Tutorial Measuring at Picometer Accuracy Dennis Weise International Conference on Space Optics 6. Oct. 2010 Outline • Introduction • Interferometry Basics • Noise Sources in the Measurement Chain • Specific Challenges for Inter-S/C Metrology 6. Oct. 2010 International Conference on Space Optics 2010 Page 2 Outline • Introduction • Interferometry Basics • Noise Sources in the Measurement Chain • Specific Challenges for Inter-S/C Metrology 6. Oct. 2010 International Conference on Space Optics 2010 Page 3 Quantum Metrology in Space Space-Time Anisotropy Research © ESA LISA Pathfinder International Conference on Space Optics 2010 Search for Anomalous Gravitation using Atomic Sensors © TESAT Laser Communication Formation Flying Terrestrial Planet Finder Cosmic Vision SIM PlanetQuest Matter Wave eXplorer of Gravity Cosmic Vision © NASA Fundamental Physics NG2 Geodesy Large Structures International X-Ray Observatory © NASA Gravitational Waves 6. Oct. 2010 Laser Interferometer Space Antenna Page 4 A “Picometer” is really not very much… 6. Oct. 2010 International Conference on Space Optics 2010 Page 5 What does Picometer “Accuracy” Mean? • Terminology “Accuracy”: deviation of the measured value from the actual value “Precision”: deviation between the results of repeated measurements (“reproducibility”) Here, we look at detection of translation at picometer precision! 6. Oct. 2010 International Conference on Space Optics 2010 Page 6 Tutorial n o i s i Measuring at Picometer Accuracy c e Pr Dennis Weise International Conference on Space Optics 6. Oct. 2010 Timescales • The “precision” to report generally depends on the applicable measurement time “Measurement Band”: sampling time – vs. – uninterrupted duration of measurement 6. Oct. 2010 International Conference on Space Optics 2010 Page 8 Time Domain Analysis Allan Standard Deviation • IEEE and NIST recommend to use the Allan Variance for specification of stability in the time domain David W. Allan et al., 1966 Mostly used in the context of clocks to characterize frequency fluctuations fractional stability over integration time “two-sample variance” 6. Oct. 2010 International Conference on Space Optics 2010 Page 9 Frequency Domain Analysis (Root) Power Spectral Density • More common in the context of interferometry is an analysis in the frequency domain “Root Power Density Spectrum” The direct Fourier transform would yield an energy spectrum (Parseval’s Theorem) 6. Oct. 2010 International Conference on Space Optics 2010 Page 10 Fundamental Limits Translation of Macroscopic Objects • The lateral extension of the “measurement beam” averages to some extent over microscopic surface features • The applicability of the term “translation” for bulk objects is fundamentally limited by the presence of “thermal noise” Conversion of random (Brownian) motion into length fluctuations by mechanical loss According to the “fluctuation dissipation theorem” (Callen & Greene, 1952) (typ. magnitude at room temperature for Zerodur) L: A: Length of (cylindrical) spacer Cross Section of (cylindrical) spacer Material Mechanical Quality Q Mechanical Loss = 1/Q Young’s Modulus E [GPa] Zerodur 3.1 103 3.2 10-4 90.1 ULE 6.1 1.6 67.6 Fused Silica 6. Oct. 2010 104 106 International Conference on Space Optics 2010 10-5 10-6 71.7 Page 11 Outline • Introduction • Interferometry Basics • Noise Sources in the Measurement Chain • Specific Challenges for Inter-S/C Metrology 6. Oct. 2010 International Conference on Space Optics 2010 Page 12 Optical Metrology – Interferometry Gaussian Beams • Propagation of laser beams is generally described by decomposition into “HermiteGaussian Modes”. These fit particularly well with actual eigenmodes of Laser resonators with spherical mirrors Singlemode fibers Polarization 6. Oct. 2010 Spatial Power Distribution Propagation Phase International Conference on Space Optics 2010 Page 13 Optical Metrology – Interferometry Superposition • At the output of an interferometric beam splitter, a photodetector delivers a signal proportional to the light intensity of the superposed waves Finite bandwidth Energy conservation 6. Oct. 2010 International Conference on Space Optics 2010 Page 14 Optical Metrology – Interferometry