Dynamic characteristics of rotating disk-shaped flight vehicle during skipping considering configuration
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摘要:
旋转碟状飞行器可通过模仿石块水漂有效提升海上拒止环境突防能力,保障连续水漂和降低冲击过载是其水漂动力学设计的关键。水漂动力学特性主要取决于初始运动参数,而构型参数也是影响水漂过程位姿运动和载荷分布的重要因素。针对旋转碟状飞行器水漂动力学特性影响参数耦合、作用机制不清等问题,本文提出一种旋转碟状飞行器的参数化构型,并基于任意拉格朗日-欧拉(ALE)单元法和罚函数法完成其水漂仿真分析,分别得到构型参数和初始运动参数对其水漂动力学特性的影响规律,并探究2类参数的耦合关系。结果表明,增大边缘曲率半径可有效减小水漂过程中飞行器所受过载,而增大自旋角速度可大大提高飞行器姿态稳定性。所提研究可为旋转碟状飞行器等新型水漂式反舰设计提供参考。
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关键词:
- 旋转碟状飞行器 /
- 水漂动力学 /
- 运动参数 /
- 构型参数 /
- 任意拉格朗日-欧拉单元法
Abstract:The rotating disk-shaped vehicle can significantly enhance penetration capabilities in denied environments by imitating stone skipping. Ensuring continuous skipping and reducing impact overload are critical dynamic design objectives. While setup settings are also important for the vehicle’s posture motion and load distribution during skipping, the dynamic aspects of skipping are mostly determined by the starting motion parameters. Therefore, the parameters affecting the dynamic characteristics of the rotating disk-shaped vehicle are strongly coupled, making the mechanisms of their influences remain unclear. This paper proposes a parameterized configuration for the disk-shaped vehicle. Utilizing the arbitrary Lagrange-Euler (ALE) method and penalty function method, a simulation analysis of the rotating disk-shaped vehicle is conducted. The study investigates the coupling relationship between configuration parameters and starting motion parameters and reveals their influence patterns on the vehicle's dynamic characteristics while skipping. The results demonstrate that increasing the edge curvature radius can effectively reduce the overload on the vehicle during skipping. Additionally, a better attitude stability can be achieved by increasing the spin rate. The findings presented in this paper can serve as valuable references for the design of new types of skipping anti-ship weapons, such as a rotating disk-shaped vehicle.
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表 1 状态方程参数取值
Table 1. Values of parameters in state equation
$ {\rho }_{0,{\mathrm{w}}}/\left(\text{kg}\cdot {\text{m}}^{{-3}}\right) $ $ C_{\mathrm{w}}/\left({\text{m}}\cdot {\text{s}}^{-1}\right) $ $ {\gamma }_{0{\mathrm{w}}} $ $ A_{\mathrm{w}} $ $ {S}_{1{\mathrm{w}}} $ $ {S}_{2{\mathrm{w}}} $ $ {S}_{3{\mathrm{w}}} $ $ w_{\mathrm{w}}/\left({\text{J}}\cdot {\text{m}}^{-3}\right) $ $ {\rho }_{0,{\mathrm{a}}}/\left(\text{kg}\cdot {\text{m}}^{{-3}}\right) $ $ {c}_{1{\mathrm{a}}} $ $ {c}_{2{\mathrm{a}}} $ $ {c}_{3{\mathrm{a}}} $ $ {c}_{4{\mathrm{a}}} $ $ {c}_{5{\mathrm{a}}} $ $ {c}_{6{\mathrm{a}}} $ $ w_{\mathrm{a}}/\left(\text{J}\cdot {\text{m}}^{-3}\right) $ 1 000 1 650 0.5 0.35 1.92 −0.096 0 1.9×105 1.225 0 0 0 0.4 0.4 0 2.1×105 表 2 几何模型参数
Table 2. Geometric model parameters
质量/kg 半径/m $ {I}_{x} $/(kg·m−2) $ {I}_{y} $/(kg·m−2) $ {I}_{{\textit{z}}} $/(kg·m−2) $ {k}_{1} $ $ {k}_{2} $ $ {k}_{3} $ 14 550.0 7.0 22 837.9 45 462.1 22 800.0 1.5 0.2 10 表 3 初始运动参数
Table 3. Initial motion parameters
速度/(m·s−1) 速度倾角/(°) 俯仰角/(°) 偏航角/(°) 自旋角速度/(rad·s−1) 100.0 −20.0 15.0 0 400.0 表 4 构型参数和初始运动参数影响规律
Table 4. The influence pattern of configuration parameters and initial motion parameters
影响因素 影响因素 V 过载 $\Delta \theta $ $\Delta \varphi $ $ {k}_{1} $ \ $ - $ $ + $ $ - $ $ {k}_{2} $ $ + $ $ - $ $ - $ $ + $ $ {k}_{3} $ $ + $ $ + $ $ - $ \ $\theta $ $ - $ $ - $ \ $ - $ V \ $ + $ $ + $ $ + $ 速度倾角 $ - $ $ + $ $ + $ $ + $ $\omega $ $ - $ $ + $ $ + $ $ - $ 注:首行中的V为旋转碟状飞行器离开水面后的速度大小;过载为飞行器在水漂过程中所受的最大过载;“$\Delta \theta $”“$\Delta \varphi $”为飞行器离开水面后与初始时刻的角度之差的绝对值,即角度的变化量,可以表示飞行器姿态的稳定性;“\”表示该参数不随初始参数单调变化;“$ + $”表示正相关,“$ - $”表示负相关。 -
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