames Research ...
A computer simulation of a human response pilot mechanism within the flight control loop of a high-p...
The dynamic coupling between the rotor system and the fuselage of a simplified helicopter model in h...
A mathematical model of an advanced helicopter is described. The model is suitable for use in contro...
The optimal control model (OCM) of the human operator is used to predict the effect of simulator cha...
The study of a control system for the Da Vinci 2 human-powered helicopter in hovering flight is docu...
A mathematical model of the Sikorsky SH-3G helicopter based on classical nonlinear, quasi-steady rot...
Flight tests for verifying an analytical aerodynamic derivative model of a CH-47 helicopter were con...
A computer program was developed to integrate avionics research in navigation, guidance, controls, a...
An amended six degree of freedom helicopter stability and control derivative model was developed in ...
A linear time-varying helicopter simulation program (TVHIS) is described. The program is designed as...
A math model was formulated to represent some of the aerodynamic effects of low speed, low altitude,...
A study on the kinematic relationship of the variables of helicopter motion in steady, coordinated t...
A mathematical model, suitable for piloted simulation of the flying qualities of helicopters, is a n...
A generalized, real time, piloted, visual simulation of a single rotor helicopter, suspension system...
A nonlinear simulation model of the CH-47B helicopter was adapted for use in the NASA Ames Research ...
A computer simulation of a human response pilot mechanism within the flight control loop of a high-p...
The dynamic coupling between the rotor system and the fuselage of a simplified helicopter model in h...
A mathematical model of an advanced helicopter is described. The model is suitable for use in contro...
The optimal control model (OCM) of the human operator is used to predict the effect of simulator cha...
The study of a control system for the Da Vinci 2 human-powered helicopter in hovering flight is docu...
A mathematical model of the Sikorsky SH-3G helicopter based on classical nonlinear, quasi-steady rot...
Flight tests for verifying an analytical aerodynamic derivative model of a CH-47 helicopter were con...
A computer program was developed to integrate avionics research in navigation, guidance, controls, a...
An amended six degree of freedom helicopter stability and control derivative model was developed in ...
A linear time-varying helicopter simulation program (TVHIS) is described. The program is designed as...
A math model was formulated to represent some of the aerodynamic effects of low speed, low altitude,...
A study on the kinematic relationship of the variables of helicopter motion in steady, coordinated t...