Design and visualization of 3D reconstruction of aircraft maneuver movements library
-
摘要:
机动动作库是飞机空战仿真的重要基础,可靠的、具有针对性的机动动作库能够提高空战仿真的真实性和应用价值。为了建立具有针对性的机动动作库,提出了一种通过三维逆向建模进行气动特性计算再建立飞机机动动作库的技术途径,对气动参数未知飞机的空战仿真问题提供了技术支撑。首先,对飞机的几何外形进行了三维重建,计算分析了其纵向气动特性;然后,将气动数据加入飞行仿真的限制环节,设计了针对该型飞机典型战术动作的机动动作库;最后,基于MATLAB函数进行了机动动作的可视化研究。研究结果表明:机动动作库体现了对于飞机类型的针对性和可靠性,可视化实现了飞行轨迹和飞机姿态的三维显示及参数游标,为空战决策、空战仿真模拟训练和提高作战效能奠定了基础。
Abstract:Maneuver movements library is an important basis for aircraft air combat simulation. Reliable and targeted maneuver movements library can improve the authenticity and application value of air combat simulation. In order to establish a targeted maneuver movements library, a technical approach of calculating aerodynamic characteristics through 3D reverse modeling and then establishing the maneuver movements library of the aircraft is proposed, which provides technical support for the air combat simulation of aircraft with unknown aerodynamic parameters. Firstly, the aircraft's geometry was reconstructed in three dimensions, and its longitudinal aerodynamic characteristics were calculated and analyzed. Secondly, the aerodynamic data was added into the restricted link of flight simulation, and a maneuver movements library for the typical tactical movements of the aircraft was designed. Finally, based on MATLAB function, the visualization of maneuver movements was studied. The results show that the maneuver movements library reflects the pertinence and reliability of aircraft types, and visualizes the 3D display of flight trajectory and aircraft attitude and the parameter cursor, which lays a foundation for air combat decision-making, air combat simulation training and combat effectiveness improvement.
-
表 1 不同网格数下升力系数和阻力系数计算结果
Table 1. Calculation results of lift coefficient and drag coefficient with different mesh quantities
网格分类 网格数/104 CL CD 粗网格 483 5.241 4×10-1 7.591 9×10-2 中网格 922 5.235 6×10-1 7.612 7×10-2 细网格 1 473 5.224 3×10-1 7.754 8×10-2 方差 5.041 5×10-7 5.240 1×10-7 -
[1] 朱可钦, 董彦非. 空战机动动作库设计方式研究[J]. 航空计算技术, 2001, 31(4): 50-52. https://www.cnki.com.cn/Article/CJFDTOTAL-HKJJ200104014.htmZHU K Q, DONG Y F. Study on the design of air combat maneuver library[J]. Aeronautical Computing Technique, 2001, 31(4): 50-52(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKJJ200104014.htm [2] 梁鸿飞, 范广才, 董彦非. 空战战法训练系统目标机飞行轨迹实现[J]. 计算机仿真, 2005, 22(12): 32-34. https://www.cnki.com.cn/Article/CJFDTOTAL-JSJZ200512011.htmLIANG H F, FAN G C, DONG Y F. Generation of target aircraft's flight track in air combat plan simulation[J]. Computer Simulation, 2005, 22(12): 32-34(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-JSJZ200512011.htm [3] 程泉, 李嘉林, 胡孟权. 空战训练模拟系统目标敌机生成问题的研究[J]. 计算机测量与控制, 2006, 14(12): 1663-1664. https://www.cnki.com.cn/Article/CJFDTOTAL-JZCK200612025.htmCHENG Q, LI J L, HU M Q. Research of target drone for air war training simulation system[J]. Computer Measurement & Control, 2006, 14(12): 1663-1664(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-JZCK200612025.htm [4] 刘雪松. X-51A高超声速飞行器三维重建及气动/隐身特性分析[D]. 南京: 南京航空航天大学, 2015: 10-28.LIU X S. Three-dimensional reconstruction and analysis of aerodynamic and stealth characteristic of X-51A hypersonic vehicle[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2015: 10-28(in Chinese). [5] HORN B K P. Shape from shading: A method for obtaining the shape of a smooth opaque object from one view[D]. Boston: Massachusetts Institute of Technology, 1970. [6] VOGEL O, BREUB M, WEICKERT J. Perspective shape from shading with non-Lambertian reflectance[C]//Proceedings of DAGM Symposium on Pattern Recognition. Berlin: Springer, 2008: 517-526. [7] TANKUS A, SOCHEN N, YESHURUN Y. Shape-from-shading under perspective projection[J]. International Journal of Computer Vision 2005, 63(1): 21-43. doi: 10.1007/s11263-005-4945-6 [8] 曾蔚, 王汇源, 刘莹奇, 等. 