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一种实现垂直攻击的导弹末制导律研究
Study of Terminal Guidance Technique of Missile in Vertical Attack
【摘要】 为了使导弹的战斗部能够发挥最大的效能或使导弹能够实现对特殊目标的打击,研究了一种纵向制导律.此制导律能够对落角进行约束,从而使导弹实现对目标的垂直攻击.对传统比例制导律进行了改进,在充分发挥导弹机动能力的条件下,设计了一种既能够击中目标,又能够满足对落角要求的轨迹预测比例制导律.最后通过仿真,验证了此制导律在对目标实现垂直攻击中的可行性.
【Abstract】 A longitudinal guidance law for vertical attack is designed to improve the effectiveness of missile or to attack special targets.In consideration of maneuverable ability of missile,a track forecast guidance law is presented to meet the requirement of falling angle and to hit targets precisely based on traditional proportional guidance law.Simulation is carried out to validate the feasibility and effectiveness of the guidance law in vertical attack.
- 【文献出处】 战术导弹技术 ,Tactical Missile Technology , 编辑部邮箱 ,2006年03期
- 【分类号】TJ765.3
- 【被引频次】13
- 【下载频次】325