[1] Owens D B, Brandon J M, Croom M A, et al. Overview of dynamic test techniques for flight dynamics research at NASA LaRC// Proceedings of 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2006.
[2] Morelli E A. Real-time dynamic modeling-data information requirements and flight test results//Proceedings of AIAA Atmospheric Flight Mechanics Conference. Honolulu, 2008.
[3] Wolowicz C H., Jr Bowman J S, Gilbert W P. Similitude requirements and scaling relationships as applied to model testing. NASA, 1979.
[4] 恽起麟. 风洞试验. 北京: 国防工业出版社, 2000.
[5] 中国人民解放军总装备部军事训练教材编辑工作委员. 模型自由飞试验. 北京: 国防工业出版社, 2002.
[6] Regan C. In-flight stability analysis of the X-48B aircraft. AIAA-2008-6571, 2008.
[7] Morelli E A. Determining the accuracy of maximum likelihood parameter estimates with colored residuals//NASA CR 194893. Virginia, 1994.
[8] Jordan T L, Langford W M, Hill J S. Airborne subscale transport aircraft research testbed, aircraft model development//AIAA 2005-6432, AIAA Guidance, Navigation, and Control Conference. Washington: AIAA, 2005.