METHOD FOR DETERMINING NAVIGATION PARAMETERS FOR LANDING AIRCRAFT ON DRIFTING ICE FLOE

摘要

The invention relates to navigation, specifically to determining navigational parameters for performing aircraft landing (LA) to the drifting ice floe. The aim of the invention is to improve the accuracy of determining navigational parameters of the landing aircraft and increasing security by accounting planning and azimuthal instability and features and possible deformation of the runway. The method comprises that placed on the ice transponders is formed at the reference location transponders, and flying over the runway, are formed and indicate at all subsequent approach and landing side avoidance, corrections to the actual rate and other navigational parameters. Before performing approach manufac t overflew control, which resulted in the absence of the runway set deformation to form and display the message to permit landing. In this navigation parameters are generated in the coordinate system of the current position of the ice floe, which provided an automatic formation of transponders and runway coordinates floes before entering the landing set fact no deformation ldiny.2 yl. ff On