The invention discloses a testing method and a testing
system for aircraft parameter display results. The testing method comprises the steps that at the step S1, a
test case is compiled or loaded; at the step S2, the
test case at the step S1 is executed, and a source of data in the
test case is formed; at the step S3, data corresponding to the test case is grasped from an airborne
bus, and the data is compared with the source of the data in the test case; at the step S4, display data of a display picture of an avionic
system is recognized, and a recognition result is compared with the source of the data in the test case; and at the step S5, the source of the data in the test case, analytical data of the airborne
bus, and a
list of the display
picture recognition data are output. The testing
system comprises a testing computer, an airborne display, a display control computer, the airborne
bus, an airborne inertial navigation computer, an inertial navigation
exciter, a reflective internal storage net, an atmospheric engine
exciter and an airborne atmospheric computer. The testing method and the testing system disclosed by the invention have the advantages that testing efficiency of parameter display results of an avionic system is increased; and workloads of testing workers are reduced.