| 反舰导弹末端立体机动的质心控制指令设计 |
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| 引用本文： | 顾文锦,李聪颖,王士星,尚安利.反舰导弹末端立体机动的质心控制指令设计[J].飞行力学,2004,22(4):49-52. |
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| 作者姓名： | 顾文锦 李聪颖 王士星 尚安利 |
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| 作者单位： | 1. 海军航空工程学院,自动控制系,山东,烟台,264001
2. 海军航空工程学院,研究生一队,山东,烟台,264001 |
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| 摘 要： | 比较了几种末端机动控制方式的不同,分析了它们的应用场合.采用姿态控制下的质心控制方式,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,以及非平面的螺旋机动、椭圆螺旋机动等形式,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.
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| 关 键 词： | 反舰导弹 末端机动 增益调度控制 蛇行机动 螺旋机动 |
| 文章编号： | 1002-0853(2004)04-0049-04 |
| 修稿时间： | 2003年10月16 |
Instruction Design for Centroid Control of Terminal Tridimensional Maneuver for Anti-ship Missiles |
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| GU Wen-jin,LI Cong-ying,WANG Shi-xing,SHANG An-li.Instruction Design for Centroid Control of Terminal Tridimensional Maneuver for Anti-ship Missiles[J].Flight Dynamics,2004,22(4):49-52. |
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| Authors: | GU Wen-jin LI Cong-ying WANG Shi-xing SHANG An-li |
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| Institution: | GU Wen-jin~1,LI Cong-ying~2,WANG Shi-xing~1,SHANG An-li~2 |
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| Abstract: | Several kinds of terminal tridimensional maneuver control methods were compared in this article, and followed with the analysis of their application situation. Different kinds of maneuver methods, such as zig-zag maneuver in lateral plane, longitudinal plane, and inclined plane, barrel roll maneuver and ellipse roll maneuver were realized by centroid control command in gain schedule PID attitude control system. Incorporate formula of these maneuver methods is brought out. Full trajectory 6DOF nonlinear simulations were carried out in VC++. |
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| Keywords: | anti-ship missile terminal maneuver gain schedule control zig-zag maneuver barrel-roll maneuver |
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