The invention belongs to the technical field of robot sensing and measurement and discloses a fiber bragg grating monitoring device and method for flapping deformation of a flapping-wing robot in flight. A first flapping wing and a second flapping wing are respectively assembled on the left and right sides of a trunk part; a first array polymer fiber bragg grating, a second array polymer fiber bragg grating, a third array polymer fiber bragg grating and a fourth array polymer fiber bragg grating are respectively implanted in the first flapping wing and the second flapping wing; an optical fiber connector is arranged at an upper part of the trunk part and is connected with a multi-core quartz optical fiber; the other end of the multi-core silica fiber is connected with one end of a fiber grating wavelength demodulator; and the fiber grating wavelength demodulator is used for demodulating and outputting a transmitted grating signal. According to the device, a polymer fiber grating implantation mode is adopted, and high-precision and spatial-constraint-free real-time measurement of flapping deformation can be realized.
本发明属于机器人传感与测量技术领域,公开了一种扑翼机器人飞行中扑动变形的光纤光栅监测装置、方法,设置有:躯干部分;躯干部分左右两侧分别装配有第一扑翼与第二扑翼;第一扑翼、第二扑翼内分别植入有第一阵列聚合物光纤光栅、第二阵列聚合物光纤光栅以及第三阵列聚合物光纤光栅、第四阵列聚合物光纤光栅;躯干部分上部设置有光纤连接器,光纤连接器与多芯石英光纤相连接;多芯石英光纤的另一端与光纤光栅波长解调器的一端连接;所述光纤光栅波长解调器用于对传输的光栅信号进行解调输出。本发明采用聚合物光纤光栅植入的方式,可以对扑动变形的高精度、无空间约束的实时测量。
Fiber bragg grating monitoring device and method for flapping deformation of flapping-wing robot in flight
一种扑翼机器人飞行中扑动变形的光纤光栅监测装置、方法
2021-12-21
Patent
Electronic Resource
Chinese
IPC: | G01B MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS , Messen der Länge, der Dicke oder ähnlicher linearer Abmessungen / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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