Synthesis of the quad-rotor flight control system

Abstract

The problem of the synthesis of the advanced algorithms for quad-rotor horizontal flight control is considered. The modified procedure of the linear quadratic synthesis is applied. Two kinds of algorithms are considered here. The control goal in the 1st case is the achieving the certain point in the given navigation frame, meanwhile for the 2nd case the control goal is the stabilization of the cruise speed. Represented examples prove the efficiency of both kinds of algorithms.