Modal method of optimization of energy flight control system of flying vehicles

The energy approach is a methodological basis of flying vehicles control systems development with extended requirements to quality of control. However, vehicles with strongly varying properties need adjustment of parameters of a control system. For purpose of parameters optimization the modal method is used. The version of a modal method of synthesis has been developed, allowing to calculate a feedback matrix without the use of iterative procedures, during one computing cycle. Results of modeling of the maneuverable high-speed aircraft are produced. These results have shown that the combination of rational energy approach to flight control and formal mathematical methods provide control quality practically identical in large flight envelope.