ARMAMENT CONTROL METHOD FOR MULTIFUNCTIONAL TACTICAL AIRCRAFT AND A SYSTEM FOR ITS IMPLEMENTATION Russian patent published in 2021 - IPC F42D1/00 

FIELD: multifunctional tactical aircraft armament control.

SUBSTANCE: invention relates to the field of armament control for multifunctional tactical aircraft. The method consists in creating an interactive information and display system, which provides the recording of data on the features of the upcoming flight into the RAM from the flight task carrier, identification and tracking of air and ground targets during the flight based on the use of radar and optical channels, recognition of helicopters in the mode hovering based on the analysis of Doppler frequencies, determination of small-sized ground targets that are hardly noticeable in the radar spectrum of radiation based on changes in the radiation pattern, provision of intellectual support to the crew, depending on the situational situation, performance of training and combat functions of a fighter, interceptor, bomber, attack aircraft, jammer, operational reconnaissance officer, coordinated in space and time, implementation of target designations for guided missiles in conditions of target maneuvering based on taking into account its angular velocity and ensuring launching missiles in conditions of covert observation of the target. The armament control system of multifunctional aircraft contains a control and registration system, complexes of navigation and aerobatic aids, an onboard information exchange channel, a unit for analyzing target movement parameters, a unit for determining possible missile launch zones, optical-location sighting devices and electronic countermeasures, a radar sighting system, a control system for weapons and passive counteraction, a set of weapons and passive counteraction, a communication and identification system, two multifunctional indicators, a collimator indicator on the windshield with a television camera, operational controls, backup indication devices, a portable storage medium of initial data and an on-board computer system. In the latter, the computational and logical modules of the combined database are interconnected along the computational exchange line, the formation of navigation and flight parameters, the formation of target designation and application parameters, the formation of displayed information, the input-output of exchange control, the recognition in the radar spectrum of helicopters in hover mode, spectrum of ground targets, formation of parameters of emergency analysis of flight, long-range and short-range air battles and battles on the surface.

EFFECT: expansion of functionality by ensuring the launch of the rocket in conditions of covert observation of the target, when it moves along an inclined trajectory.

3 cl, 7 dwg