METHOD trajectory control of the aircraft with flight ZONE adverse weather conditions

摘要

A method of controlling manned and unmanned aerial vehicles (LA) with flight hazardous areas with adverse weather conditions from the control (command) of paragraph (DP), which consists in the fact that the withdrawal of the aircraft to the intended flight path is produced along the path detour danger zone (OZ) to adverse weather conditions with a predetermined rate φ, characterized in that the OZ approximated ellipse, and when approaching aircraft trajectory with PH is corrected by replacing the predetermined rate φLA on to pc φ, calculated according to the rule: where w w- velocity vector components managed LA defined as: φ- orientation angle of the danger zone with unfavorable weather conditions, a and b - axis of the ellipse; u, u- variables determining the position coordinates of the aircraft with respect to managed hazardous area center in a coordinate system associated with the direction of axes of the ellipse, is defined as: where x and y- coordinates of the center OZ (elliptical approximation); x and y - coordinates managed aircraft; α - angle determining the direction vector of aircraft velocity Appar ata relatively dangerous area with the rotation of the earth coordinate system through the angle φ, defined by the rule: gdei- components of the relative velocity vector of the aircraft managed based motion PH are defined as: u components of the velocity vector of the dangerous area of ​​movement with unfavorable weather conditions, components of the vector u speed aircraft managed, defined by the rule: where V - velocity value managed LA; φ- managed rate value LA, the LA managed adjustment path begins at the moment to