1. KLEIN V, BATTERSON J G, MURPHY P C. Determination of airplane model structure from flight data by using modified stepwise regression [R]. NASA Technical, 1981.
2. TOBAK M, SCHIFF L B. A nonlinear aerodynamic moment formulation and its implications for dynamic stability testing [R]. AIAA, 1971.
3. CAI Jing-shi, WANG Qing, WANG Wen-zheng. System identification of aircraft [M]. Beijing: National Defense Industry Press, 2002: 26–62. (in Chinese)
4. LINSE D J, STRENGEL R F. Identification of aerodynamic coefficients using computational neural networks [J]. Journal of Guidance, Control and Dynamics, 1993, 16(6): 1018–1025.
5. KUMAR R, GANGULI R, OMKAR S N, KUMAR M V. Rotorcraft parameter estimation from real time flight data using radial basis function networks [J]. Journal of Aircraft, 2008, 45(1): 333–341.