[1] 刘玉标,刘维玮,程载斌,等. 通过缩比试验数据计算潜射导弹的载荷[J]. 兵工学报, 2012. 33(8): 916-920. LIU Yu-biao, LIU Wei-wei, CHENG Zai-bin, et al. Load calculation for submarine launched missile based on scaled model test [J]. Acta Armamentarii, 2012. 33(8): 916-920.(in Chinese) [2] 尹云玉. 固体火箭横向响应载荷识别方法[J].宇航学报, 2009, 30(6): 2135-2139. YIN Yun-yu. The identification method of transverse responding load for solid rocket [J]. Journal of Astronautics, 2009, 30(6):2135-2139.(in Chinese) [3] 尹云玉. 固体火箭自由运行状态截面弯矩识别方法[J]. 宇航学报, 2010, 31(7): 1706-1710. YIN Yun-yu. An identification method for transverse response moment of solid rocket during free flight state[J]. Journal of Astronautics, 2010, 31(7):1706-1710.(in Chinese) [4] 彭超, 史玉杰, 陈竹. 某飞机部件高速风洞测力天平研制[J]. 实验流体力学, 2009, 23(4):98-101. PENG Chao, SHI Yu-jie, CHEN Zhu. Forcing balance development of a certain airplane components in high speed wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2009, 23(4):98-101.(in Chinese) [5] 胡凯征, 刘献伟, 黄帅军, 等. 导弹挂飞应力天平测力系统设计[J]. 科学技术与工程, 2008, 8(20):5716-5719. HU Kai-zheng, LIU Xian-wei, HUANG Shuai-jun, et al. Design and development of system for the measurement of missile's embarkation flight loads based on strain-gauge balance[J]. Science Technology and Engineering, 2008,8(20):5716-5719.(in Chinese) [6] 杨双龙. 风洞应变天平动态特性与动态校正方法研究[D]. 合肥:合肥工业大学, 2014. YANG Shuang-long. Studies on dynamic characteristics and dynamic correction methods for wind tunnel strain gauge balance[D]. Hefei: Hefei University of Technology, 2014. (in Chinese) [7] 解亚君, 宋笔锋, 郭琦, 等. 杆式应变天平的优化设计[J]. 传感器技术, 2002, 21(12):18-20. XIE Ya-jun, SONG Bi-feng, GUO Qi, et al. Optimizing design of beam strain-gauge balance[J]. Journal of Transducer Technology, 2002, 21(12):18-20.(in Chinese) [8] 汤吉晨. 飞机尾翼载荷飞行测量研究[J].航空学报, 1989, 10(10):B474-B478. TANG Ji-chen. Investigation on the determination of airplane tail loads by flight tests[J]. Acta Aeronautica et Astronautica Sinica, 1989, 10(10):B474-B478.(in Chinese) [9] 胡昌荣. 飞机飞行载荷测量载荷方程的优选[J]. 航空学报, 1994,15(1):102-105. HU Chang-rong. The optimization of load equation during aircraft flight load measurement[J]. Acta Aeronautica et Astronautica Sinica, 1994, 15(1):102-105.(in Chinese) [10] 尚琳, 何发东, 杨华保, 等. 基于神经网络的垂尾飞行载荷模型研究[J]. 强度与环境, 2011, 38(5):49-53. SHANG Lin, HE Fa-dong, YANG Hua-bao, et al. Research on flight loads model of vertical tail based on neural networks[J]. Structure & Environment Engineering, 2011, 38(5):49-53.(in Chinese) [11] Allen M J, Dibley R P. Modeling aircraft wing loads from flight data using neural networks[R]. Edwards, CA:SAE, 2003. [12] 方保镕, 周继东, 李医民. 矩阵论[M]. 北京:清华大学出版社, 2009. FANG Bao-rong, ZHOU Ji-dong, LI Yi-min. Matrix theory[M]. Beijing:Tsinghua University Press, 2009.(in Chinese) |