There is an increasing number of flight mechanics studies where the influence of manoeuvre type has been found to be of importance. A notable example has been the upgrade to the U.S. Mil. Spec, for handling qualities which includes a set of aggressive tasks to be flown as part of the flight test requirements. Another recent development has been the wider use of inverse simulation where a flight path is used to drive a helicopter mathematical model, the aim being to calculate the control actions corresponding to the flight path being flown. Although the evaluation of helicopter performance through the use of standard manoeuvres has become established, there is little information available on the precise form of the manoeuvre, or on h...
The objective of this paper is to present general techniques for simulating helicopter flight trajec...
The control displacements required for a helicopter to fly a defined manoeuvre may be calculated by ...
The paper deals with the assessment of the reliability of simplified rotorcraft models in the evalua...
There is an increasing number of flight mechanics studies where the influence of manoeuvre type has...
Helicopter performance and handling qualities are now routinely assessed in relation to specific man...
Abstract: The helicopter has evolved into one of the most powerful ¯ight vehicles for air domination...
Inverse simulation is a technique whereby the control actions required for a modelled vehicle to fly...
The paper presents a technique for assessing the reliability of a set of helicopter models in predic...
The paper presents a technique for assessing the reliability of a set of helicopter models in predic...
The helicopter is specific in regards to other traffictransportation means, not just by its structur...
A collaborative programme of research into helicopter handling qualities and mission effectiveness ...
The paper deals with the assessment of the reliability of simplified rotorcraft models in the evalua...
This paper outlines a method of measuring the Inherent Agility (i.e. the agility of the aircraft alo...
Inverse simulation is used to calculate the control displacements required for a modeled vehicle to ...
The validation of theoretical flight-mechanics models for helicopters is of considerable practical i...
The objective of this paper is to present general techniques for simulating helicopter flight trajec...
The control displacements required for a helicopter to fly a defined manoeuvre may be calculated by ...
The paper deals with the assessment of the reliability of simplified rotorcraft models in the evalua...
There is an increasing number of flight mechanics studies where the influence of manoeuvre type has...
Helicopter performance and handling qualities are now routinely assessed in relation to specific man...
Abstract: The helicopter has evolved into one of the most powerful ¯ight vehicles for air domination...
Inverse simulation is a technique whereby the control actions required for a modelled vehicle to fly...
The paper presents a technique for assessing the reliability of a set of helicopter models in predic...
The paper presents a technique for assessing the reliability of a set of helicopter models in predic...
The helicopter is specific in regards to other traffictransportation means, not just by its structur...
A collaborative programme of research into helicopter handling qualities and mission effectiveness ...
The paper deals with the assessment of the reliability of simplified rotorcraft models in the evalua...
This paper outlines a method of measuring the Inherent Agility (i.e. the agility of the aircraft alo...
Inverse simulation is used to calculate the control displacements required for a modeled vehicle to ...
The validation of theoretical flight-mechanics models for helicopters is of considerable practical i...
The objective of this paper is to present general techniques for simulating helicopter flight trajec...
The control displacements required for a helicopter to fly a defined manoeuvre may be calculated by ...
The paper deals with the assessment of the reliability of simplified rotorcraft models in the evalua...