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M. S. Ramaiah School of Advanced Studies 1
M. Sc. (Engg.) in Electronics System Design
Engineering
GREESHMA SCWB0913004 , FT-2013
10th Module Presentation
Module code : ESE2516
Module name : Electronic System Design &
Development
Module leader : Mr. Ugra Mohan
Presentation on : 15/09/2014
Task Clarification of Pico and NanoSatellites
M. S. Ramaiah School of Advanced Studies 2
Contents
o INTRODUCTION
o PROBLEM DEFINITION
o TASK SPECIFICATION
o DETAILS
o AEROSPACE INVENTION
o CONCLUSION
o REFERENCE
M. S. Ramaiah School of Advanced Studies 3
Introduction
Fig 1 Satellite in Earth Orbit Fig 2 PICOSat
M. S. Ramaiah School of Advanced Studies 4
Problem Definition [1]
M. S. Ramaiah School of Advanced Studies 5
Task Specification [2]
M. S. Ramaiah School of Advanced Studies 6
Details [2]
Orbit Sun Synchronous Polar Orbit, 500-850 Km
Mass 3Kg
Structure 10 cm x 10 cm x 32 cm
Imaging (Payload) Near IR range (700-850 nm), GSD - 138.6 m , Focal
length - 50 mm
GPS (Payload) Position Accuracy ~20 m , 12 ch, Patch Antenna
IMU (Payload) Analog Device ADXL Accelerometer, 3 axis Gyros, 24 bit
ADC
On board Computer 1. MSP 430(16 MHz) processor, 8KB RAM and 128 KB
Flash
2. ARM 7 core 64 KB RAM 512 flash
Data Storage Triple modular redundancy memory, SD card 2 GB
Attitude Determination and Control
System
3 axis Magnetometer, 3 axis MEMS Gyro, Reaction wheel,
Magnetorques
Power System Li-ion Batteries, Average power 3 Watts
Communication Data Downlink : 430-440 MHz, 9600 bps, Data Uplink :
144-146 MHz, 1200 bps, Beacon Downlink: 430-440 MHz
Ground Station GUI interface in Lab VIEW, rotary system
Thermal Control System Passive System, Thermal Grease, Surface Coatings
M. S. Ramaiah School of Advanced Studies 7
Aerospace Invention [1]
M. S. Ramaiah School of Advanced Studies 8
Conclusion
Components are designed to serve specific task. It is accomplished by this pico and nano
satellites task clarification process. Problem Definition defined with output as a specification
Convergent thinking is done during Task Clarification.
M. S. Ramaiah School of Advanced Studies 9
Reference
1. Jordi Puig-Suari (2011). Sun Oriented and Powered, 3 Axis and Spin Stabilized
Cubesats. Korea: CALPOLY University. 1-11.
2. Fuat lnce (2003). A Role for Cubesats in Responsive Space. Illinios: Marmara
University arid TuAP Academy. 1-19.
M. S. Ramaiah School of Advanced Studies 10
Thank You