Numerical Simulation for Ascending Trajectory of Submarine-Launched Carrier with Coupled Motion
-
摘要: 潜射运载器的无动力上浮弹道因受发射条件、海流等因素的影响会出现大攻角和大侧滑角, 进而表现出非线性特征, 传统弹道预报手段难以满足需求。基于动网格技术和刚体空间运动方程建立3D六自由度数值模型, 实现运载器与外流场的双向耦合, 通过改变初始条件对运载器的无动力上浮弹道进行仿真, 并与MK46鱼雷弹道模型的计算值进行比较。仿真结果表明, 上浮过程中俯仰角逐渐增大, 攻角先增大后减小; 上浮俯仰角及攻角峰值随着发射速度的增大而减小; 上浮时间、出水俯仰角随着发射深度的增大而增大。文中研究可为水下航行器的强机动弹道预报提供参考。Abstract: The unpowered ascending trajectory of a submarine-launched carrier presents large angle of attack and side-slip angle due to the effects of launching condition and ocean current, and then shows nonlinear characteristics. The conventional trajectory prediction method cannot meet the requirement of practical application. In this paper, a three-dimensional computational model with six degrees of freedom is established based on dynamic mesh and spatial kinetic equation of rigid body to achieve a two-way coupled simulation of the carrier and external flow field. The unpowered ascending trajectory of the submarine-launched carrier is simulated by changing the initial conditions, and the results are compared with that of the MK46 torpedo trajectory model. The comparison shows that: 1) the pitching angle gradually increases during the ascending process, while the angle of attack increases first and then decreases; 2) the ascent pitching angle and peak angle of attack decrease with the increasing launching speed; and 3) the duration of ascent and the pitching angle of breaking out of water increase with the increase in launching depth. This study may provide a reference for prediction of enhanced maneuvering trajectory of undersea vehicles.
-
[1] Xiong J. Guidance and Control Research on Underwater Unpowered Anti-Submarine Weapons[J]. Advanced Materials Research, 2013, 648: 323-327. [2] Pan G, Shi Y, Wang P, et al. Study on the Control Law for Water Trajectory of Unpowered Carrier under Wave Force[J]. Applied Mechanics & Materials, 2013, 401-403: 525-530. [3] Saraparung S. A Study of the World’s Naval Surface-to-air Missile Defense Systems[J]. 1984, 75(12): 1308-1327. [4] Smallwood D A, Whitcomb L L. Model-based Dynamic Positioning of Underwater Robotic Vehicles: Theory and Experiment[J]. Oceanic Engineering IEEE Journal of, 2004, 29(1): 169-186. [5] Caccia M, Indiveri G, Veruggio G. Modeling and Identification of Open-frame Variable Configuration Unmanned Underwater Vehicles[J]. IEEE Journal of Oceanic Engineering, 2002, 25(2): 227-240. [6] 袁绪龙, 王亚东, 张宇文. iSIGHT在运载器出水弹道优化设计中的应用[J]. 鱼雷技术, 2010, 18(4): 253-257.Yuan Xu-long, Wang Ya-dong, Zhang Yu-wen. Application of iSIGHT to Optimization Design of Water-exit Trajectory for Missile Carrier[J]. Torpedo Technology, 2010, 18(4): 253-257. [7] 仲维国, 张嘉钟. 潜射航行器的水下弹道模拟[J]. 弹道学报, 2005, 17(1): 8-12.Zhong Wei-guo, Zhang Jia-zhong. Simulation of Submarine Vehicle to Underwater Trajectory[J]. Journal of Ballistics, 2005, 17(1): 8-12. [8] 马震宇, 刘曜. 无动力运载器水弹道特性计算[J]. 四川兵工学报, 2011, 32(6): 4-7.Ma Zhen-yu, Liu Yao. Computing of Water Ballistic Trajectory Characteristic for Unpowered Vehicle[J]. Journal of Sichuan Ordnance, 2011, 32(6): 4-7. [9] 杜晓旭, 宋保维, 胡海豹, 等. 潜空导弹运载器水下弹道仿真研究[J]. 系统工程理论与实践, 2007, 27(10): 172-176.Du Xiao-xu, Song Bao-wei, Hu Hai-bao, et al. Simulation of Submarine-Aerial Missile Carrier‘’s Water Trajectory[J]. Systems Engineering-Theory & Practice, 2007, 27(10): 172-176. [10] Shih T H, Liou W W, Shabbir A, et al. A New Kappa-epsilon Eddy Viscosity Model for High Reynolds Number Turbulent Flows-model Development and Vali-dation[J]. Linthicum Heights Md Nasa Center for Aero-space Information, 1995, 24(3): 227-238. [11] 严卫生. 鱼雷航行力学[M]. 西安: 西北工业大学出版社, 2005. [12] 张宇文. 鱼雷外形设计[M]. 西安: 西北工业大学出版社, 1998.
点击查看大图
计量
- 文章访问数: 744
- HTML全文浏览量: 1
- PDF下载量: 403
- 被引次数: 0