The effects on handling qualities of elastic modes interaction with the rigid body dynamics of a large flexible aircraft are studied by a mathematical computer simulation. An analytical method to predict the pilot ratings when there is a severe modes interactions is developed. This is done by extending the optimal control model of the human pilot response to include the mode decomposition mechanism into the model. The handling qualities are determined for a longitudinal tracking task using a large flexible aircraft with parametric variations in the undamped natural frequencies of the two lowest frequency, symmetric elastic modes made to induce varying amounts of mode interaction
Effects of aeroservoelasticity on the manual control of large civil aircraft are investigated throu...
Flexible systems deflect, vibrate, or oscillate when moved. This behavior results in decreased perfo...
An analytical technique for investigating transport aircraft handling qualities is exercised in a st...
The effects on handling qualities of low frequency symmetric elastic mode interaction with the rigid...
The notion of airplane stability and control being a balancing act between stability and control ha...
The problem of ameliorating the discomfort of passengers on a large air transport subject to flight ...
Full motion flight simulators are quite commonly used to evaluate handling qualities of an aircraft ...
A modal analysis technique was developed for evaluating the effects of elastic modes on aircraft dyn...
The NASA Langley Research Center Cockpit Motion Facility (CMF) was used to conduct a piloted simulat...
The RQ trends which large flexible aircraft exhibit under various parameterizations of control laws ...
A high order rotorcraft mathematical model is developed and validated against the XV-15 and a Large ...
An experimental evaluation of analytical techniques for predicting certain stability and control cha...
This article aims to indicate the differences between rigid and flexible wing aircraft ...
Classical flight dynamics analyses and pilot-in-the-loop simulations are traditionally based on rigi...
The optimal control model (OCM) of the human pilot is applied to the study of aircraft handling qual...
Effects of aeroservoelasticity on the manual control of large civil aircraft are investigated throu...
Flexible systems deflect, vibrate, or oscillate when moved. This behavior results in decreased perfo...
An analytical technique for investigating transport aircraft handling qualities is exercised in a st...
The effects on handling qualities of low frequency symmetric elastic mode interaction with the rigid...
The notion of airplane stability and control being a balancing act between stability and control ha...
The problem of ameliorating the discomfort of passengers on a large air transport subject to flight ...
Full motion flight simulators are quite commonly used to evaluate handling qualities of an aircraft ...
A modal analysis technique was developed for evaluating the effects of elastic modes on aircraft dyn...
The NASA Langley Research Center Cockpit Motion Facility (CMF) was used to conduct a piloted simulat...
The RQ trends which large flexible aircraft exhibit under various parameterizations of control laws ...
A high order rotorcraft mathematical model is developed and validated against the XV-15 and a Large ...
An experimental evaluation of analytical techniques for predicting certain stability and control cha...
This article aims to indicate the differences between rigid and flexible wing aircraft ...
Classical flight dynamics analyses and pilot-in-the-loop simulations are traditionally based on rigi...
The optimal control model (OCM) of the human pilot is applied to the study of aircraft handling qual...
Effects of aeroservoelasticity on the manual control of large civil aircraft are investigated throu...
Flexible systems deflect, vibrate, or oscillate when moved. This behavior results in decreased perfo...
An analytical technique for investigating transport aircraft handling qualities is exercised in a st...