Projection method for projection of overall view at inner walls of aircraft, involves determining limiting region of two fields of overall view

摘要

The projection method involves determining (S20) a limiting region of two fields of an overall view (100). The limiting regions are adapted (S30) at each other to appropriate partial image edges depending on the distance of partial limiting regions. The fields are Predistorted (S40) on the basis of a Geometry of a projection surface such that a distortion is perceptible only to a decreased extent on a projection surface during a representation of the fields. An independent claim is also included for an aircraft with a projection device.