摘要
某制导弹药采用鸭式布局,执行机构为两对对称且垂直安装的"十字"鸭舵。论文根据"十字"鸭舵结构和特点,研究了由弹体转速、滚转姿态角和理论控制力求解两对舵实时舵偏角的方法,并进行试验验证,解决了"十字"鸭舵如何实现低旋转尾翼稳定弹所需的控制合力问题。
A Guided Projectile has two pairs of canards which equipping symmetric and upright. Base on the strcture and characteristic of this canards, the toothed of solving the canards deflexion angle by roll rate, roll angle and control force has been researched, and has been validated by experimentatiorL The problem of how to produce control force of finstabi lized projectile with low spin speed by two pairs of canards has been solved by this method.
出处
《舰船电子工程》
2014年第1期73-74,82,共3页
Ship Electronic Engineering
关键词
制导炮弹
鸭舵控制
滚转姿态
guided projectiles, canard control, roll angle
