A Passive Laser Gyroscope Based on Phase Sensitive Heterodyne Measurement
A laser gyroscope and passive technology, applied in the field of laser gyroscopes, can solve problems such as backscattering noise, frequency drift in the free spectrum region, etc., to improve the resolution of rotation detection, solve the frequency drift in the free spectrum region, and improve the detection resolution Effect
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no. 1 example
[0023] The invention provides a passive laser gyroscope based on phase-sensitive heterodyne measurement, figure 1 It is an overall structure diagram of the present invention, mainly consisting of a Sagnac interferometer 100, a balance detection device 200 and a signal extraction device 300; Ring cavity and three injection laser beams 1021, 1022, 1023; the four high reflectivity cavity mirrors 1011, 1012, 1013, 1014 include three input cavity mirrors 1011, 1012, 1013 and one output cavity mirror 1014; the three beam injection Lasers 1021, 1022, and 1023 are respectively injected into the optical ring cavity from three input cavity mirrors 1011, 1012, and 1013, wherein two beams of laser light 1021 and 1022 are injected clockwise along the ring cavity, and one beam of laser light 1023 is injected counterclockwise; The angular frequencies of the three laser beams are ω 1 , ω 2 and ω 3The balance detection device 200 includes a Mach-Zehnder interferometer 201 and a balance dete...
no. 2 example
[0033] like image 3 and Figure 4 As shown, the present embodiment provides a passive laser gyroscope based on phase-sensitive heterodyne measurement, image 3 It is an overall structure diagram of the present invention, mainly consisting of a Sagnac interferometer 100, a balance detection device 200 and a signal extraction device 300; Ring cavity and three injection laser beams 1021, 1022, 1023; the four high reflectivity cavity mirrors 1011, 1012, 1013, 1014 include three input cavity mirrors 1011, 1012, 1013 and one output cavity mirror 1014; the three beam injection Lasers 1021, 1022, 1023 are respectively injected into the optical ring cavity from three input cavity mirrors 1011, 1012, 1013, wherein two beams of laser light 1021 and 1022 are injected counterclockwise along the ring cavity, and one beam of laser light 1023 is injected clockwise; The angular frequencies of the three laser beams are ω 1 , ω 2 and ω 3 ; The balance detection device 200 includes a Mach-Z...
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