The method of tracking maneuvering aircraft based on the model with random discontinuous structure using the maneuver intensity indicator information

Behavior maneuverable target in the conduct of air combat characterizes the implementation of complex maneuvers with large overloads. On-time electronic warfare support based on the -filtering algorithm that uses the model of a uniformly accelerated motion or motion with constant velocity, which is insufficient to describe the reality of the process.

Maneuvering target has a strong influence on the quality of maintenance. The late detection of start of the maneuver objectives often leads to the disruption of auto-tracking because of the appearance of large errors of servo meters from the inadequacy of models embedded in meters, the actual behavior goals. Reacquisition requires additional time, and this - the reason for failure of the first attack, which, in a highly battle is very important.

In connection with distinguished the circumstances of the modern and perspective electronic tracking means is advisable to include ad hoc device to detect and determine the intensity of the maneuver - indicators are intended to correct the parameters or structure of the tracking filter in line with the real situation.

Information to make decisions about maneuvering air target and its intensity can serve as the value of accelerating convergence.

Of particular interest is the construction of filters on the basis of the theory of systems with random discontinuous structure. A characteristic feature of information processing algorithms in systems with random discontinuous structure is the ability to integrate different models of movement of aircraft and the integration of information gauges and indicators. At the same time to improve the accuracy of ratings issued by the filters, by changing the filter structure on the testimony of indicators.