INDICATORS OF MANEUVERABILITY OF SHOCK UNMANNED AIRCRAFT WITH FIXED WING AS A FACTOR IN ENSURING SURVIVABILITY

Modern development of information systems creates the conditions for the development of the latest tools that allow you to automate and distance the operator and the management object, and thus more efficiently implement control processes. With the increase in complexity of automated systems and information technologies, their functionality increases and new opportunities for their use are increased. The intensive introduction of robotic systems caused by armed aggression is also available in the military sphere, in particular for transportation, intelligence and attacking actions. The operation of the video transmitter on board the mobile robotic complex has allowed to provide feedback channel with the operator, which significantly improved the capabilities of these systems. Significant achievements in the outlined direction were achieved in the creation of unmanned aerial vehicles of the shock and reconnaissance class. It is important for them to ensure the combat problem in the face of active opposition of the enemy. It is for this purpose that the aerial apparatus is equipped with a number of applications for protection against electronic warfare and fire damage. The means of counteracting radio electronic influence are intended to protect the channels of obtaining coordinates and control, and from fire damage by means of air defense, protecting the apparatus can be used by the use of structural features that improve its shunting characteristics. Systems of weapons of air defense have some technical capabilities to respond to air purposes, that is, the detection of a target, the transfer of targets, and a rocket shot, which in flight also searches for targets and completion, which is also spent some time. Since these capabilities are due to their tactical characteristics, it is relevant to improve the characteristics of maneuverability in the UAV, which will allow to change its position in space during a time equal to, or is less than the time of response of the enemy air defense system, that is, it will allow him to perform the evasion maneuver. Possible ways to solve this problem are to introduce an improved electromagnetic type UAV type control system, which have less inertia compared to existing types and can provide rapid and unambiguous reincarnation of steering surfaces at a certain fixed angle and retention in such a clear position. Changing the position of the apparatus in the space in this case is due to the deviation of the steering surfaces on the steady angle with different time in the rejected position.