Surface aircraft stability whole-machine power model basin test method

Disclosed is a surface aircraft stability whole-machine power model basin test method. The surface aircraft stability whole-machine power model basin test method comprises the test steps of a, installation of a whole-machine power model and a test device; b, installation of a data collecting device. Specifically, the method comprises observing and recording the motion state and the motion process of the whole-machine power model (1) under disturbance; during the test, recording the state of the whole-machine power model (1) as well parameters such as the angle of deflection of flaps, the angle of deflection of an elevator, test weight and center of gravity and test speed. After finishing the test, data analyzing personnel should perform comprehensive analysis on the collected data according to the collected data and test phenomena as well as validity evaluation on test data. The surface aircraft stability whole-machine power model basin test method has the advantages of being practical, feasible, simple in operation and reliable in test results.