ukube-1: a multi-payload technology demonstration...
TRANSCRIPT
25 April 2011 © Clyde Space Ltd 2010
UKube-1: A Multi-Payload Technology Demonstration Platform Ritchie Logan, Steve Greenland, Clyde Space Ltd
25 April 2011 © Clyde Space Ltd 2010
Outline
1. Timeline and functional overview2. Payload Details & Management3. Enabling Rapid Development and AIT4. Conclusions
25 April 2011 © Clyde Space Ltd 2010
UKube-1United Kingdom Universal Bus Experiment
• Artist’s impression
25 April 2011 © Clyde Space Ltd 2010
Mission Objectives
• Ukube-1 shall demonstrate:– new UK space technology– the capability of useful science to be performed within a
CubeSat sized spacecraft– industry and university based training in spacecraft
development– education and outreach in STEM subjects– Payload Kick-Off to flight qualified spacecraft in less than 12
months
25 April 2011 © Clyde Space Ltd 2010
Mission Team
Platform prime
S-Band Transmitter
Project Management, Technical review
Platform support
FUNCube
MissionComputer
Partnership Majority of effort is self-funded
Exciting “coalition of the willing”
25 April 2011 © Clyde Space Ltd 2010
Timeline
18 months to design and build a 3U CubeSat
July 2010•Official announcement by Science Minister at Farnborough
July 2010•Platform Kickoff in Clyde Space
Nov 2010•Official AO for payloads•22 Responses
Jan 2011•7 Payloads selected
Mar 2011•4 Payloads Downselectedfor flight
Summer 2011•Platform and payload AIVT
Dec 2011•Launch
Design and deliver Interface Emulator
25 April 2011 © Clyde Space Ltd 2010
Additional FUNCube Payload
• FUNCube Transceiver provides– Provides a full-duplex transceiver for the platform (secondary
transceiver for very low data rate communications)– Provides education & outreach objectives and infrastructure, with the
aim to integrate with UKSA outreach and the UKube program beyond this pilot with existing AMSAT experience
– Provides a pre-made payload for leading the platform-payload integration effort
– Provides and supports the amateur radio community in response to their support in frequency allocation
– Harnesses the experience of professionalamateurs into the UKube program
– Provides redundancy for the FUNcube spacecraft
25 April 2011 © Clyde Space Ltd 2010
4x Payloads now selected
• Astrium Janus– Cosmic Radiation random
number generator– Techdemo for effects of
radiation on Xilinx FPGA
• Open University Imager– Take high quality images– Techdemo of a European
CMOS imager using 0.18u process
• Univ of Bath TOPCAT– Dual freq COTS GPS– Techdemo of GPS for
measurement of space weather in plasmasphere
• UKSEDS MyPocketQub– Miniature platform for up
to 365 additional experiments
– Techdemo of OS s/craft
25 April 2011 © Clyde Space Ltd 2010
Payload Management
• From early in the program, we knew that the payloads would be provided via an open competition
• Platform and payload development would need to happen concurrently
• Physical envelope was fairly easy• Power and data more difficult
Interface Emulator
25 April 2011 © Clyde Space Ltd 2010
Interface Emulator
• Out of box solution for payload providers allowing rapid development
• Emulates mechanical and electrical interfaces• Multiple emulators enable multiple payloads
– Concurrent development of payloads– Concurrent development of platform
• Minimise integration time between platform and payload
25 April 2011 © Clyde Space Ltd 2010
Interface Emulator
• 2x Arduino uP boards• 4x power switches• Full mechanical
interface• Payload I2C and Comms
SPI
Power Switches
Power Sources
Payload Arduino
Payload Header
Data Header
Routing Blocks
USB
CSK PC/104 Header
CSK PC/104 Standoff
I2C
Payload IO (30)
12V
5V
3.3V
GND
(10)
(4)
(4)
(4)
Platform Arduino USB
Arduino Dock
Level Translator
I2C Block
Comms SPI BATV (4)
(2)
BATV 12V 5V 3.3V
Switching
Synch Pulse
25 April 2011 © Clyde Space Ltd 2010
Working with CSK (PC/104)
The dilemma• Wide variety of COTS
subsystems– Cost & availability benefits
• PC/104 is not ideal during subsystem development and AIVT
• Debugging of new subsystems very difficult
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CSK Format Flatsat
6x PC/104Board docks
1x invertedBoard dock
InterfaceBoard dock
ExtensionConnectors
104 LEDs and 104 Test points
25 April 2011 © Clyde Space Ltd 2010
Interface Board
• Primary interface for test equipment and computer
• Power interface for CubeSat
• Simulation of sep switch/pull pin on CubeSat structure– Both Pumpkin and Isis
format
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Aiding Rapid Development
• Using flatsat to aid debugging of UKubesystems
• Plan to make some (small) changes– Supports– PCB thickness?
• Expect to have ready for wider use early Q2
25 April 2011 © Clyde Space Ltd 2010
Conclusions
• Novel technical approaches (hardware and software emulators) facilitate community based engineering projects
• CubeSats present an excellent opportunity as a low cost tech demo platform
• When government funds become available, act quickly to secure! COTS + rapid development of subsystems allows this to happen
• UKube1 is envisaged as the pilot for a full national Cubesatprogramme supported by Government, industry and academia.
• Announcement on the pilot will hopefully be made in the summer, UK Space Agency budget negotiations permitting.