[2] ukasz S′wich. Calibration of a load measurement system for an unmanned aircraft composite wing based on fibre Bragg gratings and electrical strain gauges[J]. Aerospace, 2020, 7(3): 7030027.
[3] Raffaella D S. Fiber optic sensors for structural health monitoring of aircraft composite structures: Recent advances and applications[J]. Sensors, 2015, 15(8): 18666-18713.
[4] Daichi W, Hirotaka I, Masato T, et al. Flight demonstration of aircraft fuselage and bulkhead monitoring using optical fiber distributed sensing system[J]. Smart Materials and Structures, 2018, 27(2): 055007.
[5] Iele M, Leone M, Consales G V, et al. Load monitoring of aircraft landing gears using fiber optic sensors[J]. Sensors and Actuators A: Physical, 2018, 281: 31-41.
[6] Iadicicco A, Natale D, Di P P, et al. Strain monitoring of a composite drag strut in aircraft landing gear by fiber Bragg grating sensors[J]. Sensors (Basel, Switzerland), 2019, 19(10): 31096575.