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Spacecraft Technology from Dundee
Steve Parkes
Space Technology Centre, University of Dundee
STAR-Dundee Ltd

Spacecraft images courtesy of ESA

1
Spacecraft onboard data-handling
 Computer network technology for spacecraft
– SpaceWire

 Connects together data-handling elements
onboard a spacecraft:
–
–
–
–

Instruments
Processors
Mass memory
Telemetry and Telecommand

 Standard interface
 Forms the nervous system of a spacecraft

2
3
4
5
6
7
SpaceWire Key Features
 Similar purpose to USB
– Different technology







8

Designed for space applications
Simple
Implementation requires few logic gates
High performance
Flexible architecture
9

Image courtesy NASA
Lunar Reconnaissance Orbiter
DRLE

CRATER

LOLA

NAC
1

NAC
2

WAC

Mini-RF
Radar

LRO Camera (LRCO)
ACS

SpW

LEND

1553B

SpW

HK/IO

SpW
Large
Memory

Command and Data
Handling Computer

SpaceWire Router
SpW
KaCOMMS

10

SpW

S-COMMS

LAMP
11
Image courtesy NASA
12

Image courtesy NASA
13
Plug and Play Sat

Image courtesy AFRL

14
Plug and Play Sat

Image courtesy AFRL

15
16
GAIA

17
18

Image EADS Astrium
19
20
21
22
xx

23

Illustration: Akihiro Ikeshita / JAXA.
Sentinel 3

24
SpaceWire
 SpaceWire standard
– Written by University of Dundee
– With inputs from international spacecraft
engineers

 SpaceWire technology
– Being used or designed into over 100 spacecraft
– Over $15 billion worth of spacecraft rely on it
 Scientific, Exploration, Earth observation, Commercial

 Dundee SpaceWire chip technology
designed into
– European, Japanese, USA, Chinese spacecraft

 Successful spin-out company STAR-Dundee
25
STAR-Dundee Ltd
 Operational for 11 years
 Grown organically
 Winner of Courier
– “Business of the Year” Award 2013
– “Digital Business of the Year” Award 2013

 Winner of two SMART awards
 Customers include
– ESA
– NASA
– JAXA

 Many leading aerospace companies in
26

– USA
– Europe

© STAR-Dundee Ltd 2012
2011
STAR-Dundee
 Products
– SpaceWire test equipment
– SpaceWire chip designs

 High value, low volume
 Responsive to customer
requirements
 Support important

27

© STAR-Dundee Ltd 2012
2011
The Team






18 people
16 FTEs
8 PhDs
Other highly skilled people
Mix of technical skills
–
–
–
–
–
–

28

Chip design
Circuit design
Board design
Box design
Software drivers
Application software

© STAR-Dundee Ltd 2012
2011
29

© STAR-Dundee Ltd 2012
2011
Planetary Landers
 How to land a spacecraft on a distant planet?
–
–
–
–

Without a pilot on board
Long communication delays
Precision landing
In potentially hazardous terrain

 Robotic pilot
 Eyes of robotic pilot
– Computer vision
– Measure spacecraft motion relative to the surface
– Visual information combined with information from
other navigation sensors
– Used to guide the spacecraft
30
Feature Tracking
Image (N)

Image (N+1)
“Landmark”
Tracking

Target
Landing
Site
Eyes for Spacecraft Robotic Pilot
 NPAL Camera Prototype
– Navigation for Planetary Approach and Landing

 Team
– EADS Astrium (France)
– Selex Galileo (Italy)
– University of Dundee
Image Memory
Image
Proc.

Control
Proc.

Imaging
Chip

SpW
To
OBC
Testing Vision Based Navigation
 Having built a lander navigation system
– How can we test it?

 Simulation
– PANGU:
 Planet and Asteroid Natural-scene Generation Utility

– Software tool
 Simulates planets and asteroids
 Simulates cameras and other sensors viewing those
bodies
 Developed specifically to test vision based GNC
algorithms
 Realistic and high performance
 Extensively tested and validated so that it can be used
for testing space flight systems
35

– Being used for lander, rover, orbiter simulation
Descent videos: Malapert Ridge
– Based on a 960 m DEM centred on Malapert
Ridge near the South Pole Model with resolution
varying from 960 m to 47 cm.

