More Related Content Similar to Optically pumped cesium enabling ePRC and ePRTC Class B (20) Optically pumped cesium enabling ePRC and ePRTC Class B1. Optically pumped cesium enabling ePRC and ePRTC
Class B
Alain Michaud, director, R&D and PLM, time and frequency
ITSF 2017
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Cesium clock as time source
PRC (G.811)
Frequency
PRC : Cs or GNSS
Sync
network
SSU
SSU
NE NE NE
PRTC (G.8272)
Frequency + phase
PRTC : GNSS
Sync
network
Packet slave clock
Packet master clock
NE NE NE
ePRTC (G.8272.1)
Frequency + phase
GNSS
Sync
network
Packet slave clock
Packet master clock
NE NE NE
CsCombiner
Cs as backup
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ePRTC: enhanced PRTC (ITU-T G.8272.1)
What is enhanced?
Cesium clock to filter GNSS instabilities:
• Atmospheric interference
• Solar storms
• Equatorial diurnal ionospheric variation
30ns MTIE in GNSS locked mode
Cesium clock: resiliency against GNSS outage
100ns MTIE over 14 days in holdover
mode
MTIE
τ(s)
15ns
100ns
1ns
0.1 1 10 100 400k1k 10k
10ns
100k 1M 10M 100M
30ns
4ns
30ns
30ns
100ns
4ns
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Where is ePRC hiding?
ePRTC (G.8272.1)
Frequency + phase
GNSS
Sync
network
Packet slave clock
Packet master clock
NE NE NE
Cs
Combiner
ePRTC
ePRC (G.811.1)
Frequency domain
Requires 10-12
frequency accuracy
(Achieved with magnetic
cesium clocks)
Cs
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ePRTC Class A holdover requirement
ePRTC-A
holdover
spec
Free running cesium
oscillator
Frequency of cesium
made coherent to UTC
in tracking mode
(ePRTC)
ePRTC Class A phase/time holdover measurement
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ePRTC G8272.1 – phase error in holdover
Evolution toward Class B holdover
Class B: requires a frequency accuracy below 1 x 10-14
ePRTC Class Holdover performance
ePRTC-A 100ns over 14 days
ePRTC-B 100ns over 80 days (project)
Could also be a tighter error budget over a shorter period
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F=3,4 RFLaser Laser
N
S
N
S
F=3,4 RF
• Weak flux
• Strong velocity selection (bent)
• Magnetic deflection (atoms kicked off)
• Typical performances: ADEV
• 2.7 x 10-11 x t-1/2
• High flux (x100)
• No velocity selection (straight)
• Optical pumping (atoms reused)
• Typical performances: ADEV
• 3 x 10-12 x t-1/2
Improving frequency stability with optical pumping
(versus magnetic deflection)
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Improving frequency stability with optical pumping
(versus magnetic deflection)
• Atomic energy states
• Ground states (F=3,4) equally populated
• Excited states (F’=2,3,4,5) empty
• Switching between ground states F by RF
interaction 9.192GHz without atomic
selection (no useful differential signal)
• Atomic preparation by magnetic
deflection (loss of atoms)
• Atomic preparation by optical pumping
with laser tuned to F=4 F’=4 transition
(gain of atoms)
F’=5
F’=4
F’=3
F’=2
nRF = 9.192GHz
F=4
F=3
133Cs atomic energy levels
l = 852.1nm
or
nopt = 352THz
Absorption
Spontanousemission
Cs beam
Resonant cavity
(Ramsey)
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Available commercial Cs clock products
• Long-life magnetic Cs clock
• Stability : 2.7 x 10-11 x t-1/2
• Floor : 5 x 10-14
• Lifetime : 10 years
• High-performance magnetic Cs clock
• Stability : 8.5 x 10-12 x t-1/2
• Floor : 1 x 10-14
• Lifetime : 5 years
• High-performance and long-life optical clock
• Stability : 3.0 x 10-12 x t-1/2
• Floor : 5 x 10-15
• Lifetime : 10 years
Long-life MAGNETIC
High-perf
MAGNETIC
Super-high-perf
long-life
OPTICAL
ADEV: Allan Deviation
Three generations of commercial clocks
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Decomposition of ePRTC holdover phase error budget
Origin of phase
error
Note Required for ePRTC-B
Initial phase error
GNSS instabilities + clock
stability
+/- 30ns as per ePRTC G.8272.1
How to use only ±10ns?
High-stab. GNSS+
High-stability clock
Random phase
excursions (holdover)
White frequency noise +
flicker frequency noise
cesium clock
Higher-
stability
clocks
Typ. Φ excursion magnetic Typ. Φexcursion optical
(±20ns) (±5ns)
Phase drift due to
initial clock freq. offset
Which is a function of:
- Clock stability @Tau > 1d
- GNSS stability @Tau >1d
Higher-stability GNSS +
Higher-stability clock (long term)
Required:
Freq. error < 5 x 10-14 ePRTC-A
Freq. error < 1 x 10-14 ePRTC-B
White frequency
noise
Flicker frequency noise
(floor)
Initial frequency
error
+
+
11. Thank You
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