1-D Laser-Ring Gyroscope

A 1-dimensional, laser gyroscope...on a pizza pan.

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A laser-ring gyroscope is a device most-often used in planes and space shuttles. It acts as a regular gyroscope should, with the exception of being made with a laser, and using the Sagnac Effect, which takes place when the item in question is in rotation. This effect - the laser changing its position - is then observed by an interferometer ( in short, a brightness/darkness detecting device), and then this information is picked up by a Multimeter or Oscilloscope, which display the change in distance (how far the laser moved, and therefore, the vehicle from its default position). The O-scope will present packs of sine waves that vary in density, representing the changes in dark-to-light and light-to-darkness.



- 1 aluminum mounting platform (the pizza pan!)

- 12 Chicago screws

- 2 FC/FC adapters

- 1 plastic loop form or wheel for mounting the fiber optic cable

- 1 100m single mode fiber optic cable with FC/UPC connectors

- 1 1.3 um analor IR laser ,fiber mountable, w/ ON/OFF switch

- 1 fiber mountable PIN diode deector / amplifier combo w/ zero control and 9V battery

- 1 multi-meter, 1MOhm input impedance

- 1 2x2 fiber optic coupler, single mode, w/ FC/UpC connectors

- 1 D Battery power supply

- 1 Phase controller (wheel) and mount

- 10 sets mounting clips and 6-32 screws

- (optional) rubber feet

(Special thanks to Skyhunt for easy assembly.)


The Sagnac Effect & the Journey of the Laser Light

(Go to Wikipedia for more information on the Sagnac Effect!)


The Sagnac Effect occurs when a laser light is split, and both beams are made to go the same path, but in different directions, in order to make the "ring". On return, however, both beams exit through the same door, but their collision causes interference - if both exit via a slit on a piece of paper, for instance, one would see overlapping hills and troughs of light, bright and dark bands rippling from the exit.

The Fun Part: So, when the platform that these lights are mounted upon rotates, the two beams shift, causing variations in the interference patterns. To measure the change from their initial position to their final position from each other, is to measure how far the vehicle with the gyroscope moved from their own default position. If a fighter-jet were to tip its nose downward by say, 5 degrees, the incredibly-sensitive gyroscope's lasers would shift, and the reading would come back to the pilot exactly (or almost exactly) how far they'd moved.


So, our laser light is beamed through the fiber-optic cable via the 1300nm IR laser, 1mW output - a cable composed on the inside of mirrors. The length and number of loops is directly responsible for the sensitivity of the gyroscope! The two wheels that control the phase of the light signal are simply smaller, additional loops that, when moved in a certain direction, help to stabilize the default position of that light (assumed 0) .

From there, the light is boosted by the PIN photo-diode amplifier, and likewise the "exit", where the acting interferometer (Multimeter or O-scope) picks it up and displays it.


Edit: Unfortunately, I'm out of time to put up a working video of the LRG's appearance at the Design Symposium, Spring 2014, but will definitely try for more pictures.


20140820 Wednesday: Equations

[From the Gyro Report]

Theory of Operation

The Sagnac interferometer/FOG works by having a light beam from a laser split into two light beams that travel in opposite directions, and are joined back together by a coupler. The difference in angular velocity between the two light beams causes different phase angles that are detected by the photo-diode. The photo-diode outputs a voltage dependent on the phase difference between the two light beams.

Δt = 4ΩA/c
2 , Δ fringe = 4ΩA/c
λ Sensitivity equation (for gyroscope)
Fiber-optic cable = 100m, radius (r) =0.16m, 100 turns ≈ 1 m circumference
1. Angular velocity (Ω) v/r = 6.25
2. Area (A) = 0.08m^2 * 100 = 8.04m^2
3. C = 3 * 10^8 m/s
4. Λ 1.3 * 10^6m^2
Δ fringe = 0.515, 360/(0.515 * 2) = 349.5°/s out of phase to in phase in rotation
Maximum voltage ≈ 850mV
Sensitivity = 349.5/850 = 0.41°/s/mV or .4°/s for 1mV on a meter.

  • About That Video...

    Sky Carter08/21/2014 at 00:45 0 comments

    20140820 Wednesday

    About that Video...

    I'm really camera-shy. T__T Plus, I have no video-editing software on the school's computer to record myself. But this probably does not matter, since my home won't have an established internet connection until tomorrow anyway. (Yeesh.)

    But if you'd like to know more about me, or have any questions, please check here, or visit my facebook page!

    Because my family and friends enjoy their privacy, I cannot fully open my profile to the public. Please send me a friend request first, state who you are, and message me at will. I'll try to reply on time, between classes. :)


    --Sky C.

  • Additional Images

    Sky Carter08/21/2014 at 00:22 0 comments

    Figure 2 (Skyhunt): The Completed Ring-Laser Gyro. ^

    Figure 3 (Skyhunt): The Oscilloscope Results. ^

    Block Diagram (Skyhunt)

    Laser Circuit (Skyhunt)

    This circuit uses a current limiting resistor to lower the voltage more
    suitable for the diode. The diode outputs ≈ 1mW @ 1300nm.

    PIN Diode Circuit (Skyhunt)

    This circuit uses a gain of 11 and a manual null adjust to zero out the output. This circuit is known as a "common mode rejection amplifier", which is used to reduce noise on the output. The Ouput could be displayed by either a Multimeter or an Oscilloscope.

  • Troubleshooting

    Sky Carter08/21/2014 at 00:08 0 comments

    Testing & Troubleshooting

    Upon completing the assembly of the ring-laser gyroscope, the gyro’s voltmeter would not properly read the changes in voltage. Each step of assembly was revisited to isolate the problem. Phase-controller and Photodiode found to be improperly set, and adjusted accordingly to the requirements provided by the manual. Problem isolated to the voltmeter, which was revealed to have low batteries. The voltmeter was exchanged for another, and the problem resolved.

                                                           Figure 2 (Skyhunt)
    The gyro was then connected to an oscilloscope to display the bright and dark bands of incoming interference patterns in the light. Output waveforms were “snakes”. Determined that higher frequencies = brighter light bands, and lower frequencies = darker bands. Gyro was extremely sensitive to the slightest change / interference, and reacted seismically to the lightest vibration around it, making an accurate reading for rotation without some system or program of filtering noise next to impossible. This resulted in the gyroscope being unable to properly calibrate.

                                                             Figure 3 (Skyhunt)
    Switched to DC couple on the oscope and adjusted the Phase-controller up and down, to bring in a brighter or darker interference pattern to the signal. Raised the amplitude of the signal with PIN diode, and adjusted the phase-controller until the lowest (darkest) signal possible was achieved. Counted bright and dark bands: the more bands per second indicated an increase or decrease in speed of rotation. Dark-to-light and light-to-dark was indicative of the direction.

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Adam Fabio wrote 02/27/2015 at 03:47 point

You know - I can't believe this project has been up all this time with no comments! You're doing awesome work, Sky - and great documentation to boot!  I really like reading these projects where devices which sound incredibly complex (and in many ways ARE complex) are broken down and built with household items - like pizza pans!

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