毕业论文

打赏
当前位置: 毕业论文 > 机械论文 >

导弹转速-攻角闭锁现象的理论探究

时间:2022-05-26 22:32来源:毕业论文
研究了闭锁运动的规律,发现闭锁稳态转速的方向不仅和初始条件有关还和不同参数条件下稳态解的情况有关;对于存在两个反向的稳态转速的情况

摘要为了研究转速-攻角闭锁现象发生的机理和规律,推导了弹箭运动的动力学模型,进 而建立了转速-攻角闭锁的数学模型,利用劳斯判据,给出了解析形式的转速-攻角闭锁 运动的稳定性条件。以某导弹为例通过数值仿真,成功预示了闭锁现象的发生;求出了 不同参数条件下,闭锁稳态参数的解析解,通过数值仿真验证了解析解具有较好的精度; 研究了闭锁运动的规律,发现闭锁稳态转速的方向不仅和初始条件有关还和不同参数条 件下稳态解的情况有关;对于存在两个反向的稳态转速的情况,找出了全初始攻角方向 角下都不会发生稳态反转的初始转速-初始攻角区域。将解析形式的稳定性条件作为约 束,利用稳态解析解给出了稳态转速的优化设计模型,进行求解得到了较好的优化结果。81013

毕业论文关键词 转速-攻角闭锁 解析解 稳定性 优化设计模型

Title Analysis of Spin-Yaw Lock-In for a Rotationally Symmetric Missile

Abstract In order to study the mechanism and law of spin-yaw lock-in, the equations of motion were derived and thus, the mathematic model of spin-yaw lock-in motion was demonstrated。 The analytic stability condition of lock-in was given by Routh criterion,which can be used as an constraint in the later optimal design for lock-in spin.Taking a missile for an example, the paper shows that the lock-in of the coning motion and the rolling motion can occur by numerical integration of the equations of motion。 The analytical solutions for spin rate, amplitude, and phase angle for the steady-state equilibrium motion were found under different conditions。 The solutions were evaluated valid by comparison with numerical integration。 Moreover, the paper shows that the occurrence of positive or negative lock-in spin is determined not only by initial conditions but the solutions for equilibrium motion, because there can be only one lock-in spin under some conditions。 For the conditions with two opposite lock-in spin, calculations have identified regions of an initial spin rate-amplitude plane that determine only one spin can occur over all initial phase angle。 Finally, we attempted an optimal design model for lock-in spin is presented as an application of the spin-yaw lock-in model to the design of projectiles or missiles。

Keywords  spin-yaw lock-in  analytical solutions  stability  optimal design

本科毕业设计说明书 第 I  页

1  绪论 1

1。1  研究背景 1

1。2  研究现状 2

1。3  本文的研究内容 6

2  弹箭动力学模型 7

2。1  坐标系及变量定义 7

2。2  空气动力和力矩 8

2。2。1  气动力 8

2。2。2  气动力矩 9

2。2。3  非线性诱导力矩 12

2。3  质心运动及绕心运动方程 13

2。4  阻力方程和转速方程 15

2。5  复攻角运动方程 16

3  转速-攻角闭锁的数学模型 导弹转速-攻角闭锁现象的理论探究:http://www.youerw.com/jixie/lunwen_94372.html

------分隔线----------------------------
推荐内容