Study on Coordination Technology of Guidance Integrated Fuze and Gimbaled Warhead
XU Jun-fen
Abstract
XU Jun-fen
Abstract
The kill probability calculating models of one-missile to one-target for the gimbaled warhead, which is designed to fire the fragments in the target direction,are studied in order to optimize lethality. Two encounter concepts of side-attack and forward-intercept at endgame are formulated in the missile coordinate system. The kill probability is calculated using Monte-Carlo method. Based on the circular spray pattern with uniform pattern density,the optimum lethal radius is established for forward-intercept concept. And then the effects of missile-target relative velocity and miss distance on kill probability are analyzed. According to the study,the preferred conditions for side-attack or forward-intercept are proposed: if vr≥1 700 m/s and ρ≤2. 5 m or vr≥3 000 m/s and ρ≤4 m,then the encounter concept of forward-intercept is preferable; In other cases,the encounter concept of side-attack is preferable.
A significance statement is not available in the OpenAlex record.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
The kill probability calculating models of one-missile to one-target for the gimbaled warhead, which is designed to fire the fragments in the target direction,are studied in order to optimize lethality. Two encounter concepts of side-attack and forward-intercept at endgame are formulated in the missile coordinate system. The kill probability is calculated using Monte-Carlo method. Based on the circular spray pattern with uniform pattern density,the optimum lethal radius is established for forward-intercept concept. And then the effects of missile-target relative velocity and miss distance on kill probability are analyzed. According to the study,the preferred conditions for side-attack or forward-intercept are proposed: if vr≥1 700 m/s and ρ≤2. 5 m or vr≥3 000 m/s and ρ≤4 m,then the encounter concept of forward-intercept is preferable; In other cases,the encounter concept of side-attack is preferable.
Key concepts: Warhead, Fuze, Missile, Gimbal, RADIUS, Monte Carlo method, Aerospace engineering, Simulation