Difference between revisions of "The Field of Optical Communications"

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==NASASmall Satellites Technology Project==
 
==NASASmall Satellites Technology Project==
 
===Optical Communications and Sensor Demonstration (OCSD)===
 
 
{{satellite
 
{{satellite
 
| header = OCSD-1 (AeroCube 7A)
 
| header = OCSD-1 (AeroCube 7A)
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| size = 1.5U
 
| size = 1.5U
 
}}
 
}}
The Optical Communications and Sensor Demonstration (OCSD) project, managed by NASA with payloads built by The Aerospace Corporation, addresses two cross-cutting capabilities of value to many future small spacecraft missions: high-speed optical transmission of data and small spacecraft proximity operations. Optical data rates demonstrated by OCSD are expected to be 200 megabits per second (Mb/s) or higher, a factor of 100 increase over current high-end CubeSat communications systems. [http://www.nasa.gov/sites/default/files/atoms/files/ocsd_fact_sheet_21oct2015.pdf]
 
 
The optical communications system on OCSD differs from other space-based laser communication systems because the laser is hard-mounted to the spacecraft body. The beam is pointed by controlling the orientation of the entire spacecraft. This makes the laser system much more compact than anything previously flown in space. The attitude control system developed for these satellites includes a pair of miniature star trackers, devices that measure the position of stars for navigational purposes. These star trackers were designed to enable pointing to an accuracy of 0.05 degrees, which is 20 times the precision previously demonstrated in a satellite of this size.
 
 
====OCSD-1====
 
 
OCSD-1 was launched on October 8, 2015. OCSD-1 was the first of three planned satellites, carrying a 6W fiber laser with a 0.7° divergence half angle designed to downlink with a 30 cm ground telescope. This was later enlarged to 80 cm. [https://directory.eoportal.org/web/eoportal/satellite-missions/a/aerocube-ocsd] Projected data rates from OCSD-1 range from 5 to 100 Mbits/s. On October 30, 2015, NASA acknowledged that the Attitude Determination and Control System ([https://en.wikipedia.org/wiki/Attitude_control ADCS]) onboard the satellite is not functioning properly, preventing a test of the satellite's optical communications systems.[http://www.nasa.gov/feature/ocsd] OCSD-1 does not contain any fine beam steering systems, relying wholly on the ADCS for optical alignment. The stated minimum ADCS precision for basic link function is 0.15°; NASA and The Aerospace Corporation has claimed the optical link could achieve data rates above 1 Gbit/s with an higher precision ADCS.
 
 
====OCSD-2(A/B)====
 
 
{{satellite
 
{{satellite
 
| header = OCSD-2 (AeroCube 7B/C)
 
| header = OCSD-2 (AeroCube 7B/C)
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| size = 2 x 1.5U
 
| size = 2 x 1.5U
 
}}
 
}}
 +
===Optical Communications and Sensor Demonstration (OCSD)===
 +
 +
The Optical Communications and Sensor Demonstration (OCSD) project, managed by NASA with payloads built by The Aerospace Corporation, addresses two cross-cutting capabilities of value to many future small spacecraft missions: high-speed optical transmission of data and small spacecraft proximity operations. Optical data rates demonstrated by OCSD are expected to be 200 megabits per second (Mb/s) or higher, a factor of 100 increase over current high-end CubeSat communications systems. [http://www.nasa.gov/sites/default/files/atoms/files/ocsd_fact_sheet_21oct2015.pdf]
 +
 +
The optical communications system on OCSD differs from other space-based laser communication systems because the laser is hard-mounted to the spacecraft body. The beam is pointed by controlling the orientation of the entire spacecraft. This makes the laser system much more compact than anything previously flown in space. The attitude control system developed for these satellites includes a pair of miniature star trackers, devices that measure the position of stars for navigational purposes. These star trackers were designed to enable pointing to an accuracy of 0.05 degrees, which is 20 times the precision previously demonstrated in a satellite of this size.
 +
 +
====OCSD-1====
 +
 +
OCSD-1 was launched on October 8, 2015. OCSD-1 was the first of three planned satellites, carrying a 6W fiber laser with a 0.7° divergence half angle designed to downlink with a 30 cm ground telescope. This was later enlarged to 80 cm. [https://directory.eoportal.org/web/eoportal/satellite-missions/a/aerocube-ocsd] Projected data rates from OCSD-1 range from 5 to 100 Mbits/s. On October 30, 2015, NASA acknowledged that the Attitude Determination and Control System ([https://en.wikipedia.org/wiki/Attitude_control ADCS]) onboard the satellite is not functioning properly, preventing a test of the satellite's optical communications systems.[http://www.nasa.gov/feature/ocsd] OCSD-1 does not contain any fine beam steering systems, relying wholly on the ADCS for optical alignment. The stated minimum ADCS precision for basic link function is 0.15°; NASA and The Aerospace Corporation has claimed the optical link could achieve data rates above 1 Gbit/s with an higher precision ADCS.
 +
 +
====OCSD-2(A/B)====
 +
 
