1. ESA/DLR Blue Book Proposal High-Flux Scenario
ESA Presentation to CCSDS Optical Communications Working Group
11 November 2014

2. Books Under Development by OCWG
Blue Book
Optical Communications Physical Layer
Green Book Material
Optical Communications Physical Layer
Green Book
Optical Communications Concepts and Technologies
Editor: ESA
Draft uploaded
Material uploaded by ESA/DLR
Blue Book
Optical Communications Coding & Synchronization
Green Book Material
Optical Communications Coding & Synchronization
Green Book
Real-Time Weather and Atmospheric Characterization Data
Material uploaded by ESA/DLR
Material uploaded by ESA/DLR

3. ESA/DLR Input
Most material was provided by European industry, specifically TESAT Spacecom at the Spring 2014 CCSDS meeting.
Existing terminal implementation LCT is a commercially available product, with heritage extending back to 1997 (LEO-LEO) and a 2nd generation for LEO-GEO links developed since 2006.
LCT was flown on NFIRE and the German TerraSAR-X satellites, and has been selected for EDRS, with first terminals already launched on Sentinel 1a and AlphaSat. Operational validation is successfully underway.

4. Evolution of Existing Implementation
Current user bandwidth is 1.8 Gbps ( Gbps raw)
Doubling the clock rate (already in space since 2007 on NFIRE and TerraSAR-X) results in 3.6 Gbps user data rate.
Switching from BPSK to QPSK provides a user data rate of 7.2 Gbps. Benefit: Detector bandwidth remains within validated performance regime.
Further scaling by WDM around 1064 nm. Yb amplifier bandwidth is ≥60 nm.
Reply to NASA comment, that LCT is not scalable.

5. 1. Proposal Draft Blue Book Optical Communications Physical Layer
Green Book Material
Optical Communications Physical Layer
Green Book
Optical Communications Concepts and Technologies
Blue Book
Optical Communications Physical Layer
Material uploaded by ESA/DLR
Editor: ESA
Draft uploaded
Blue Book
Optical Communications Coding & Synchronization
Green Book Material
Optical Communications Coding & Synchronization
Green Book
Real-Time Weather and Atmospheric Characterization Data
Material uploaded by ESA/DLR
Material uploaded by ESA/DLR

6. Blue Book Optical Communications Physical Layer – Proposed Contents

7. 1.1 Signal Acquisition Terminal A
The center frequency shall be GHz ± 0.14%
The transmit beam shall have a Left-hand Circular Polarization (LCP: where the E-vector rotates counter-clockwise as viewed from the transmitter in the direction of propagation)
During spatial acquisition, the transmit signal shall be amplitude modulated with a frequency of MHz +/- 200 ppm and a modulation index higher than 95%.
Terminal B
The center frequency shall be ± 0.14%
The transmit beam shall have a Right-hand Circular Polarization (RCP: where the E-vector rotates clockwise as viewed from the transmitter in the direction of propagation)
During spatial acquisition, the transmit signal shall be amplitude modulated with a frequency of MHz +/- 200 ppm and a modulation index higher than 95%.

8. 1.2 Communication Signal (1/6)
Terminal A
The center frequency shall be GHz
The transmit beam shall have a Left-hand Circular Polarization (LCP: where the E-vector rotates counter-clockwise as viewed from the transmitter in the direction of propagation)
Terminal B
The center frequency shall be GHz
The transmit beam shall have a Right-hand Circular Polarization (RCP: where the E-vector rotates clockwise as viewed from the transmitter in the direction of propagation)

9. 1.2 Communication Signal (2/6)
Both Terminals
The TX laser shall be tunable within a range of +-10 GHz
The maximum laser tuning rate shall be 120 MHz/s in communication mode
The un-modulated TX laser shall have a line width of less than 100 kHz over a time scale of 100 msec
The TX laser Relative Intensity Noise (RIN) shall be less than -30 dB in the frequency range between 0.01 Hz and 1 MHz.

10. 1.2 Communication Signal (3/6)
Both Terminals
The spectral density of the RIN shall be better than given in the Figure below

11. 1.2 Communication Signal (4/6)
Both Terminals
The frequency noise of the free running TX laser shall be less than the limit in Figure below:
The change rate of the laser phase noise shall be below 6400 rad/s (Δφ/ Δt).

12. 1.2 Communication Signal (5/6)
Both Terminals
Modulation scheme: Binary Phase-Shift Keying (BPSK) with Non-Return to Zero (NRZ).
Nominal symbol rate: Megasymbols/sec (Msps).
The modulating base-band spectrum of the transmit signal shall fulfill the spectral mask defined in the Figure below. This spectrum shall be generated by the Line Product Code (LPC) as defined in Ref. CCSDS W-0 (Optical Communication Modulation and Coding Proposed Draft Recommended Standard White Book)

13. 1.2 Communication Signal (6/6)
Both Terminals
The base-band eye-pattern shall fulfill the requirements listed in the Table and as defined by the Figure below.