Superposition • At the output of an interferometric beam splitter, a photodetector delivers a signal proportional to the light intensity of the superposed waves Finite bandwidth Energy conservation 6. Oct. 2010 International Conference on Space Optics 2010 Page 15 Optical Metrology – Interferometry Homodyne Interferometers • Homodyne interferometers utilize a single (narrow linewidth) laser frequency 6. Oct. 2010 International Conference on Space Optics 2010 Page 16 Optical Metrology – Interferometry Homodyne Interferometers • Homodyne interferometers utilize a single (narrow linewidth) laser frequency Various beam routing possibilities, depending on the application Multiple-Beam Interference Optical Resonator (Cavity) Fabry-Perot Michelson Mach-Zehnder Sagnac 6. Oct. 2010 International Conference on Space Optics 2010 Page 17 Optical Metrology – Interferometry Homodyne Interferometers • Homodyne interferometers detect translation by observing variations in the light intensity on the photodetector “Dark fringe” detection @ DC 6. Oct. 2010 International Conference on Space Optics 2010 Page 18 Optical Metrology – Interferometry Heterodyne Interferometers • Detection @ DC suffers from various environmental noise sources Typically @ acoustic frequencies: DC – approx. 100 kHz Heterodyne detection of the beat signal phase above this frequency band 6. Oct. 2010 International Conference on Space Optics 2010 Page 19 Optical Metrology – Interferometry Heterodyne Interferometers • The initial phase of the utilized laser beams – and therefore – is arbitrary and in general unstable Phase comparison between Measurement Interferometer and Reference Interferometer A successful comparison relies on pathlength stability in the Reference Interferometer! 6. Oct. 2010 International Conference on Space Optics 2010 Page 20 Optical Metrology – Interferometry Phase Measurement • The photodetection process converts photon flux into photo current Responsivity /Quantum Efficiency of photodiode substrate Heterodyne Efficiency / Contrast 6. Oct. 2010 International Conference on Space Optics 2010 Page 21 Optical Metrology – Interferometry Phase Measurement • The detection of the beat signal phase is typically performed by “mixing it down to DC” Both analog and digital processing is common The “Phasemeter” clock defines the timebase “Quadrature” detection removes the amplitude ambiguity 6. Oct. 2010 International Conference on Space Optics 2010 Page 22 Optical Metrology – Interferometry A typical Interferometric System 6. Oct. 2010 International Conference on Space Optics 2010 Page 23 Outline • Introduction • Interferometry Basics • Noise Sources in the Measurement Chain • Specific Challenges for Inter-S/C Metrology 6. Oct. 2010 International Conference on Space Optics 2010 Page 24 Noise Sources Laser Frequency Noise • If the individual optical pathlengths are not equal, variations of the laser frequency cause a variation of the measured phase Pathlength “matching” ‒ The laser phase noise of each laser shall reach all fiducial points of the measurement at the same time ‒ Symmetric setups Frequency-stable lasers 6. Oct. 2010 International Conference on Space Optics 2010 Page 25 Noise Sources Choice of Laser System • The choice of laser system is driven by requirement for maximum “free-running” frequency stability The choice laser wavelength is a secondary criterion, and strongly restricted by available laser sources e.g. Innolight Mephisto 6. Oct. 2010 International Conference on Space Optics 2010 Page 26 Noise Sources Choice of Laser System FBH/Astrium DBR Diode Laser Innolight NPRO Koheras DFB Fiber Laser TESAT LTP RLU In general it is necessary to improve the stability of the free-running laser by active frequency stabilization In particular for metrology between 2 or more satellites/spacecraft! 6. Oct. 2010 International Conference on Space Optics 2010 Page 27 Noise Sources Frequency Stabilization • Most common for “medium-term” stabilization of the laser frequency is Pound-Drever-Hall locking to an Optical Resonator (Cavity) R. V. Pound (1946) Best result achieved to date R. W. P. Drever, J. L. Hall (1983) • Alternatives include Hänsch-Couillaud stabilization (1980) ‒ Comparatively low complexity ‒ Relies on polarization dispersion in the cavity Unequal Armlength Interferometer (!) 