D-optimal six position testing method for dynamically tuned gyro

[1] 王惠文,孟洁.多元线性回归的预测建模方法[J].北京航空航天大学学报,2007,33(4):500-504 Wang Huiwen, Meng Jie. Predictive modeling on multivariate linear regression [J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(4): 500-504 ( in Chinese) [2] 何麟书,刘刚.一种求解函数全局优化问题的正交方向法[J].北京航空航天大学学报,2005,31(4):425-429 He Linshu, Liu Gang. Orthogonal direction algorithm for global function optimization[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(4): 425-429 ( in Chinese) [3] 许国祯.惯性技术手册[M].北京:中国宇航出版社,1995:12-14 Xu Guozhen. Inertial technology handbook[M]. Beijing: China Astronautics Publishing House, 1995: 12-14 (in Chinese) [4] 徐利治.现代数学手册[M].武汉:华中科技大学出版社,2000:140-142 Xu Lizhi. Modern mathematics handbook[M]. Wuhan: Huazhong University of Science and Technology Press, 2000: 140-142 ( in Chinese) [5] 方开泰,马长兴,李久坤.正交设计的最新发展和应用-正交设计的D最优性[J].数理统计与管理,1999,18(4):43-52 Fang Kaitai, Ma Changxing, Li Jiukun. Recent develop of orthogonal factorial designs and their applications D-optimality of orthogonal designs[J]. Application of Statistics and Management, 1999, 18(4): 43-52 ( in Chinese). [6] ANSI/IEEE Std 813-1988, IEEE specification format guide and Test procedure for two-degree-of freedom dynamically tuned gyros[S]