[1]
Jia Pei-ran, Use Special Trajectory Error Coefficient of Guidance Tool and Deduce Guidance Tool Error of Normal Trajectory [J]. Journal of National University of Defense Technology, 1985, (02): 59-66.
Google Scholar
[2]
Zhang Zui-liang, A Notation on the Analysis of the Error in Inertial Guidance Tools [J]. Journal of National University of Defense Technology, 1981, (04):83~88.
Google Scholar
[3]
Sha Yu, Wu Yi, Wang Zheng-ming, Development and Improvement of Principal Components Estimation and Its Application in the Separation of Guidance Instrumental Tool Errors[J]. Aerospace Control, 1991, (S1): 136-146.
Google Scholar
[4]
Luo Jian-shu, Wu Yi, The Method for Appraising Accuracy of Estimated Values of Regression Coefficients by Hypothesis Test[J]. Missile and Space Vehicles, 1994, (01): 23-29.
Google Scholar
[5]
Wang Zheng-ming, Yi Dong-yun, The Calibration and Evaluation of Trajectory Tracking Data. Changsha: Publishing House of National University of Defence Technology, 1999, pp.328-384.
Google Scholar
[6]
Cheng Guang-xian, Selection of Data Reasonableness Check and Error Separation Methods[J]. Aerospace Control, 1991, (S1): 104-111.
Google Scholar
[7]
Xu Ai-ping, An Instrumental Error Analysis Method for Strap-down Guidance System[J]. Aerospace Control, 1992, (02): 34-39.
Google Scholar
[8]
Zhao Min, Conversion Method of Guidance Instrumental Error[J]. Missile and Space Vehicles, 1993, (01): 42-48.
Google Scholar
[9]
Yao Jing, Duan Xiao-jun, Zhou Hai-yin, Modeling and Parameters Estimation of Marine Guidance Instrumental Systematic Error[J]. Journal of Ballistics, 2005,(01): :33-39.
Google Scholar
[10]
Zhang Xian-da, Matrix Analysis and Applications[D], Springer, 2004: 54-56.
Google Scholar