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PRECISON TIMING CONTROL FOR RADIO ASTRONOMY

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THE HUBBLE TELESCOPE AND ITS IMAGE FROM NEW MEXICO ... back to correlaters in Central Bldg to finally generate astronomical images. ... – PowerPoint PPT presentation

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Title: PRECISON TIMING CONTROL FOR RADIO ASTRONOMY


1
PRECISON TIMING CONTROL FOR RADIO ASTRONOMY
2
GROUP MEMBERS
  • SURENDRA KUMAR BATCHU
  • SRIDHAR SONGOJU
  • SAI SAMEER TADIMETI VENKATA
  • AMARDEEP BADDAM
  • DILEEP THAMMAIAHGARI

3
ATACAMA LARGE MILLIMETER ARRAY
  • An international radio astronomical facility
    under construction in Chile
  • In collaboration with USA,Canada,Europe and Japan
  • Consists of an array up to 64 12m parabolic
    antennas
  • Detects radio waves in the frequency band 91-350
    ghz
  • Located at an elevation of 5000m

4
MAIN ADVANTAGES
  • Able to reveal the structure of the cold regions
    of the universe with greater sensitivity and
    resolution
  • And even the dark at visible wave lengths
  • Moves is various directions

5
BASIC SETUP
6
THE HUBBLE TELESCOPE AND ITS IMAGE FROM NEW MEXICO
7
Photonic Local Oscillator (LO) reference
distribution system
8
Photonic Local Oscillator (LO) reference
distribution system
  • Distribution system consists of Central Building
    and
  • array of 64 Antennas .
  • Central Building houses
  • Master Laser (ML)
  • Laser Synthesizer (LS)
  • Line length corrector (LLC)
  • Each Antenna has a
  • Photo detector
  • Local/Antenna Oscillators
  • Mixers Digitization and Transmission
    circuit

9
Photonic Local Oscillator (LO) reference
distribution system
  • Distribution system aims at optical transmission
    of LO reference signal to the antennas with
    required stability(38 fs).
  • LO signal consists of two optical waves -- Master
    Laser and Slave Laser-- of wavelength around
    1.556 µm.
  • Slave Laser is phase locked with Master Laser
    with frequency offset ranging between 27-142 GHz.
  • Lo reference is transmitted to each and every
    antenna through LLC.

10
Photonic Local Oscillator (LO) reference
distribution system
11
Photonic Local Oscillator (LO) reference
distribution system
  • At each antenna LO signal is sent to photo
    detector which outputs Lo ref signal ranging
    between 27-142GHz.
  • This 27-142 GHz LO ref is used to phase-lock the
    antenna oscillators which output LO ref at 27
    -938GHz.
  • This LO ref is used to down convert sky signals
    (31-950 GHz ) to Intermediate frequency (IF) band
    of 4-12 GH z.
  • IF signal is transmitted back to correlaters in
    Central Bldg to finally generate astronomical
    images.

12
ALMA LASER SYNTHESIZER
13
OPTICAL PHASE LOCK LOOP
  • Laser can be thought of as a noisy oscillator
    whose output is not an ideal sinusoidal wave and
    the output is given by
  • E(t) A(t) cos(2p fc t
    f(t))..(1)
  • where E(t) is the amplitude of the
    electrical field of the optical wave, A(t) is the
    amplitude noise, fc is the average optical
    frequency of the wave and f(t) is the phase
    noise.
  • The beat signal equation is given by
  • ibeat(t) A1(t)A2(t) cos(2p( f1 - f2)t
    f1(t) - f2(t))

14
LOOP BANDWIDTH
  • The bandwidth of OPLL is computed by measuring
    the power spectral density (PSD) of the combined
    phase noise of the ML and slave Lasers and
    applying the transfer function correspo0nding to
    the closed loop response of the error signal
    relative to input changes.
  • Low-frequency phase fluctuations are thus tracked
    almost perfectly, whereas fluctuations outside
    the locking bandwidth remain largely unaffected.
  • The total residual phase noise power is given by

15
LOOP BANDWIDTH
  • In this case, the OPLL acts as a highpass filter
    and the OPLL cutoff frequency necessary for
    meeting a given phase noise level can be
    estimated.

16
OPTICAL PHASE CONTROL
  • To provide actuation for closed loop control, a
    mechanism for changing the optical phase of slave
    laser a bandwidth of at least 1MHz is needed.
  • One mechanism uses the tuning of the frequency of
    the fiber which is achieved by applying a voltage
    to a piezo crystal, which stretches the Bragg
    grating.
  • A "Bragg Grating" is a periodic or non-periodic
    perturbation of the effective absorption
    coefficient and/or the effective refractive index
    of an optical waveguide. More simply put, a Bragg
    Grating can reflect a predetermined narrow or
    broad range of wavelengths of light incident on
    the grating, while passing all other wavelengths
    of the light.

17
OPTICAL PHASE CONTROL
  • By increasing the frequency of the optical wave,
    the optical wave of the slave laser will
    oscillate more rapidly and consequently the phase
    also gets increased.
  • In this way the frequency is increased until the
    slave laser catches up the phase with the ML and
    vice versa.
  • The laser tuning is mechanical in nature and
    displays lightly damped mechanical resonances
    above 20KHz. These resonances introduce phase
    lags that prevent high loop bandwidth.

18
OPTICAL PHASE CONTROL
  • To prevent this we use an external optical
    frequency shifter (AOM-acousto-optic modulator
    which is used to apply small but fast frequency
    changes to the laser output.

