precision navigation sensors based on atom interferometry
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Precision Navigation Sensors based on Atom Interferometry Mark Kasevich Depts. of Physics and Applied Physics Stanford University Youngs double slit interferometer with atoms Mlynek, PRL, 1991 Youngs double slit interference fringes


  1. Precision Navigation Sensors based on Atom Interferometry Mark Kasevich Depts. of Physics and Applied Physics Stanford University

  2. Young’s double slit interferometer with atoms Mlynek, PRL, 1991

  3. Young’s double slit interference fringes Mlynek, PRL, 1991

  4. 1991 Light-Pulse Atom Interferometer

  5. Light-pulse atom interferometry Pulses of light are used to coherently manipulate atom de Broglie waves: Kasevich and Chu, PRL, 1991

  6. Images of atoms in interferometer Chiow, PRL, 2011

  7. 1.4 cm wavepacket separation (!) Interference Control Interference contrast observed for 1.4 cm wavepacket separation. Est. δ g < 1e-11 g/shot accelerometer sensitivity. 10 m atomic fountain apparatus

  8. Simple model for acceleration sensitivity As atom climbs gravitational potential, velocity decreases and de Broglie wavelength increases …. g Phase shift determines probability of detecting atom in a given output port.

  9. Simple model for rotation sensitivity Sagnac effect for de Broglie waves ….

  10. Gyroscope (1997) 10 Gustavson, PRL, 1997

  11. Gyroscope interference fringes Noise: 3 µ deg/hr 1/2 Bias stability: < 60 µ deg/hr Scale factor: < 5 ppm Gustavson, PRL, 1997 11 Durfee, PRL, 2006

  12. Light-pulse AI Gyroscope Performance AI Source: Proc. IEEE/Workshop on Autonomous Underwater Vehicles

  13. Light-pulse AI Accelerometer Performance AI

  14. Why superb sensors? Accelerometer • Atom = near perfect inertial Sensor reference. Case Laser • Laser/atom interactions register Atoms relative motion between atom and sensor case. • Sensor accuracy derives from Gyroscope the exceptional stability of Sensor Case optical wavefronts. v • Direct read-out of angular and Atoms linear displacements.

  15. Hybrid sensor/Gyroscope mode Measured gyroscope output vs.orientation: Typical interference fringe record: • Inferred ARW: < 100 µ deg/hr 1/2 • 10 deg/s max input • <100 ppm absolute accuracy Stockton, PRL, 2011

  16. Hybrid sensor operation F=4 F=3 Interior view Interior view of Interference fringes are sensor recorded by measuring number of atoms in each quantum state. Fringes are scanned electro- optically.

  17. Hybrid sensor/Gravity gradient mode

  18. Hybrid sensor/Absolute accelerometer Horizontal input axis, microGal resolution.

  19. Gravimeter, Measurement of g Fabricated and tested at AOSense, Inc., Sunnyvale, CA. Sensors designed for precision navigation. AOSense, Inc. DARPA DSO 19

  20. Gyroscope/Rotational Seismology CMG3 Honduras/offshore 7.3 +30 min ANGLE VELOCITY Gyroscope output necessary to disambiguate tilt from horizontal motion (navigation problem). AOSense, Inc. DARPA DSO 20

  21. The challenge… ? how 408-735-9500 AOSense.com 21 Sunnyvale, CA

  22. Compact Zeeman slower 408-735-9500 AOSense.com 22 Sunnyvale, CA

  23. AOSense Commercial Compact Gravimeter Commercial Cold Atom Gravimeter • Noise < 1 µ g/Hz 1/2 • Shipped 11/22/10 • First commercial atom optics sensor 408-735-9500 AOSense.com 23 Sunnyvale, CA

  24. (Optical) Atomic Clock 6 L physics package. Includes all sub-systems except electronics. Sr oven, 3 W Sr clock laser Zeeman slower 408-735-9500 AOSense.com Sunnyvale, CA 24

  25. System implementation Space/time vector tracking with integrated atom inertial and clock (courtesy J. Spilker) 408-735-9500 AOSense.com 25 Sunnyvale, CA

  26. Technology Vision • Inertial+ grade IMU • Navigation grade IMU < 10 liters < 0.1 liters < 10 m/hr drift < 1 Watt < 100 Watts Low-cost ($1K ?) Gravity compensated 408-735-9500 AOSense.com 26 Sunnyvale, CA

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