36
37
38
39
Landmark Recognition
 Landmarks: sites of prominent Harris corners
 Connected by a surface mesh
 Surface mesh allows tracking of landmarks
– Lying over the asteroid horizon
– and in concave areas

40
Landmark Recognition
 Landmarks are projected into the image
– Using an estimate of the spacecraft position &
orientation

 Matches are made with features in the
current navigation imagery
 Estimated spacecraft position & orientation
optimised
– By minimising the difference between
– Expected and observed landmark position in the
image

41
42
Planetary Landers
 Navigation camera
– Prototype built and tested
– Engineering model currently under development
– Dundee providing image processing chip design

 Test system
– PANGU simulator designed and built at Dundee
– Widely used in Europe for testing vision-based
navigation systems




43

Descent and landing, e.g. Lunar Polar
Asteroid landing, e.g. Marco Polo
Rover navigation, e.g. ExoMars
Spacecraft rendezvous and docking, e.g. Mars Sample
Return
Earth Observation Data Reception
 Dundee Satellite Receiving Station
 One of main receiving stations in UK
 Funded by NERC
– Natural Environment Research Council

 Part of NEODAAS
– NERC Earth Observation Data Acquisition and
Analysis Service
45
User community across UK
 Marine
 Atmospheric
 Earth
 Terrestrial & Freshwater
 Polar
 Earth Observation
48
Haar
Sarahan Dust Over UK
 www.spacetech.dundee.ac.uk
 www.sat.dundee.ac.uk
 www.neodaas.ac.uk
 www.star-dundee.com
 www.rapidqualitysystems.com

52

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Space wire illustrated map

  • 1. Spacecraft Technology from Dundee Steve Parkes Space Technology Centre, University of Dundee STAR-Dundee Ltd Spacecraft images courtesy of ESA 1
  • 2. Spacecraft onboard data-handling  Computer network technology for spacecraft – SpaceWire  Connects together data-handling elements onboard a spacecraft: – – – – Instruments Processors Mass memory Telemetry and Telecommand  Standard interface  Forms the nervous system of a spacecraft 2
  • 3. 3
  • 4. 4
  • 5. 5
  • 6. 6
  • 7. 7
  • 8. SpaceWire Key Features  Similar purpose to USB – Different technology      8 Designed for space applications Simple Implementation requires few logic gates High performance Flexible architecture
  • 10. Lunar Reconnaissance Orbiter DRLE CRATER LOLA NAC 1 NAC 2 WAC Mini-RF Radar LRO Camera (LRCO) ACS SpW LEND 1553B SpW HK/IO SpW Large Memory Command and Data Handling Computer SpaceWire Router SpW KaCOMMS 10 SpW S-COMMS LAMP
  • 13. 13
  • 14. Plug and Play Sat Image courtesy AFRL 14
  • 15. Plug and Play Sat Image courtesy AFRL 15
  • 16. 16
  • 19. 19
  • 20. 20
  • 21. 21
  • 22. 22
  • 25. SpaceWire  SpaceWire standard – Written by University of Dundee – With inputs from international spacecraft engineers  SpaceWire technology – Being used or designed into over 100 spacecraft – Over $15 billion worth of spacecraft rely on it  Scientific, Exploration, Earth observation, Commercial  Dundee SpaceWire chip technology designed into – European, Japanese, USA, Chinese spacecraft  Successful spin-out company STAR-Dundee 25
  • 26. STAR-Dundee Ltd  Operational for 11 years  Grown organically  Winner of Courier – “Business of the Year” Award 2013 – “Digital Business of the Year” Award 2013  Winner of two SMART awards  Customers include – ESA – NASA – JAXA  Many leading aerospace companies in 26 – USA – Europe © STAR-Dundee Ltd 2012 2011
  • 27. STAR-Dundee  Products – SpaceWire test equipment – SpaceWire chip designs  High value, low volume  Responsive to customer requirements  Support important 27 © STAR-Dundee Ltd 2012 2011
  • 28. The Team      18 people 16 FTEs 8 PhDs Other highly skilled people Mix of technical skills – – – – – – 28 Chip design Circuit design Board design Box design Software drivers Application software © STAR-Dundee Ltd 2012 2011
  • 30. Planetary Landers  How to land a spacecraft on a distant planet? – – – – Without a pilot on board Long communication delays Precision landing In potentially hazardous terrain  Robotic pilot  Eyes of robotic pilot – Computer vision – Measure spacecraft motion relative to the surface – Visual information combined with information from other navigation sensors – Used to guide the spacecraft 30
  • 31.
  • 32. Feature Tracking Image (N) Image (N+1) “Landmark” Tracking Target Landing Site
  • 33.
  • 34. Eyes for Spacecraft Robotic Pilot  NPAL Camera Prototype – Navigation for Planetary Approach and Landing  Team – EADS Astrium (France) – Selex Galileo (Italy) – University of Dundee Image Memory Image Proc. Control Proc. Imaging Chip SpW To OBC
  • 35. Testing Vision Based Navigation  Having built a lander navigation system – How can we test it?  Simulation – PANGU:  Planet and Asteroid Natural-scene Generation Utility – Software tool  Simulates planets and asteroids  Simulates cameras and other sensors viewing those bodies  Developed specifically to test vision based GNC algorithms  Realistic and high performance  Extensively tested and validated so that it can be used for testing space flight systems 35 – Being used for lander, rover, orbiter simulation
  • 36. Descent videos: Malapert Ridge – Based on a 960 m DEM centred on Malapert Ridge near the South Pole Model with resolution varying from 960 m to 47 cm. 36
  • 37. 37
  • 38. 38
  • 39. 39
  • 40. Landmark Recognition  Landmarks: sites of prominent Harris corners  Connected by a surface mesh  Surface mesh allows tracking of landmarks – Lying over the asteroid horizon – and in concave areas 40
  • 41. Landmark Recognition  Landmarks are projected into the image – Using an estimate of the spacecraft position & orientation  Matches are made with features in the current navigation imagery  Estimated spacecraft position & orientation optimised – By minimising the difference between – Expected and observed landmark position in the image 41
  • 42. 42
  • 43. Planetary Landers  Navigation camera – Prototype built and tested – Engineering model currently under development – Dundee providing image processing chip design  Test system – PANGU simulator designed and built at Dundee – Widely used in Europe for testing vision-based navigation systems     43 Descent and landing, e.g. Lunar Polar Asteroid landing, e.g. Marco Polo Rover navigation, e.g. ExoMars Spacecraft rendezvous and docking, e.g. Mars Sample Return
  • 44. Earth Observation Data Reception  Dundee Satellite Receiving Station  One of main receiving stations in UK  Funded by NERC – Natural Environment Research Council  Part of NEODAAS – NERC Earth Observation Data Acquisition and Analysis Service
  • 45. 45
  • 46.
  • 47. User community across UK  Marine  Atmospheric  Earth  Terrestrial & Freshwater  Polar  Earth Observation
  • 48. 48
  • 49. Haar
  • 51.
  • 52.  www.spacetech.dundee.ac.uk  www.sat.dundee.ac.uk  www.neodaas.ac.uk  www.star-dundee.com  www.rapidqualitysystems.com 52

