Frequency electronics, inc. Rb and quartz oscillators for space applications

Содержание

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Frequency Electronics, Inc. FEI was started 51 years ago with a

Frequency Electronics, Inc.

FEI was started 51 years ago with a mission

to bring precision timing technology from the laboratory to the real world
FEI is a Long-Recognized Technology Leader
High Precision Timing, Space Applications
Low Phase Noise Microwave Sources and Synthesizers
Low “G”- Sensitivity Clocks
Timing/Frequency Systems for Severe Environments
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Development of Rb and Quartz Oscillators for Space Applications Quartz Clock

Development of Rb and Quartz Oscillators for Space Applications

Quartz Clock Performance

in Space
Rb Atomic Clocks in Space – The Results So Far
Next Generation Rb Atomic Clock for Space Applications
Design, Rb Atomic Frequency Standard (RAFS)
Performance Results, RAFS
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Introduction For the past 50 years, most satellite systems have used

Introduction

For the past 50 years, most satellite systems have used precision

quartz oscillators as the time and frequency reference
Reliable
Low Power
Light Weight
Atomic Frequency Standards have demonstrated reliable operation in space during the last 25 years on a limited number of programs
GPS
Glonass
Milstar/AEHF
Galileo
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Technology Trade-offs Quartz oscillators are the most reliable, lowest cost technology

Technology Trade-offs

Quartz oscillators are the most reliable, lowest cost technology for

providing precision frequency and time in space applications
Quartz is inherently sensitive to nuclear radiation
Atomic frequency standards cost more, are less reliable, but provide improved frequency stability, and are relatively immune to radiation
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Development of Rb and Quartz Oscillators for Space Applications Quartz Clock

Development of Rb and Quartz Oscillators for Space Applications

Quartz Clock Performance

in Space
Rb Atomic Clocks in Space – The Results So Far
Next Generation Rb Atomic Clock for Space Applications
Design, Rb Atomic Frequency Standard (RAFS)
Performance Results, RAFS
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State of the Art Quartz Performance in Space Usage of “Premium

State of the Art Quartz Performance in Space

Usage of “Premium Q

Swept Quartz” or radiation hardened quartz material.
SC-cut crystals (SC-cut crystals stabilize faster than AT-cut crystals. The retrace of SC-cut crystals is orders of magnitude better than AT-cut crystals).
5th overtone resonators (aging is significantly affected by the thickness of the resonator, hence, the thickest quartz blank should be used at the highest practical overtone for best aging performance).
Crystals exhibiting monotonically-positive aging slope (radiation offsets the positive aging trend of quartz as further explained below).
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Radiation Effects on Quartz Quartz sensitivity to most radiation has been

Radiation Effects on Quartz

Quartz sensitivity to most radiation has been shown

to be approximately: -1E-12 per Rad
Typical background radiation for geosynchronous orbit is: 6 Rads/day
Typical frequency aging on earth is ~1E-11/day for high precision quartz oscillators
On-orbit compensation resulting in frequency aging of ~1E-12/day is possible for positive aging quartz resonators
Quartz sensitivity to protons is similar magnitude, but less predictable; and can result in positive or negative frequency changes

Even with compensation for background radiation:
best performance observed in space is ~2E-13/day
effect of solar flare is 1E-10 to 4E-10 over several days

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State of the Art Quartz Oscillator Lᵠ(f) = -133 dBC/Hz @

State of the Art Quartz Oscillator

Lᵠ(f) = -133 dBC/Hz @ 1

Hz offset
ADEV = 7E-14 @ 10 sec
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Development of Rb and Quartz Oscillators for Space Applications Quartz Clock

Development of Rb and Quartz Oscillators for Space Applications

Quartz Clock Performance

in Space
Rb Atomic Clocks in Space – The Results So Far
Next Generation Rb Atomic Clock for Space Applications
Design, Rb Atomic Frequency Standard (RAFS)
Performance Results, RAFS
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Overview Compared to crystal oscillators, atomic clocks are inherently insensitive to

Overview

Compared to crystal oscillators, atomic clocks are inherently insensitive to space

radiation.1
Compared to other types of atomic clock (e.g., Cs),
Rb clocks have the advantage of size, weight, and power,
Rb clocks have the (believed) disadvantage of relatively large frequency aging.
To better understand the utility of Rb clocks for long-term space missions, we have investigated Milstar Rb clocks (on-orbit) over the past two decades.
Contrary to popular mythology,
Rb clocks can have exceptionally long life with stable operation,
Rb clocks can have extremely low frequency-aging rates: 10-14 to 10-15/day

1) J. Camparo, S. Moss, & S. LaLumondiere, Space-system timekeeping in the presence of solar flares, IEEE Aerospace and Electronic SYSTEMS Magazine, 19(5), 3-8 (2004).

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Milstar Rb Clocks The Milstar Rb atomic clocks are manufactured by

Milstar Rb Clocks

The Milstar Rb atomic clocks are manufactured by Frequency

Electronics, Inc. (FEI)
The clock is a classical Rb vapor-cell design, with optical excitation using an rf-discharge lamp.2
The clock has a 10 year design life.
The clock has a weight of 2.3 kg (i.e., 5 lbs.).
The clock frequency can be tuned with a resolution better than 1× 10-12.

