Algorithm for Operational Optimization of Two-Stage Hypersonic Unmanned Aerial Vehicle Branching Path

The algorithm for calculating the path of two-stage hypersonic unmanned aerial vehicle consisting of unmanned carrier aircraft and unmanned orbital aircraft is proposed. Optimal values of phase coordinates and controls at points of structural transformations of the branching path of two-stage hypersonic unmanned aerial vehicle are calculated. The proposed algorithm allows to optimize the path of two-stage hypersonic unmanned aerial vehicle in any section of the path, including the separation phase and initial disengagement of orbital stage from air launch aircraft, taking into account the mutual influence of stages.