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Operations Design, Test and In-Flight Experience of the Sentinels Optical Communications Payload (OCP)

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Abstract

The Copernicus Sentinel-1 and Sentinel-2 Earth Observation missions are the first in history to use a LEO to GEO optical communications (i.e. laser) link to routinely downlink stored science data to the ground. The start of routine operations with EDRS A has represented a major milestone for both of the Sentinels missions and is the culmination of more than two years of intense and sustained operational validation activities by the FCTs. This chapter provides a summary of validation and test activities that have been performed during the Sentinel-1 and 2 satellite commissioning, then with Alphasat and finally with EDRS A, to achieve the current operational state. This chapter also describes how the OCPs are accommodated on the Sentinel-1 and Sentinel-2 satellites and the on-board services each OCP requires. The basic principles of how the OCPs on the LEO and GEO spacecraft establish a communications link with each other are also described. Each Sentinel spacecraft executes between 9 and 12 OCP communications links per day. The timing of these links is scheduled by the Sentinels Payload Data Ground Segment (PDGS) with the EDRS A service provider. The PDGS provides the link timing information to the Sentinels Flight Operations Segment (FOS) at ESOC where the Sentinels Mission Planning System has a dedicated function that is used to determine the necessary telecommand parameters for uplink and execution. We will describe the end-to-end link planning concept and process, highlighting the data exchange interfaces and will explain what telecommand parameters the OCP requires to execute a link and how they are calculated. The start of routine OCP operations with EDRS A has also introduced an extra level of operational complexity into the daily operations working practice of both Sentinel-1 and 2. Next, we will describe the impact of the routine OCP operations on the following operational areas; mission planning operations; orbit maintenance operations; collision avoidance operations; anomaly recovery operations; general operations working practice. The chapter will also focus on the operation lessons learned. We will also summarize the benefits to each mission of optical communications, showing how the use of optical communications, together with X-band ground station downlinks, has been used to maximize the data output of the missions. Finally, we will describe how the OCPs will be used in the future on both Sentinel-1 and Sentinel-2.

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Abbreviations

AOCS:

Attitude and Orbit Control Subsystem

AVS:

Avionics Subsystem

CAM:

Collision avoidance manoeuvre

COD:

Coarse Orbit Determination (on-board)

CPA:

Coarse Pointing Assembly

CW:

Calendar week

DM:

Deployment mode

DSHA:

(Science) Data Storage and Handling Assembly

EDRS:

European Data Relay Satellite

EM:

AOCS Emergency Mode (AOCS)—spacecraft 3-axis stabilized

EOL:

End of life

EPS:

Electrical Power Subsystem

FCT:

Flight Control Team

FD:

Flight dynamics

FDIR:

Fault Detection, Isolation and Recovery

FOS:

Flight Operations Segment (i.e. ESOC)

FOV:

Field of view

GEO:

Geostationary orbit

GPSR:

Global Positioning System Receiver

GPST:

Global Positioning System (GPS) Time

GS:

Ground Segment

GSOC:

German Space Operations Centre

GSOV:

Ground Segment Operational Validation

HKTM:

Housekeeping telemetry

HW:

Hardware

LCT:

Laser Communication Terminal

LEO:

Low Earth Orbit

LIAU:

LCT interface adapter unit

LLD:

Launch lock device

LRAD:

LCT radiator

LOS:

Line of sight

MCS:

Mission Control System

MPS:

Mission Planning System

NMM:

(Spacecraft) Nominal Mission Mode (SAR payload on)

NPM:

AOCS Nominal Pointing Mode—fine pointing using GSPR and star trackers

NPPF:

Nominal Payload Planning File

NVRAM:

Non-volatile random access memory

OBOP:

On-board operations procedure

OCM:

Orbital control manoeuvre

OCP:

Optical communication payload

OEM:

Orbit Ephemeris Message

OPLL:

Optical phase-locked loop

OPA:

Optical power amplifier

ORR:

Operational readiness review

PAA:

Pointing Ahead Assembly

PDGS:

Payload Data Ground Segment (i.e. ESRIN)

PDHT:

Payload Data Handling and Transmission subsystem

PPS:

Pulse Per Second

POD:

Precise Orbit Determination (on-board)

PVT:

Position, Velocity, Time

RAM:

Random access memory

RCT:

Reaction control thruster

S1A:

Sentinel-1A

S1B:

Sentinel-1B

S2A:

Sentinel-2A

S2B:

Sentinel-2B

SAR:

Synthetic aperture radar (payload)

S/C:

Spacecraft

SKM:

Station keeping manoeuvre

SW:

Software

T 0 :

OCP Link Synchronization Time

TB:

Terabyte

TC:

Telecommand

TM:

Telemetry

References

  1. Sentinels FOS Team. Sentinels FOS System Architecture Document, GM-IC-ESC-FS-1020.

    Google Scholar 

  2. Shurmer, I., Marchese, F., & Morales, J. (2018). Sentinels optical communications payload (OCP) operations: From test to in-flight experience. In Spaceops 2018.

    Google Scholar 

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Acknowledgements

Mr. I. Shurmer and Mr. F. Marchese would like to thank the Sentinel-1 and Sentinel-2 FCTs for their great work, and stamina, over the last 3–4 years in implementing and executing the OCP operations concept. They would also like to thank the Sentinel-1 and Sentinel-2 PDGS and project teams for their support. Finally, they would like to thank the industry team at Tesat for their, always cheerful, expert technical support over the whole period.

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Correspondence to F. Marchese .

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Shurmer, I., Marchese, F., Morales, J. (2019). Operations Design, Test and In-Flight Experience of the Sentinels Optical Communications Payload (OCP). In: Pasquier, H., Cruzen, C., Schmidhuber, M., Lee, Y. (eds) Space Operations: Inspiring Humankind's Future. Springer, Cham. https://doi.org/10.1007/978-3-030-11536-4_27

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  • DOI: https://doi.org/10.1007/978-3-030-11536-4_27

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-030-11535-7

  • Online ISBN: 978-3-030-11536-4

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