SYNTHESIS OF A RANGE-MEASURING AND ANGLE-MEASURING CHANNEL FILTERING ALGORITHM TO ESTIMATE THE ACCELERATION OFA MANEUVERING AIR TARGET
An algorithm has been developed for filtering an estimate of the acceleration of an air target for an air-to-air guided missile based on two tracking channels. The estimates formed in the rangefinder channel are used in filtering the parameters of the relative motion of the rocket and the target in the goniometer channel, in which the acceleration of the air target is presented as a narrow-band process. The simulation results show high accuracy estimates of the acceleration of the air target of the developed algorithm compared to the existing one.