Control of aerial vehicle of non-typical designs in automatic mode

Non-standard layouts are increasingly used for modern aerial vehicle, especially unmanned or manned in automatic control mode, due to the complexity of the design for new tasks: asymmetric forms of helicopter and multi-rotor vehicles and the presence of loads on the external load, “flying wing” without vertical plumage, asymmetric arrangement of the bearing surfaces of cruise missiles. It is usually impossible to apply control methods to such vehicles based on traditional methods of simplifying mathematical models of objects, in particular, decoupling control channels. One of the classes of unmanned aerial vehicles is considered in the work and a method for constructing a trajectory control system based on the principle of error control and elimination of intermediate tasks of maintaining accurate angular orientation is proposed.