Editor's Notes

  1. SpaceWire is a data-handling network technology specifically designed or use onboard spacecraft.It connects together instruments, processors, mass memory and the telemetry/telecommand subsystem.SpaceWire provides a standard interface between all these elements, which simplifies integration and testing of the onboard data-handling system.Instruments and other units designed with SpaceWire interfaces are easy to reuse on other spacecraft,The SpaceWire standard was written by the University of Dundee with input from spacecraft engineers from across Europe.
  2. SpaceWire is attractive for spacecraft designers because it is simple requiring relatively few logic gates to implement and is easy to use in a wide range of applications.It has a high performance providing high-speed, bidirectional communication at up to 200 Mbits/s.SpaceWire sends information in packets.SpaceWire is also extremely flexible, being adaptable to many different data-handling architectures.It has some special features like time-codes which are not present in other networks.
  3. Launched June 2009
  4. View from Surveyor 3 (landed April20,1967) to Apollo 12 Intrepid (landed Nov 19, 1969)I watched this on TV as a 13 year old.40 years later technology that I helped developed was being used to photograph the footsteps of these courageous explorers.It is humbling to think of what engineers in the 60’s achieved with the technology they had at hand.
  5. GAIA:is an ESA star mapping mission with an extremely high resolution CCD.SpaceWire is being used to transfer images from the CCD to the onboard mass memory. SpaceWire was an enabling technology for this mission, with 16 SpaceWire links being used to transfer the data.
  6. GAIA service unit
  7. Bepi Colombo is the joint ESA/JAXA mission to Mercury.SpaceWire is being used for almost all the onboard data handling in both ESA and JAXA spacecraft
  8. James Webb Space Telescope is the big brother of the Hubble Space Telescope. Hubble had a 2.5 m diameter mirror. JWST has a 6.5 m diameter mirror!JWST is a NASA mission with some ESA instruments.SpaceWire used for all the onboard data handling except for one star-tracker.
  9. JWST NIR Camera
  10. The purpose of ASTRO-H is to explore the structure and evolution of Universe with the following observational capabilities:One of the first imaging and spectroscopic observations with the hard X-ray telescope.The first spectroscopic observations with an extremely high energy resolution of the micro-calorimeter.The most sensitive wideband observation over an energy range from 0.3 to 600 keV.Launch 2014 "Illustration: Akihiro Ikeshita / JAXA".
  11. The Sentinel-3 mission's main objective is to measure sea-surface topography, sea- and land-surface temperature and ocean- and land-surface colour with high-end accuracy and reliability in support of ocean forecasting systems, and for environmental and climate monitoring.The first Sentinel-3 satellite is expected to launch in 2013, followed by the second to provide the required level of coverage for GMES services
  12. STAR-Dundee is a spin-out company from the Univesity of Dundee, set up to support users of SpaceWire with an extensive range of SpaceWire evaluation, development and test equipment.SpaceWire related IP is also available.
  13. STAR-Dundee’s team has evolved over the past seven years, starting with a few people working part time, to 17 people now, 14 full-time equivalent staff. There are 7 PhDs and other highly skilled people covering a mix of technical skills. Sales and support are highly technical, but we now have one person responsible for sales, one responsible for the Chinese market, and an Administrator.