The invention provides an 
airplane rising, landing and taxiing performance comprehensive 
verification platform integrating 
airplane inertia simulation, lateral wind load 
simulation, taxiing speed 
simulation, 
runway state simulation and 
brake control and very high in universality, and by means of the 
airplane rising, landing and taxiing performance comprehensive 
verification platform, all-factor simulation and testing evaluation in the airplane rising, landing and taxiing processes can be achieved. The airplane rising, landing and taxiing performance comprehensive 
verification platform comprises an aircraft 
simulation system, an undercarriage airplane 
system, a 
braking system, a lateral 
wind simulation loading 
system, a 
runway simulation system, a measurement and control and 
simulation system and the like. By means of the airplane rising, landing and taxiing performance comprehensive verification platform, the taxiing speed, the course heading, the loading force and the braking torque can be measured, and visual simulation and braking control strategy researches can be conducted as well. The airplane rising, landing and taxiing performance comprehensive verification platform can provide an early-period theory, simulation and experiment basis for active-service or researched 
aircraft landing gear system design, taxiing control rate design and whole airplane 
inertia optimal allocation. The problem that at present, the control strategy can only be researched at the test flight taxiing stage is solved, and thus the cost and risks of out-field taxiing tests are greatly lowered.