Article

Article title INERTIAL AIRCRAFT CONTROL AT INTENSE MANEUVERING AEROSPACE PURPOSES INTERCEPTION
Authors D.A. Milyakov, A.D. Kraylyuk
Section SECTION V. SYSTEM AND CONTROL POINTS
Month, Year 01, 2015 @en
Index UDC 629.7.058.54
DOI
Abstract Purpose of the article is to describe one of the possible approaches to the development of a method for managing inertial aircraft at interception intense maneuvering of air and space attack on stage homing. The objectives of the study include the analysis of the ways of development of air and space attack, as well as existing and applicable methods targeting aircraft and missiles; formulation drawbacks of existing methods of guidance, as well as new types of problems interception aerospace purposes, including the main interest is in aerospace manned and unmanned means of attack; algorithm development guidance for the purpose of intensive maneuvering the aircraft because of its inertia; studies of the proposed control method. The proposed method is a fundamentally new, eliminating the disadvantages of the classical methods of guidance in existing aircraft and homing missiles and providing all-round precision interception intense maneuvering targets by taking into account the angular velocity derivatives line of sight. In a study prepared by the process of homing performed simulation process intercepting aircraft-adapting high-speed maneuvering aerospace purpose. The simulation was performed in a wide range of maximum modulus of transverse acceleration and velocity goals, moving along a sinusoidal path, using the proposed method interception and existing (classic) methods of homing. Some results of the simulation method developed guidance, illustrated with drawings. Based on the results of the study concluded that the possibility of eliminating disadvantages of classical methods of guidance in existing systems homing missiles and aircraft, including by taking into account the proposed method to intercept application, which allows for stable interception in a wider range of angular velocities and accelerations.

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Keywords Aerospace attack vehicles; hypersonic aircraft; maneuverability; inertia of aircraft; guidance method.
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