HYBRID INVERSE METHODS FOR HELICOPTERS IN AGGRESSIVE MANOEUVRING FLIGHT

The need to implement a process of constraints handling into conventional inverse simulation represents an important problem. To achieve this, a modification of the conventional inverse simulation technique which includes predictive capability is proposed in this paper. After giving details of the development of the predictive inverse simulation algorithm, the paper demonstrates the applicability of the developed methodology on two aggressive helicopter manoeuvres: pop-up and lateral realignment.