14. 2. Material Collection for Future Green Book Optical Communications Physical Layer
Blue Book
Optical Communications Physical Layer
Green Book
Optical Communications Concepts and Technologies
Green Book Material
Optical Communications Physical Layer
Editor: ESA
Draft uploaded
Material uploaded by ESA/DLR
Blue Book
Optical Communications Coding & Synchronization
Green Book Material
Optical Communications Coding & Synchronization
Green Book
Real-Time Weather and Atmospheric Characterization Data
Material uploaded by ESA/DLR
Material uploaded by ESA/DLR

15. Contents - Green Book Material Optical Communications Physical Layer

16. 2.1 Spatial Acquisition PAT
Mutual spatial tracking and, in the case of homodyne communications, locking and tracking of the opposing terminals carrier frequency must be achieved.
Depending on the relative size of the open-loop pointing Uncertainty Cone (UC) and the aperture dependent Tx beam divergence, acquisition sequences either assisted by a higher-divergence Beacon or “Beaconless” acquisition schemes may be appropriate.
Detection and centering of a beacon requires utilization of a 2-D sensor (e.g. CCD or Quadrant Photodiode).
High divergence beacon requires high optical transmit power.
Size of UC determines necessary acquisition strategy and speed. Contributing factors are:
Timing accuracy
Position knowledge
Attitude knowledge
(Micro)-vibration
Planning cycle and Telecommand opportunities

17. 2.1 Spatial Acquisition Beaconless PAT
A beaconless PAT scheme is implemented in the European Data Relay System (EDRS) and has been verified in-orbit with the TerraSar-X NFire optical LEO intersatellite links.
It uses the comms beam (i.e. same wavelength and beam divergence as the comms signal) and scans the UC to achieve spatial acquisition.
The scanning methodology mandates a time tagged sequence of steps.
The transmitted beam is modulated to facilitate terminal identification and to improve the PAT link budget.
Establishment of a link with the EDRS optical terminals requires knowledge of only the normative characteristics of the optical signal (wavelength, modulation, etc.).
The knowledge of the time tagged acquisition sequence is beneficial and recommended to be agreed upon in a mission-specific ICD.

18. 2.2 Acquisition Sequence Beaconless PAT
Beacon-less acquisition sequence in a master-slave approach. M: master terminal, S: slave terminal

19. 2.2 Acquisition Sequence Beaconless Spatial Acquisition
Simplified flow chart of the beaconless spatial acquisition algorithm

20. 2.2 Acquisition Sequence Frequency Acquisition
After successful spatial acquisition, the next step in the acquisition sequence is to achieve homodyne tracking by performing frequency acquisition. The laser frequencies of the respective local oscillators must be adjusted such that they are phase-locked to the received signal.
On completion, each terminal is coherently phase locked to the counter terminal. Homodyne tracking is thus achieved and the terminals are ready to initiate communication.

21. 2.3 Acquisition Time
Length of the acquisition time is determined mainly the size of the total UC of the link.
Based on the size of the UC, a trade-off between reliability and speed of link acquisition is required.
In a highly dynamic LEO-LEO intersatellite link configuration acquisition times of 8 s (and in specific cases 2 s) have been demonstrated in-orbit.
For uncertainty cones of 1 mrad, acquisition times of 55 s are guaranteed for the EDRS intersatellite and ground link (including a safety margin).
Shorter acquisition times are expected after in-orbit verification.

22. 2.4 Optical Signal Characteristics
Optical signal characteristics are valid for coarse and fine spatial acquisition. For tracking, communications signal characteristics apply (direct detection on acquisition sensors, but coherent detection on tracking detector).

23. 3. Material for Blue Book Optical Communications Coding & Synchronization
Optical Communications Physical Layer
Green Book Material
Optical Communications Physical Layer
Green Book
Optical Communications Concepts and Technologies
Blue Book
Optical Communications Coding & Synchronization
Editor: ESA
Draft uploaded
Material uploaded by ESA/DLR
Material uploaded by ESA/DLR
Green Book Material
Optical Communications Coding & Synchronization
Green Book
Real-Time Weather and Atmospheric Characterization Data
Material uploaded by ESA/DLR

24. Contents - Blue Book Material Optical Communications Coding & Synchronization

25. 4. Material Collection for Future Green Book Optical Communications Coding & Synchronization
Blue Book
Optical Communications Physical Layer
Green Book Material
Optical Communications Physical Layer
Green Book
Optical Communications Concepts and Technologies
Green Book Material
Optical Communications Coding & Synchronization
Editor: ESA
Draft uploaded
Material uploaded by ESA/DLR
Material uploaded by ESA/DLR
Blue Book
Optical Communications Coding & Synchronization
Green Book
Real-Time Weather and Atmospheric Characterization Data
Material uploaded by ESA/DLR

26. Contents - Green Book Material Optical Communications Coding & Synchronization