2) T. McClelland, I. Pascaru, M. Meirs, Development of a Rb Frequency Standard for the MILSTAR Satellite System, 41st Annual Symposium on Frequency Control, 1987, p. 66

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On-Orbit Data: Rb Satellite Clocks Functional Fit: y(t) = Ae-γwt +

On-Orbit Data: Rb Satellite Clocks Functional Fit: y(t) = Ae-γwt + Be-γet

+ Dt

Empirically, we find that as a family the data is well fit by a bi-exponential plus linear term:
Clock “warm-up”
Ae-γwt
This term may be due to movement of the liquid Rb pool in the discharge lamp.
Clock Equilibration4
Be-γet
The mechanism of equilibration is not yet understood.
Nevertheless, helium permeation remains an open possibility.
Linear Frequency Aging
Dt
The mechanism of linear frequency aging is not yet understood.

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Six clocks have operated on orbit (data for three presented here)4

Six clocks have operated on orbit (data for three presented here)4
Longest

operating time on-orbit is 14.8 years
Including estimates for ground operation, 3 of these clocks have logged more than 18 years of operation!

Milstar Rb Satellite Clocks Summary

4) J. Camparo, T. McClelland, and J. Hagerman, “Long Term Behavior of Rb Clocks in Space,” European Frequency and Time Forum, 2012.

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Development of Rb and Quartz Oscillators for Space Applications Quartz Clock

Development of Rb and Quartz Oscillators for Space Applications

Quartz Clock Performance

in Space
Rb Atomic Clocks in Space – The Results So Far
Next Generation Rb Atomic Clock for Space Applications
Design, Rb Atomic Frequency Standard (RAFS)
Performance Results, RAFS
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Design Goals Precision Rubidium Atomic Frequency Standard (RAFS) for Space Applications

Design Goals

Precision Rubidium Atomic Frequency Standard (RAFS) for Space Applications
Best possible

frequency stability
20 year operating life
Emphasis on frequency stability rather than size, weight and power (SWAP)
“Classical” Rb vapor frequency standard
Optical pumping using Rb lamp to create ground state hyperfine population difference
Temperature controlled filter cell with Rb85
Temperature controlled resonance cell, with Rb87, in microwave cavity
One prototype, 3 engineering models
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Development of Rb and Quartz Oscillators for Space Applications Quartz Clock

Development of Rb and Quartz Oscillators for Space Applications

Quartz Clock Performance

in Space
Rb Atomic Clocks in Space – The Results So Far
Next Generation Rb Atomic Clock for Space Applications
Design, Rb Atomic Frequency Standard (RAFS)
Performance Results, RAFS
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Rb Atomic Frequency Standard (RAFS) 15 x 4.6 x 5.2 inches

Rb Atomic Frequency Standard (RAFS)

15 x 4.6 x 5.2 inches (381 x

117 x 132 mm)
16.5 Lbs (7.5 kg)
28 VDC Input
30 Watts
10 MHz Output
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Block Diagram Temperature controlled chassis (±1°C) operates from -34°C to +25°C

Block Diagram

Temperature controlled chassis (±1°C) operates from -34°C to +25°C
Modular Design


Digital Rb control loop
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Digital Rb Control Loop Digital processing of analog signal from physics

Digital Rb Control Loop

Digital processing of analog signal from physics package
Space

qualified FPGA
Direct Digital Synthesizer (within FPGA) to tune output frequency (1 x 10-14 tuning resolution)
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6.8 GHz Frequency Synthesizer Phase locked CRO at 2.278 GHz Output

6.8 GHz Frequency Synthesizer
Phase locked CRO at 2.278 GHz
Output signal at

6.8 GHz has no sidebands within a ±2.278 GHz window
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Radiation Hardening Component selection FPGA Frequency setting stored on select resistors

Radiation Hardening

Component selection
FPGA
Frequency setting stored on select resistors connected to input

pins
Fuse programmed (write once)
Hardware triple redundant logic, with three way voting to minimize single event effects
Software triple redundant logic with 3 way voting of critical values (digital output to DAC (quartz oscillator control voltage))
Radiation shields
Chassis, covers (material and thickness)
Spot shields for critical components
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Development of Rb and Quartz Oscillators for Space Applications Quartz Clock

Development of Rb and Quartz Oscillators for Space Applications

Quartz Clock Performance

in Space
Rb Atomic Clocks in Space – The Results So Far
Next Generation Rb Atomic Clock for Space Applications
Design, Rb Atomic Frequency Standard (RAFS)
Performance Results, RAFS
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Relative Frequency vs Time prototype unit in vacuum

Relative Frequency vs Time prototype unit in vacuum

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Allan Deviation Prototype Unit in vacuum

Allan Deviation Prototype Unit in vacuum

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Allan Deviation multiple units, in vacuum

Allan Deviation multiple units, in vacuum

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Warm-Up and Stabilization SN 01 in vacuum, -4°C

Warm-Up and Stabilization SN 01 in vacuum, -4°C

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Initial Warmup SN 01 in vacuum, -4°C

Initial Warmup SN 01 in vacuum, -4°C

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Frequency vs Temperature SN 01, in vacuum 1E-14 per °C

Frequency vs Temperature SN 01, in vacuum

1E-14 per °C

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Power Consumption SN 01 in Vacuum

Power Consumption SN 01 in Vacuum

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Frequency vs Magnetic Field SN 01 in vacuum

Frequency vs Magnetic Field SN 01 in vacuum

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Allan Deviation SN 03 SN 03, vacuum

Allan Deviation SN 03 SN 03, vacuum