OCSD-2 is scheduled for launch during 2016 aboard a currently unidentified Falcon 9 launch from Vandenberg AFB. The first such launch is currently scheduled for July. OCSD-2 contains the remaining two of the three planned satellites, which will launch as a single 3U unit and separate into 2 independent satellites. The OCSD-2 A and B payloads will attempt satellite-earth and satellite-satellite communications at speeds in excess of 500 Mbit/s, with the primary purpose of demonstrating technologies for satellites operating in proximity to each other. It is unclear what systems will differ between the OCSD-1 and OCSD-2 payloads.
 
OCSD-2 is scheduled for launch during 2016 aboard a currently unidentified Falcon 9 launch from Vandenberg AFB. The first such launch is currently scheduled for July. OCSD-2 contains the remaining two of the three planned satellites, which will launch as a single 3U unit and separate into 2 independent satellites. The OCSD-2 A and B payloads will attempt satellite-earth and satellite-satellite communications at speeds in excess of 500 Mbit/s, with the primary purpose of demonstrating technologies for satellites operating in proximity to each other. It is unclear what systems will differ between the OCSD-1 and OCSD-2 payloads.
  

Revision as of 22:18, 17 March 2016

MIT Lincoln Labs LLCD/LADEE

JPL 1U Optical Comms Terminal

NASASmall Satellites Technology Project

OCSD-1 (AeroCube 7A)
OCSD1.jpg
Organization NASA, The Aerospace Corporation
Launch provider ULA - Atlas V
Launch date October 8, 2015
Launch site Vandenberg AFB
Orbit LEO 1000 x 1200 km x 63.4°
Size 1.5U


OCSD-2 (AeroCube 7B/C)
OCSD2.jpg
Organization NASA, The Aerospace Corporation
Launch provider SpaceX - Falcon 9
Launch date July 2016 (projected)
Launch site Vandenberg AFB
Orbit Unknown
Size 2 x 1.5U

Optical Communications and Sensor Demonstration (OCSD)

The Optical Communications and Sensor Demonstration (OCSD) project, managed by NASA with payloads built by The Aerospace Corporation, addresses two cross-cutting capabilities of value to many future small spacecraft missions: high-speed optical transmission of data and small spacecraft proximity operations. Optical data rates demonstrated by OCSD are expected to be 200 megabits per second (Mb/s) or higher, a factor of 100 increase over current high-end CubeSat communications systems. [1]

The optical communications system on OCSD differs from other space-based laser communication systems because the laser is hard-mounted to the spacecraft body. The beam is pointed by controlling the orientation of the entire spacecraft. This makes the laser system much more compact than anything previously flown in space. The attitude control system developed for these satellites includes a pair of miniature star trackers, devices that measure the position of stars for navigational purposes. These star trackers were designed to enable pointing to an accuracy of 0.05 degrees, which is 20 times the precision previously demonstrated in a satellite of this size.

OCSD-1

OCSD-1 was launched on October 8, 2015. OCSD-1 was the first of three planned satellites, carrying a 6W fiber laser with a 0.7° divergence half angle designed to downlink with a 30 cm ground telescope. This was later enlarged to 80 cm. [2] Projected data rates from OCSD-1 range from 5 to 100 Mbits/s. On October 30, 2015, NASA acknowledged that the Attitude Determination and Control System (ADCS) onboard the satellite is not functioning properly, preventing a test of the satellite's optical communications systems.[3] OCSD-1 does not contain any fine beam steering systems, relying wholly on the ADCS for optical alignment. The stated minimum ADCS precision for basic link function is 0.15°; NASA and The Aerospace Corporation has claimed the optical link could achieve data rates above 1 Gbit/s with an higher precision ADCS.

OCSD-2(A/B)

OCSD-2 is scheduled for launch during 2016 aboard a currently unidentified Falcon 9 launch from Vandenberg AFB. The first such launch is currently scheduled for July. OCSD-2 contains the remaining two of the three planned satellites, which will launch as a single 3U unit and separate into 2 independent satellites. The OCSD-2 A and B payloads will attempt satellite-earth and satellite-satellite communications at speeds in excess of 500 Mbit/s, with the primary purpose of demonstrating technologies for satellites operating in proximity to each other. It is unclear what systems will differ between the OCSD-1 and OCSD-2 payloads.

Space Optical Communications Using Laser Beam Amplification (SOCLBA)

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