19
FEEDBACK NETWORK
  • The feedback network circuit of the OPLL
    is split into two parallel branches
  • One with the fast frequency shifter
    handling the high frequency, low-amplitude
    compensation.
  • The remaining low-frequency phase error is
    cancelled by a second feedback network circuit
    driving the laser-piezo.

20
AUTOMATION OF PHASE LOCKING
  • The phase locking control system is based on
    analog electronics to achieve high accuracy and
    high bandwidth
  • The LS (Laser Synthesizer) includes an embedded
    computer that receives frequency tuning requests
    from the ALMA central controller through a CAN
    (controller area network) Bus link.
  • The controller then sets the RF frequency
    synthesizer to a particular offset and tunes the
    slave laser until the frequency difference
    between ML and slave lasers is close enough to be
    within the phase-locking range.

21
LINE LENGTH CORRECTOR
  • The reference LO signal arriving at antenna must
    be stable.
  • Change in the length of Fiber due to Optical and
    Electrical components, antenna rotation.
  • Introduces the propagation delay.
  • So a technique to stabilize the fiber length is
    needed.

22
LINE LENGTH CORRECTOR
  • Line Length Correction (LLC) is used to correct
    the length
  • LLC is used to correct the length of the fiber to
    maintain the constant phase difference.
  • The Optical wave shifts by 2p when length
    changes by 1.5 µm.

23
LINE LENGTH CORRECTOR
24
LINE LENGTH CORRECTOR
  • Gain of each loop must be set to prevent the
    destabilizing of system.
  • Maximum Bandwidth of LLC is limited by
    propagation delay of light in the fiber.

25
LINE LENGTH CORRECTION RESULTS
26
THE MASTER LASER
  • INTRODUCTION
  • LASER SOURCE
  • THE OPTICAL REFERANCE
  • THE FREQUENCY CONTROL LOOP
  • AUTOMATION OF FREQUENCY LOCKING

27
INTRODUCTION
  • The interferometric measurement of the fiber
    length performed
  • by the LLC uses the optical beam originating
    in the ML as a
  • reference.
  • This measurement method imposes two important
  • requirements on the ML.
  • The coherence length of the ML must be
    sufficiently long (gt30 km in fiber)
  • (The distance over which
    interference will occur )
  • 2. The optical frequency of the ML must possess
    a relative frequency stability that is better
    than the required relative fiber length accuracy

28
The laser source
  • A 1,556-nm distributed feedback (DFB) fiber
    laser is
  • used as the source for the ML.
  • This laser provides a compact and robust device
    with a
  • narrow line width and, therefore, a long
    coherence
  • length.
  • The frequency stability of such lasers is
    insufficient for the
  • LLC system since their frequency can fluctuate
    by tens of
  • MHz as a function of ambient temperature and
    time.

29
Optical Reference
  • The optical reference selected for the ML is a
    transparent
  • cell containing low-pressure gas of rubidium
    (Rb) atoms.
  • Rb has the property that when a 778-nm (red)
    laser beam
  • with the exact right frequency passes through
    the gas, a
  • faint 420-nm (blue) fluorescence signal is
    emitted by the
  • excited Rb atoms
  • Since this two photon transition is highly
    stable and occurs
  • only in a narrow band of optical frequencies
    (theoretically less
  • than 200 kHz at 1,556 nm), the transition can
    be used as a
  • sensitive frequency discriminator signal to
    which the laser
  • can be locked to improve its frequency
    stability

30
THE MASTER LASER PROTOTYPE
31
  • The 1,556-nm DFB fiber laser output is converted
    into
  • 778-nm light by using an optical frequency
    doubler.
  • The frequency doubling is performed by a
    periodically
  • poled lithium niobate (PPLN) crystal, which
    is an
  • optically nonlinear element.
  • The temperature set point of the oven is
    continuously
  • optimized by the ML controller using a slow
    locking loop
  • algorithm implemented in software.
  • The 778-nm light is then sent through the Rb
    cell
  • and reflected back on itself to stimulate
    the two-
  • photon transition of Rb

32
The Frequency Control Loop
  • To facilitate laser locking at the frequency
    where
  • fluorescence is maximum, the 778-nm beam is
    phase
  • modulated using an electro-optic modulator
    (EOM).
  • This phase modulation creates a sideband of
    opposite
  • phase on each side of the optical carrier
  • If the optical frequency of the laser is on the
    center
  • of the symmetrical two-photon transition, both
    sidebands
  • are absorbed equally by the narrow line width,
    cancelling
  • out completely.

33
Automation of the Frequency Locking
  • An embedded controller plays the crucial role of
    automating
  • the locking of the ML on the desired
    two-photon transition of
  • Rb.
  • It is not possible to tune the laser with
    sufficient accuracy to
  • place its frequency within the locking range
    of the desired
  • transition.
  • To solve this problem, the ML embedded software
    implements
  • an automatic frequency calibration and locking
    algorithm
  • Once the correct transition is found, the
    frequency of the
  • laser is adjusted close to the targeted value
    and the locking
  • loop is activated.

34
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35
CONCLUSION
  • Dealt with three important subsystems namely
    1)Laser Synthesizer
  • 2)Line Length Corrector
  • 3)Master Laser
  • ALMA is built around more control systems and
    feedback loops and antenna positioning systems.
  • Gives what was invisible to previous instruments

36
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37
THANK YOU
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