Algorithm of Estimation of Boundaries of Accessibility Area of Flying Vehicle with Regard for Thrust

Problems of estimation of accessibility area of flying vehicle in 3D-space are considered. Description of boundaries of accessibility area is parameterized, parameters being as follows: angle of roll of the flying vehicle, a position of a point of switching a sign of the tangential acceleration (thrust) within the time interval, an also a position of a point of switching/turning off the normal acceleration. Based on the parameterization of the flying vehicle control an algorithm is obtained for calculation of boundaries of the 3D accessibility area for determination of controls of the flying vehicle.