海军航空工程学院学报2017，Vol.32Issue(3)：284-289,294,7.DOI:10.7682/j.issn.1673-1522.2017.03.006
基于最优机动参数的靶弹变轨研究
Research on the Variable Trajectory Maneuvers of Target Missiles Based on the Best Penetration Maneuvers Parameter
毕开波 1张翼飞 1隋先辉1
作者信息
- 1. 大连舰艇学院导弹系,辽宁大连116018
- 折叠
摘要
Abstract
To solve the design problem of variable trajectory maneuver of target missiles, an integrated design model was presented. By closely cooperating between the control signals of displacements and overloads, the integrated design model could make target missiles to realize the maneuver of jump trajectory, the maneuver of snake-wriggling trajectory, the ma-neuver of pendulum trajectory, the maneuver of spiral trajectory, and so on. On this basis, the penetration effect models of variable trajectory maneuvers of target missiles were studied. The design methods of the best penetration maneuvers param-eter were put forward. According to these parameters, target missiles could realize the best penetration effect, promote train effect of air defense missile.关键词
导弹靶弹/突防效果/弹道变轨/机动参数Key words
target missile/penetration effect/variable trajectory maneuvers/maneuvers parameter分类
军事科技引用本文复制引用
毕开波,张翼飞,隋先辉..基于最优机动参数的靶弹变轨研究[J].海军航空工程学院学报,2017,32(3):284-289,294,7.
