Abstract
The modern Control Configurated Vehicle (C.C.V.) design technologies aims at taking simultaneously into account performances and maneuvrability requirements, and handling quality specifications. Therefore it is very important to provide the modern stability and control engineers with a tool which allows to determine the maximum allowable range of aircraft parameter variation according to handling quality requirements. By using decoupled linearized model of longitudinal and latero-directional dynamics, handling qualities are expressed in terms of pole location, with assigned tolerance, in the complex plane. With reference to a General Aviation aircraft Partenavia AP68 TP-VIATOR, in this paper we present a procedure whichallows to compute an estimate of the domains in the planes altitude-speed (Flight Envelope) and weight-center of gravity location (Weight and Balance Envelope) inside which the specified handling qualities are respected.
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