The algorithm for determining the switch rule of continuous steering on two-channel flying objects with the requirements of normal acceleration

Abstract

The article deals with a solution to build an algorithm for determining the switch rule of continuous steering pairs on the two-channel flying objects with the requirement of normal acceleration while approaching the maneuvering air target. The content of this paper focuses on determining the dependence of the attack angle and the edge sliding angle on the steering deflection angle. Thereby, the authors have built the dependent expression of the steering deflection angle on the desired normal acceleration. Through the analysis of a mathematical model describing the flight kinematics of flying objects, the authors have determined the switching rule of continuous steering pairs is a harmonic function. Where frequency is the rotation speed of the longitudinal axis, amplitude and phase as a function of the flying object’s characteristics and the desired normal acceleration.