6. Oct. 2010 J. Alnis et al., “Subhertz linewidth diode lasers by stabilization to vibrationally and thermally compensated ultralow-expansion glass Fabry-Pérot cavities”, Physical Review A 77, 2008. International Conference on Space Optics 2010 Page 28 Noise Sources Frequency Stabilization • For observation over very long timescales (days, weeks, months), stabilization to an absolute reference could be more suitable Systematic drifts of cavities due to temperature, material relaxation, etc. Our future time will be “optical” (I2, Sr, Hg, Al, …) Astrium GmbH Iodine Clock (2007) Iodine Standard ULE Cavity 6. Oct. 2010 International Conference on Space Optics 2010 Page 29 Noise Sources Frequency Combs • The frequency transfer between frequency references and the application wavelength can be accomplished by optical “Frequency Combs” Precise “rulers” at optical frequencies Available since 2000 (Hänsch, Hall, et al.) Mode-locked lasers with “carrier-envelope phase control” (fs pulse duration) Frequency Comb at HU Berlin (Prof. A. Peters) 6. Oct. 2010 International Conference on Space Optics 2010 Page 30 Noise Sources Differential Pathlength Noise • Only non-common-mode pathlength variations result in measurement noise Provide dimensional stability of the Interferometer Core Minimize impact of temperature fluctuations ‒ Low CTE spacer material Structural Material CTE [10-6/K] Titanium 8.8 SiC 100 2.2 Invar36 1.8 CFRP (isotropic) 0.2 ULE 0.03 Zerodur (Class 0) 0.02 ‒ Ultrastable optics integration ‒ Exploit symmetry for common-mode suppression ‒ Provide passive thermal shielding of the interferometer core “Energy Separator Cubes” 6. Oct. 2010 International Conference on Space Optics 2010 Page 31 Noise Sources Differential Pathlength Noise • Astrium is investigating the limits of CTE tuning of CFRP by Laser Dilatometry The ability to tune the CTE of CFRP – also to negative values – allows the development of larger structures with low “System CTE” (e.g. for telescopes) Partner: XPerion Friedrichshafen 6. Oct. 2010 International Conference on Space Optics 2010 Page 32 Noise Sources Differential Pathlength Noise • Quasi-static process control with sinusoidal excitation by radiative heat transfer Cycle times >> thermalization timescales Low pass transfer function for maximum suppression of environmental thermal noise ‒ Minimal conduction & convection Laser frequency noise can be monitored by comparison to a cavity-stabilized laser Sample Length: 11 cm Temperature Variation: 1 K 6. Oct. 2010 International Conference on Space Optics 2010 Expansion: 20 nm CTE: 1.8 x 10-7/K Page 33 Noise Sources Integration Technology • Hydroxide Catalysis Bonding Creation of siloxane chains between (polished) surfaces of materials containing silica ‒ Si, Zerodur, Fused Silica, ULE, granite, SiC, … ‒ Alkaline bonding solution (NaOH, KOH, Na2SiO3) Perfected by the University of Glasgow (H. Ward) ‒ Bond thickness approx. 20 – 100 nm ‒ Absolute beam placement accuracy < 10 µm Fully qualified for space application ‒ Utilized to integrate the OBI of LISA Pathfinder ‒ Baseline integration technology for LISA Optical Bench 6. Oct. 2010 International Conference on Space Optics 2010 Page 34 Noise Sources Integration Technology S. Ressel et al., Applied Optics 49(22), p. 4296 • Adhesive Bonding Developed by Astrium GmbH as alternative integration technology for Optical Systems ‒ Tunable curing times and less critical process offer potential simplifications for some applications ‒ Space-qualified epoxy (Hysol) ‒ Bond thickness approx. 