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Article title CONFIGURING MANEUVER OF PLANNED AEROBALLISTIC AIRCRAFT
Authors V.I. Goncharenko, L.D. Gorchenko
Section SECTION I. UNMANNED AERIAL SYSTEMS
Month, Year 01, 2016 @en
Index UDC 629.192
DOI
Abstract This article discusses aeroballistic aircraft type gliding without propulsion. A method for selecting a configuration aeroballistic maneuvers of aircraft during the span of control of the air-space zones by means of a missile and air defense. The essence of the method is to advance zigzag arrangement in the space of a set of so-called anchor points, consistent guidance aeroballistic aircraft which determines its trajectory to maneuver. Despite the fact that the task of forming a path aeroballistic aircraft remains a subject of research in recent years, the solution of this problem is not trivial, and requires consideration of many factors associated primarily with features implemented targeting method. Consistent guidance aeroballistic aircraft on the pivot points convenient to consider using the method of guidance "on the required acceleration" algorithm which is a solution in each cycle guidance boundary ballistic problem with the definition of the required apparent acceleration that transforms aeroballistic aircraft from the current phase state to the desired end. The proposed method of selecting a configuration aeroballistic maneuvers the aircraft to the terminal end portion of the trajectory over the previously developed allows the planning of the reference trajectory to use all disposable current resource control on the formation maneuverable trajectory aeroballistic aircraft. Said method can be formed trajectory planning aeroballistic aircrafts both known types of maneuvers and maneuvers with arbitrary shape in view of the restrictions on the control parameters. Thus, the advantages of the proposed method are, firstly, the use of all existing at the moment of flight resource lateral control aeroballistic aircraft formation antitheft maneuver, secondly, the formation of maneuver of any configuration by the appropriate placement of reference points, taking into account compliance with the restrictions on the control parameters . Checking the effectiveness of maneuvers carried out by modeling interception aeroballistic aircraft for any initial arrangement of starting positions regarding the anti- aircraft missiles protected object.

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Keywords Aeroballistic aircraft; pivots path; guidance of the aircraft according to the method required acceleration; a method of selecting the configuration antitheft maneuver.
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