基于IR-SFS算法空间目标红外影像3D重建[J]. 中国光学, 2014, 7(3): 376-388. https://www.cnki.com.cn/Article/CJFDTOTAL-ZGGA201403005.htmZENG W, WANG H Y, LIU Y Q, et al. 3D reconstruction of space target IR image based on IR-SFS algorithm[J]. Chinese Optics, 2014, 7(3): 376-388(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-ZGGA201403005.htm [9] GUPTA S K, SHUKLA D P. Application of drone for landslide mapping, dimension estimation and its 3D reconstruction[J]. Journal of the Indian Society of Remote Sensing, 2018, 46(3): 1-12. doi: 10.1007/s12524-017-0727-1 [10] 昂海松, 于志伟. 以遮挡边界为判据的透视曲面体图像的三维重建方法[J]. 模式识别与人工智能, 1998, 11(3): 266-273. https://www.cnki.com.cn/Article/CJFDTOTAL-MSSB199803003.htmANG H S, YU Z W. 3D reconstruction of perspective curve surface objects with the criterion of occluding boundary from image[J]. Pattern Recognition and Artificial Intelligence, 1998, 11(3): 266-273(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-MSSB199803003.htm [11] 昂海松, 黄志刚, 陈杰. 未知摄影参数图象的三维特征逆变换[J]. 计算机应用与软件, 1996(5): 23-28. https://www.cnki.com.cn/Article/CJFDTOTAL-JYRJ199605003.htmANG H S, HANG Z G, CHEN J. 3D solid configuration reproduction from unknown parameter perspective image[J]. Computer Applications and Software, 1996(5): 23-28(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-JYRJ199605003.htm [12] 昂海松. 任意曲线透视投影的逆变换[J]. 工程图学学报, 1995(2): 38-45. https://www.cnki.com.cn/Article/CJFDTOTAL-GCTX502.006.htmANG H S. Inverse transform if arbitrary perspective projectioned curves[J]. Journal of Graphics, 1995(2): 38-45(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-GCTX502.006.htm [13] 昂海松, 于志伟. 复杂外形实体图像的三维重建[J]. 模式识别与人工智能, 1994, 7(4): 277-284. https://www.cnki.com.cn/Article/CJFDTOTAL-MSSB199404002.htmANG H S, YU Z W. 3-D object reconstruction of composed configuration from its images[J]. Pattern Recognition and Artificial Intelligence, 1994, 7(4): 277-284(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-MSSB199404002.htm [14] 王翔. 三维重建技术研究及其在飞行器外形设计中的应用[D]. 南京: 南京航空航天大学, 2010.WANG X. Research on 3D reconstruction technology and its application in the aircraft lofting[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2010(in Chinese). [15] 廖炎平, 刘莉, 王嘉博. 无人机外形参数化建模及CATIA二次开发[J]. 弹箭与制导学报, 2011, 31(5): 68-71. https://www.cnki.com.cn/Article/CJFDTOTAL-DJZD201105019.htmLIAO Y P, LIU L, WANG J B. Parameterization modeling of UAV configuration using API in CATIA[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011, 31(5): 68-71(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-DJZD201105019.htm [16] 王黎明. 基于CATIA CAA的飞行器参数化三维外形设计及三维重建[D]. 南京: 南京航空航天大学, 2014.WANG L M. Three-dimensional reconstruction and parametric design of aircraft configuration based on CATIA CAA[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2014(in Chinese). [17] 钟友武, 柳嘉润, 杨凌宇, 等. 自主近距空战中机动动作库及其综合控制系统[J]. 航空学报, 2008, 29(S1): 114-121. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB2008S1018.htmZHONG Y W, LIU J R, YANG L Y, et al. Maneuver library and integrated control system for autonomous close-in air combat[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(S1): 114-121(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB2008S1018.htm [18] SHAW R L. Fighter combat-tactics and maneuvering[M]. Annapolis: The United States Naval Institute Press, 1985: 139-141. [19] QUÉAU Y, MÉLOU J, CASTAN F, et al. A variational approach to shape-from-shading under natural illumination[C]//Energy Minimization Methods in Computer Vision and Pattern Recognition. Berlin: Springer, 2017: 342-357. [20] 李介古. 