Movement Analysis of the Aircraft Optoelectronic Tracking System in Lateral Plane

The paper describes the analysis of the movement transformation of the tracking optoelectronic system of a fast aircraft. The transformation is performed in the selected phase of flight in the lateral planes. The mathematical model of the aircraft was extended by an optoelectronic tracking system model and a weapon movement model. Mathematical models of the proposed integrated system are described by transfer functions, which are transferred to the state space with evaluation in the simulation environment. Control of the automatic tracking system on the aircraft was designed with the ability to control the tracking line on the selected tracking object in order to reduce the impact of the error in the dynamics of the aircraft movement, the movement of the monitored object and the optoelectronic tracking system. The laws of control of the optoelectronic system and the aircraft have been defined. The optimization of the proposed methods was realized under changing flight conditions of the aircraft and the tracking object as optimal gains. Optimal gains are determined by the values given in the difference speed and altitude for aircraft flight.