1.4 µm Qualified with respect to environmental loads and dimensional stability ‒ Thermal cycling 8x cycling between -20°C and 50°C @ 2K/min ‒ Shock and vibration testing according to ECSS Sine vibration: max. 75g @ 61Hz Random vibration: 23.5g rms ‒ Within our measurement accuracy, hydroxide and adhesive bonded mirrors show identical pathlength and pointing stability 10 pm/Hz @ 10 mHz 10 nrad/Hz @ 10 mHz 6. Oct. 2010 International Conference on Space Optics 2010 Page 35 Noise Sources Measurement Chain • More general, noise in the “Measurement Chain” may be separated into the following main contributions Pathlength Noise: variations in the optical field “piston” on the detector Photodetection Noise: noise in the “Analog Chain” Phase Measurement Noise: noise in the “Phase Measurement” 6. Oct. 2010 International Conference on Space Optics 2010 Page 36 Noise Sources Photodetection Noise • Ghost Beams/Stray Light Causes pathlength measurement noise, if its phase on the detector varies ‒ Ghost beams often are as stable as the reference beams ‒ Stray light is often not mode-matched well (low heterodyne efficiency) “Balanced Detection” suppresses “in-phase” noise on a dual-ended receiver ‒ Detect at both output ports of the beam splitter ‒ Determine both amplitude and phase of the beat signals ‒ Normalize the beat vectors to equal length before correction Individual Phases 6. Oct. 2010 International Conference on Space Optics 2010 Balanced Detection Normalized Correction Page 37 Noise Sources Photodetection Noise • Ghost Beams/Stray Light – Example for normalized stray light correction “Optical Bench Development for LISA” ESA Contract No. 22331/09/NL/HB 6. Oct. 2010 International Conference on Space Optics 2010 Page 38 Noise Sources Photodetection Noise • Shot Noise The photon flux is subject to Poisson statistics “Additive noise” is directly mapped to phase variations for synchronous phase detection relative to the signal amplitude 5 nW correspond to approx. 1 pm/Hz @ 1064 nm 6. Oct. 2010 International Conference on Space Optics 2010 Page 39 Noise Sources Photodetection Noise • Amplitude Variations May also be described by an “additive noise” model • Best practice: minimize by active stabilization Laser Intensity Noise (RIN) Polarization Fluctuations Power Stabilization Polarization cleanup before Photodetectors A RIN of 10-5/Hz corresponds to approx. 1 pm/Hz 6. Oct. 2010 International Conference on Space Optics 2010 Page 40 Noise Sources Phase Measurement Noise • The phase measurement of the analog beat signal adds 2 main noise contributions A/D Quantization Noise ‒ Discretization by finite bit depth A/D Timing Jitter ‒ Non-synchronous sampling of the individual channels ‒ Impact of jitter is relative to sampling frequency! Further digital processing is free of uncertainties! 6. Oct. 2010 International Conference on Space Optics 2010 Page 41 Astrium Interferometer Performance Phase Measurement Noise FPGA Phasemeter (10 kHz) 6. Oct. 2010 International Conference on Space Optics 2010 Page 42 Astrium Interferometer Performance Photodetection & Phase Measurement Noise FPGA Phasemeter (10 kHz) 6. Oct. 2010 International Conference on Space Optics 2010 Page 43 Astrium Interferometer Performance End-to-End Performance – Aluminum Board FPGA Phasemeter (10 kHz) 6. Oct. 2010 International Conference on Space Optics 2010 Page 44 Astrium Interferometer Performance End-to-End Performance – First Results of Bonded Setup FPGA Phasemeter (10 kHz) 6. Oct. 2010 International Conference on Space Optics 2010 Page 45 Astrium Interferometer Performance End-to-End Performance – First Results of Bonded Setup FPGA Phasemeter (10 kHz) 6. Oct. 2010 International Conference on Space Optics 2010 Page 46 Astrium Interferometer Setup 6. Oct. 2010 International Conference on Space Optics 2010 Page 47 LISA Optical Bench Current Design Status cf. Talk on Friday, 11:20 “Optical Bench Development for LISA” Lightweighted Zerodur Baseplate 6. Oct. 2010 International Conference on Space Optics 2010 Page 48 Outline • Introduction • Interferometry Basics • Noise Sources in the Measurement Chain • Specific Challenges for Inter-S/C Metrology 6. Oct. 2010 International Conference on Space Optics 2010 Page 49 Inter S/C Interferometry • The physical separation of spacecraft linked by optical metrology over a comparatively large distance involves specific challenges Optical link budget S/C pointing and line-of-sight dynamics Time keeping over the constellation 6. Oct. 2010 International Conference on Space Optics 2010 Page 50 Inter S/C Interferometry Link Budget • The receiving aperture is in general much smaller than the far field beam width Transmission of a Gaussian Beam Reception of a “top hat plane wave” Dedicated and separated beam conditioning in TX and RX paths Shot noise is important! TX ghosts/stray light are important in monostatic systems LISA Off-Axis Telescope 6. Oct. 2010 International Conference on Space Optics 2010 Page 51 Inter S/C Interferometry Pointing Dynamics • One of the most dominant noise sources on inter-s/c links is coupling of pointing variations into the longitudinal signal Geometrical interpretation: “Phase Center Offset” from the desired fiducial point Results from a combination of alignment errors & optical (wavefront) errors Appropriate imaging optics in TX as well as RX paths! 