FIELD: armament; rocket equipment.
SUBSTANCE: invention can be used in development of short-range complexes and systems with aircraft maneuvering on target. Invention is intended for analysis of aircraft guidance on different types of targets, including intensive maneuvering, with the possibility of correction of parameters of elements of aircraft control system for determination of technical capabilities of increase of control accuracy in specific tactical situations without carrying out natural experiments. Model is based on use of transfer functions of short-range aircraft control loop. Essence of the model consists in the fact that AC control commands are generated in two mutually independent channels (azimuth and elevation angle), and as initial information on input of model is supplied mixture of angular coordinates of target and angular noise generated by separate radar model of target.
EFFECT: thus obtained homing path parameters enable to analyze homing characteristics of various types of aerial targets in various tactical situations with sufficient accuracy and reliability.
1 cl, 16 dwg
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