TOTAL ENERGY CONTROL OF AIRCRAFT LATERAL MOTION
S. A. Belokon, A. P. Gerasimova, Yu. N. Zolotukhin, K. Yu. Kotov, A. S. Maltsev
Institute of Automation and Electrometry, Siberian Branch, Russian Academy of Sciences, Novosibirsk, Russia
Keywords: unmanned aerial vehicle, total energy control, simulation modeling, lateral motion control, inverse dynamics
Abstract
The article considers the creation of a control system for the lateral motion of an aircraft based on an approach similar to the control of the total energy in a longitudinal channel. The structure of the control system is presented. It includes an aircraft-independent core and blocks for transition rudder and ailerons deflection commands. These blocks are based on the principle of inverse dynamics. An approach to creating a control system is proposed. Simulation modeling of the behavior of three aircraft with different aerodynamic configurations is carried out. The control quality is studied using a numerical modeling method.
|
