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This paper clarified the contribution of front wing and rear wing to the longitudinal aerodynamic derivative by analyzing the characteristics of tandem wing aircraft. By combining the structure and aerodynamic simulation data of the aircraft, the aerodynamic derivative can be directly solved through simplification of force without introducing the tail capacity V H , and the longitudinal short-period (control) transfer function of the tandem wing aircraft can be obtained by substituting thedoi:10.1088/1757-899x/563/3/032022 fatcat:ugse2lngh5epzp3djha62hkqhi