Device for a Helicopter Modeling and Tuning using Flight Test Result for Handling Quality Simulator and Controlling Method for the Same

摘要

The present invention provides an apparatus for HQS modeling and tuning using flight test data and a control method thereof. The control method comprises: a first step of allowing a base analysis module to perform a wind tunnel test and CFD analysis for a helicopter according to helicopter modeling elements; a second step of allowing a simulation plan setting module to set a baseline model of the helicopter based on the result value analyzed by the base analysis module and set a flight test plan based on the set baseline model, after the first step; a third step of allowing a simulation module to perform a flight test by multibody dynamics techniques set by the simulation plan setting module, and organize and output the test results, after the second step; a fourth step of allowing a tuning module to tune the baseline model of the helicopter based on the result of the flight simulation performed by the simulation module after the third step; and a fifth step of allowing an evaluation module to evaluate the tuned model with a pilot on board and complete a final helicopter model by the multibody dynamics techniques based on the evaluation results after the fourth step. The present invention as described above can build a helicopter simulation model after performing HQS modeling and tuning using some flight test data to easily construct a static model of the aircraft over all sectors through the built trend, thereby maximizing ease of helicopter development.