反舰导弹姿态角、质心复合末端立体机动控制  

Attitude Angle and Centroid Hybrid Control of Terminal Tridimensional Maneuver for Supersonic Anti-ship Missile

作　　者：顾文锦[1] 李聪颖[1] 杨迎化[1] 王士星[1] 

机构地区：[1]海军航空工程学院自动控制系,山东烟台264001

出　　处：《弹箭与制导学报》2004年第S6期264-267,270,共5页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：文中比较了几种末端机动控制方式的不同点,分析了它们的应用场合。并给出了可在驾驶仪方案、惯导方案下的应用,采用姿态角、质心复合控制方式,在增益调度 PID 控制系统作用下,实现了侧向平面、纵向平面与斜平面内的蛇行机动,非平面的摆式机动、螺旋机动与椭圆螺旋等机动形式,给出了一体化公式,并在VC_(++)下进行了六自由度非线性模型的全弹道仿真。Several kinds of terminal tridimensional maneuver control methods were compared in this article,followed with the analysis of their application situation.Different kinds of maneuver methods,such as zig-zag maneuver in lateral plane,longitudinal plane,inclined plane,and pendulum maneuver,barrel roll maneuver and ellipse roll maneuver were realized by attitude angle and eentroid hybrid control command in gain schedule PID attitude control autopilot and INS. Incorporate formula of these maneuver methods is brought out.Full trajectory 6DOF nonlinear simulations were carried out in VC_(++).

关 键 词：反舰导弹 末端机动 增益调度控制 蛇行机动 摆式机动 螺旋机动 

分 类 号：TJ761.14[兵器科学与技术—武器系统与运用工程]