[1] 梁彦, 张驰, 梁明. 带翼展飞行器质量质心测量系统的设计实现及其误差分析[J]. 战术导弹技术, 2012(3): 29-35. LIANG Y, ZHANG C, LIANG M. Design realization and error analysis of mass measurement and centroid localization system for missiles[J]. Tactical Missile Technology, 2012(3): 29-35(in Chinese). [2] 罗明强, 魏城龙, 刘虎, 等. 基于三维参数化模型构建的飞机重量重心快速估算方法[J]. 航空学报, 2013, 34(3): 566-573. LUO M Q, WEI C L, LIU H, et al. Rapidestimation method for aircraft weight and center of gravity based on 3-D parametric modeling[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(3): 566-573(in Chinese). [3] 王少云, 费泽寅. CX1型无人机称重仪[J]. 航空学报, 2005, 26(1): 70-73. WANG S Y, FEI Z Y. Theweighing instrument for CX1 unmanned air vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2005, 26(1): 70-73(in Chinese). [4] 金雪. 基于质量质心测量的称重仪数据采集及处理系统研制[D]. 哈尔滨: 哈尔滨工业大学, 2010. JIN X. The weighing instrument's dataacquisitionand processing system develop based on the qualityand centroid measurement[D]. Harbin: Harbin Institute of Technology, 2010(in Chinese). [5] 顾强, 李波. 弹体质量、质心及质偏的新三点测量法[J]. 弹箭与制导学报, 2005, 25(S9): 177-178, 201. GU Q, LI B. Newthree points measurement of column structure’s mass centroid and centroidal deviation[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2005, 25(Sup 9): 177-178, 201(in Chinese). [6] 刘明勇, 罗锋, 徐健. 质量质心测量方法及实例分析[J]. 制造技术与机床, 2019(4): 138-141. LIU M Y, LUO F, XU J. Method ofmasscentroid measurement and case analysis[J]. Manufacturing Technology & Machine Tool, 2019(4): 138-141(in Chinese). [7] 张鹰华, 樊新华, 张雷雨, 等. 基于四点支撑法的导弹质量质心测量系统设计及误差分析[J]. 机械设计与研究, 2016, 32(3): 96-99. ZHANG Y H, FAN X H, ZHANG L Y, et al. Thedesignand error analysis of A new mass and centroid measurement system for missiles based on four-point support approach[J]. Machine Design & Research, 2016, 32(3): 96-99(in Chinese). [8] 李跃振. 大型带翼展飞行器质量与质心测量仪设计与开发[D].廊坊: 华北航天工业学院,2019. LI Y Z. Design anddevelopment of mass and centroid measuring instrument for large missile[D].Langfang: North China Institute of Aerospace Engineering, 2019(in Chinese). [9] 王学仓. 导弹质量特性参数测量系统设计及分析[D]. 哈尔滨: 哈尔滨工业大学, 2014. WANG X C. Mass property parameters measurement systemof missile design and analysis[D]. Harbin: Harbin Institute of Technology, 2014(in Chinese). [10] 傅德彬, 王飞, 王新星, 等. 低冲击弹射式发射箱前盖分离特性[J]. 宇航学报, 2016, 37(4): 488-493. FU D B, WANG F, WANG X X, et al. Separation characteristics for front cover of ejection launch canister with low impact[J]. Journal of Astronautics, 2016, 37(4): 488-493(in Chinese). [11] 赵威, 王伟. 非线性偏最小二乘回归法在均匀设计响应面法中的应用[J]. 航空学报, 2012, 33(5): 839-847. ZHAO W, WANG W. Application ofnon-linear partial least squares regression method to response surface method with uniform design[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(5): 839-847(in Chinese). [12] PEI J, WANG W J, YUAN S Q, et al. Optimization on the impeller of a low-specific-speed centrifugal pump for hydraulic performance improvement[J]. Chinese Journal of Mechanical Engineering, 2016, 29(5): 992-1002. [13] ZHU H G, LIU L, LONG T, et al. Global optimization method using SLE and adaptive RBF based on fuzzy clustering[J]. Chinese Journal of Mechanical Engineering, 2012, 25(4): 768-775. [14] 郑昱, 孟凡伟, 杨占立, 等. 基于试验设计方法和响应面方法的九索并联机构优化设计[J]. 机械工程学报, 2017, 53(17): 92-102. ZHENG Y, MENG F W, YANG Z L, et al. Optimizationdesign of a parallel mechanism driven by nine cables based on experimental design methods and response surface methods[J]. Journal of Mechanical Engineering, 2017, 53(17): 92-102(in Chinese). [15] 彭珍瑞, 曹明明, 刘满东. 基于加速度频响函数小波分解的模型修正方法[J]. 航空学报, 2020, 41(7): 223548. PENG Z R, CAO M M, LIU M D. Model updating method based on wavelet decomposition of acceleration frequency response function[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(7): 223548(in Chinese). [16] 胡春晓, 余光其. 舰炮武器系统动态精度海上测试方法与精度条件分析[J]. 指挥控制与仿真, 2020, 42(2): 84-88. HU C X, YU G Q. Testmethod and analysis on accuracy conditions at sea for dynamic accuracy of naval Gun weapon system[J]. Command Control & Simulation, 2020, 42(2): 84-88(in Chinese). [17] 李琳, 夏学知, 熊紫倩, 等. 面向战役级目标态势生成的航迹关联算法[J]. 华中科技大学学报(自然科学版), 2020, 48(9): 31-37. LI L, XIA X Z, XIONG Z Q, et al. Targetassociation algorithm for operational level target situation generation[J]. Journal of Huazhong University of Science and Technology(Natural Science Edition), 2020, 48(9): 31-37(in Chinese). [18] 洪林雄, 李华聪, 彭凯, 等. 基于高效搜索方法的可靠性分析改进响应面法[J]. 北京航空航天大学学报, 2020, 46(1): 95-102. HONG L X, LI H C, PENG K,et al. Improved response surface method of reliability analysis based on efficient search method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(1): 95-102(in Chinese). [19] ZHANG F, CHENG L, WU M Y, et al. Performance analysis of two-stage thermoelectric generator model based on Latin hypercube sampling[J]. Energy Conversion and Management, 2020, 221: 113159. [20] 张岳琴. 基于单摄像机的弹体位姿测量系统设计[D]. 南京: 南京理工大学, 2014. ZHANG Y Q.Design of missile pose measurement system based on single camera[D]. Nanjing: Nanjing University of Science and Technology, 2014(in Chinese). |