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.