Hyper Angle Pose.pdf ##HOT##
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2.1.2 Hypersonic Target ModelThe target maneuvers for defensive tactics can be divided into two categories: boost-gliding and boost-casing. The target maneuvers in boost-gliding are presented as an incremental change of its velocity and altitude in the horizontal plane. The motion trajectory of the target can be described as Figure 1. The following rules govern the maneuvers: (1) the target adopts a constant altitude to avoid a collision with the interceptor; (2) the total time of the boost phase is constant; (3) the target accelerates first and decelerates last; (4) the target maneuvers to intercept at a specific range and certain angle with the trajectory of the interceptor; (5) the target maneuvers at a constant speed. The target in boost-casing adopts a deceleration and acceleration maneuver to curve and intercept the interceptor. The motion trajectory is defined as Figure 1. The following rules govern the maneuvers: (1) the total time of the boost phase is constant; (2) the target accelerates first; (3) the target maneuvers at a constant speed.
As the target maneuvers in boost-gliding, the target’s velocity and altitude can be described as (pursuer’s time, target’s time, velocity, altitude, altitude) in the laboratory frame, where and are the initial values of and, respectively. The pursuer maneuvers at a constant velocity, and the maneuvering sequence is described as: (1) the target boosts to the initial altitude; (2) the target maneuvers toward the trajectory of the interceptor; (3) the target decelerates and maintains constant altitude. Boost phase is the initial stage of the interceptor’s acceleration, the total time of the boost phase is constant. The flight period is the second stage, the time of the boost phase is constant. The third stage is the deceleration phase, and the target maneuvers and maintains constant altitude. The maneuvering sequence is described as: (1) the target boosts to the initial altitude; (2) the target maneuvers to intercept at a certain range and angle with the trajectory of the interceptor; (3) the target decelerates and maintains constant altitude. For instance, if, then the pursuer intercepts the target in a head-on and constant-velocity state. The time of the boost phase is 0.5 s. The boost phase lasts for 2.
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