A computational and test method for calibrating the flight loads carried by aircraft wings is *** wing load is measured in real-time based on the resistance and fiber Bragg grating strain *** linearstepwise regressio...
详细信息
A computational and test method for calibrating the flight loads carried by aircraft wings is *** wing load is measured in real-time based on the resistance and fiber Bragg grating strain *** linear stepwise regression method is used to construct the load *** mean impact value algorithm is employed to select suitable *** the ground calibration experiment,the wing load calculation equations in both forward and reverse installation states are *** correctness of the load equations was verified through equation error and inspection error ***,the actual flight load of the wing was obtained through flight tests.
暂无评论