ukube-1: a multi-payload technology demonstration...

18
25 April 2011 © Clyde Space Ltd 2010 UKube-1: A Multi-Payload Technology Demonstration Platform Ritchie Logan, Steve Greenland, Clyde Space Ltd

Upload: lethuy

Post on 16-May-2018

214 views

Category:

Documents


0 download

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

Platform OverviewS-band Patch Antenna

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

25 April 2011 © Clyde Space Ltd 2010

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

25 April 2011 © Clyde Space Ltd 2010

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.

25 April 2011 © Clyde Space Ltd 2010

www.clyde-space.com

Questions?

facebook.com/clydespacetwitter.com/clydespace