计算机视觉的理论和实践[M]. 2版. 上海: 上海交通大学出版社, 1991: 30-37.LI J G. Theory and practice of computer vision[M]. 2nd ed. Shanghai: Shanghai Jiaotong University Press, 1991: 30-37(in Chinese). [21] 龚洁晖, 张慧. 基于工程图的三维重建研究[J]. 软件学报, 2008, 19(7): 1794-1805. https://www.cnki.com.cn/Article/CJFDTOTAL-RJXB200807024.htmGONG J H, ZHANG H. Research on solid reconstruction from engineering drawings[J]. Journal of Software, 2008, 19(7): 1794-1805(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-RJXB200807024.htm [22] 石岚峰, 邹北骥. 基于工程图三维重建中的预处理与信息提取技术研究[J]. 计算机应用研究, 2007, 24(4): 161-165. https://www.cnki.com.cn/Article/CJFDTOTAL-JSYJ200704046.htmSHI L F, ZOU B J. Research on pre-processing and information extracting for 3D reconstruction from engineering drawings[J]. Application Research of Computers, 2007, 24(4): 161-165(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-JSYJ200704046.htm [23] 于冲, 王旭, 董福安, 等. y+值对翼型气动参数计算精度的影响研究[J]. 空军工程大学学报(自然科学版), 2012, 13(3): 25-29. https://www.cnki.com.cn/Article/CJFDTOTAL-KJGC201203007.htmYU C, WANG X, DONG F A, et al. The study of effect of y+ on precision of pneumatic parameters of foil[J]. Journal of Air Force Engineering University(Natural Science Edition), 2012, 13(3): 25-29(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-KJGC201203007.htm [24] TINOCO E N, BRODERSEN O P, KEYE S, et al. Summary of data from the sixth AIAACFD drag pre diction workshop: CRM cases 2 to 5: AIAA 2017-1208[R]. Reston: AIAA, 2017. [25] 魏扬, 张登成, 赵保明, 等. 基于试飞数据的飞行模拟器气动模型校核[J]. 飞行力学, 2017, 35(1): 84-88. https://www.cnki.com.cn/Article/CJFDTOTAL-FHLX201701020.htmWEI Y, ZHANG D C, ZHAO B M, et al. Flight simulator aerodynamic model calibration based on flight test data[J]. Flight Dynamics, 2017, 35(1): 84-88(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-FHLX201701020.htm [26] 刘瑛, 李敏强, 张瑞峰. 复杂机动动作最优航迹控制模型及操纵特性分析[J]. 控制理论与应用, 2014, 31(5): 566-576. https://www.cnki.com.cn/Article/CJFDTOTAL-KZLY201405003.htmLIU Y, LI M Q, ZHANG R F. The optimal trajectory control model of the aircraft maneuver and its operation characteristics[J]. Control Theory & Applications, 2014, 31(5): 566-576(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-KZLY201405003.htm [27] 刘勋. 自动空战模拟中的机动决策和控制研究[D]. 西安: 西北工业大学, 2006: 13-15.LIU X. Study on maneuver decision and control in automatic air combat simulation[D]. Xi'an: Northwestern Polytechnical University, 2006: 13-15(in Chinese). [28] 李嘉林, 胡孟权. 飞机常规机动仿真的过载控制模型设计研究[J]. 飞行力学, 2013, 31(3): 213-216. https://www.cnki.com.cn/Article/CJFDTOTAL-FHLX201303005.htmLI J L, HU M Q. Research on the design of load control model for aircraft conventional maneuver simulation[J]. Flight Dynamics, 2013, 31(3): 213-216(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-FHLX201303005.htm [29] 陈廷楠. 飞机飞行性能品质与控制[M]. 北京: 国防工业出版社, 2007: 37-39.CHEN T N. Aircraft flight performance quality and control[M]. Beijing: National Defense Industry Press, 2007: 37-39(in Chinese). [30] 刘昶. 现代战斗机飞行力学问题的研究进展[J]. 飞行力学, 1999, 17(1): 10-16. https://www.cnki.com.cn/Article/CJFDTOTAL-FHLX901.001.htmLIU C. Development of some flight dynamics problems in modern fighter design[J]. Flight Dynamics, 1999, 17(1): 10-16(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-FHLX901.001.htm [31] 徐正军. 高超声速飞行器仿真与性能评估[D]. 西安: 西北工业大学, 2006: 42-43.XU Z J. Simulation and performance evaluation of hypersonic cruise vehicle[D]. Xi'an: Northwestern Polytechnical University, 2006: 42-43(in Chinese). [32] ZIPFEL P H. 航空航天飞行器动力学建模与仿真[M]. 3版. 高亚奎, 郭圣洪, 辛长范, 等, 译. 北京: 航空工业出版社, 2017: 60-61.ZIPFEL P H. Modeling and simulation of aerospace vehicle dynamics[M]. 3rd ed. GAO Y K, GUO S H, XIN C F, et al, translated. Beijing: Aviation Industry Press, 2017: 60-61(in Chinese).