6. Oct. 2010 International Conference on Space Optics 2010 Page 52 Inter S/C Interferometry Pointing Dynamics • “Differential Wavefront Sensing” (DWS) Very accurate acquisition of wavefront tilt (i.e. beam pointing) relative to the LO Spatially resolved phase measurement by use of Quadrant Photodetectors Tilt: Piston: 6. Oct. 2010 Quadrant Difference Quadrant Sum International Conference on Space Optics 2010 Page 53 Inter S/C Interferometry Pointing Dynamics • The “weak link” in the AOCS are thus usually the actuators (i.e. thrusters) µN Propulsion ‒ Field Emission Electric Propulsion (FEEP) ‒ RF Ion Thruster (RIT) ‒ High Efficiency Multistage Plasma Thruster (HEMPT) (In-orbit) calibration of the coupling coefficient Post-correction of the data on the basis of the ultra-precise DWS pointing information 6. Oct. 2010 International Conference on Space Optics 2010 Page 54 Inter S/C Interferometry Pointing Dynamics • Example: DWS Correction Pointing instabilities occur not only between s/c! “Optical Bench Development for LISA” ESA Contract No. 22331/09/NL/HB 6. Oct. 2010 International Conference on Space Optics 2010 Page 55 Inter S/C Interferometry Pointing Dynamics cf. Talk on Friday, 12:00 “Picometer Stable Scan Mechanism for Gravitational Wave Detection in Space” • Extreme demands on any beam manipulation mechanisms in the measurement path Pathlength stability Pointing stability pm nrad • Typical solution Piezo-based actuation principle Monolithic hinges Thermally compensated, isostatic support Point-Ahead Angle Mechanism 6. Oct. 2010 In-Field Pointing Mechanism International Conference on Space Optics 2010 Page 56 Inter S/C Interferometry Line-of-Sight Dynamics • The maximum beat frequency to be accommodated equals (at least) the Doppler shift Line-of-Sight motion of the respective s/c • Constant Doppler shift “just” generates a constant frequency offset Varying Doppler shifts require a “tracking” Phasemeter Optical frequency plan to avoid zero-crossings Astrium 8 Channel, RF DPLL Phasemeter 6. Oct. 2010 International Conference on Space Optics 2010 Page 57 Summary • In order to achieve Picometer measurement precision, each individual noise contribution in your Measurement Chain must be below a millionth of a cycle Employ heterodyne interferometry ‒ 1 – 10 MHz beat frequencies Ensure dimensional stability ‒ ‒ ‒ ‒ Low CTE baseplate Ultrastable, quasi-monolithic optics integration Athermal, isostatic mounting of mechanisms Passive & massive thermal shielding Active stabilization is better than post-correction ‒ Laser frequency stabilization ‒ Power stabilization ‒ Polarization cleanup Apply post-correction where stabilization reaches its limits ‒ Balanced Detection ‒ DWS detection of beam pointing fluctuations Optimize your Phase Measurement Chain ‒ Carefully select the laser powers on the detectors ‒ Care about the modematching of your beams ‒ Use the best ADCs with low timing jitter and high bit resolution 6. Oct. 2010 International Conference on Space Optics 2010 Page 58 Acknowledgments • Astrium • DLR • Joep Pijnenburg, Harm Hogenhuis, Ben Braam, … ESA 6. Oct. 2010 Karsten Danzmann, Gerhard Heinzel, Michael Tröbs, … TNO Science & Industry • Harry Ward, David Robertson, Ewan Fitzsimons, Christian Killow, Alasdair Taylor, Michael Perreur-Lloyd Albert-Einstein Institute • Achim Peters University of Glasgow • Claus Braxmaier HU Berlin • “Untersuchungen zur Systemleistung alternativer Nutzlastkonzepte für LISA” (DLR Contract No. 50OQ0701) HTWG Konstanz • Hans Reiner Schulte, Martin Gohlke, Ulrich Johann, … Luigi D’Arcio International Conference on Space Optics 2010 Page 59