Inverse simulation is a technique whereby the control actions required for a modelled vehicle to fly a specified manoeuvre can be established. In this paper the general concepts of inverse simulation are introduced, and an algorithm designed specifically to achieve inverse simulation of a single main and tail rotor helicopter is presented. An important element of an inverse simulation is the design of the input functions i.e. manoeuvre definitions, and the methods used are also detailed. A helicopter mathematical model is also discussed along with the validation and verification of the inverse simulation. Finally, the applicability of the method is demonstrated by illustration of its use in two flight dynamics studies
The paper presents a technique for assessing the reliability of a set of helicopter models in predic...
Inverse simulation techniques have been employed for several years to analyse the manoeuvrability, o...
The paper presents a technique for assessing the reliability of a set of helicopter models in predic...
Inverse simulation is used to calculate the control displacements required for a modeled vehicle to ...
Helicopter performance and handling qualities are now routinely assessed in relation to specific man...
Abstract: This paper focuses on a detailed description and application of inverse simulation, which ...
Inverse simulation is a technique by which the necessary control actions can be calculated for a veh...
This report documents the application of the inverse simulation algorithm Genisa [1] to the Concept...
A novel inverse simulation scheme is proposed for application to rotorcraft dynamic models. The algo...
The paper deals with the assessment of the reliability of simplified rotorcraft models in the evalua...
A novel inverse simulation scheme is proposed for application to rotorcraft dynamic models. The alg...
A conventional inverse simulation does not accommodate control constraints; hence for aggressive man...
Inverse simulation allows system inputs to be found to give model outputs that match required time h...
The paper deals with the assessment of the reliability of simplified rotorcraft models in the evalua...
This paper presents an inverse simulation methodology based on numerical optimization. The methodolo...
The paper presents a technique for assessing the reliability of a set of helicopter models in predic...
Inverse simulation techniques have been employed for several years to analyse the manoeuvrability, o...
The paper presents a technique for assessing the reliability of a set of helicopter models in predic...
Inverse simulation is used to calculate the control displacements required for a modeled vehicle to ...
Helicopter performance and handling qualities are now routinely assessed in relation to specific man...
Abstract: This paper focuses on a detailed description and application of inverse simulation, which ...
Inverse simulation is a technique by which the necessary control actions can be calculated for a veh...
This report documents the application of the inverse simulation algorithm Genisa [1] to the Concept...
A novel inverse simulation scheme is proposed for application to rotorcraft dynamic models. The algo...
The paper deals with the assessment of the reliability of simplified rotorcraft models in the evalua...
A novel inverse simulation scheme is proposed for application to rotorcraft dynamic models. The alg...
A conventional inverse simulation does not accommodate control constraints; hence for aggressive man...
Inverse simulation allows system inputs to be found to give model outputs that match required time h...
The paper deals with the assessment of the reliability of simplified rotorcraft models in the evalua...
This paper presents an inverse simulation methodology based on numerical optimization. The methodolo...
The paper presents a technique for assessing the reliability of a set of helicopter models in predic...
Inverse simulation techniques have been employed for several years to analyse the manoeuvrability, o...
The paper presents a technique for assessing the reliability of a set of helicopter models in predic...