TRIO-CINEMA 1 UCB, 2/08/2010 ClydeSpace Electronic Power System Yashraj Khaitan Space Sciences Laboratory University of California, Berkeley.

Slides:



Advertisements
Similar presentations
Controller Tests Stephen Kaye Controller Test Motivation Testing the controller before the next generation helps to shake out any remaining.
Advertisements

Solar Array & Maximum Power Point Tracker Group Senior Design Project 2003 Stephanie Chin Jeanell Gadson Katie Nordstrom Advisor: Karen Panetta.
Genasun LLC MPPT Solar Charge Controllers and Lithium Batteries Alex MeVay.
Team: – Brad Jensen – Will Klema – Nate Schares Client: – PowerFilm, Inc. Advisor: – Dr. Ayman Fayed Solar-Powered Mobile Power Station (MPS)
ECE480 Team 8: Maximum Power Point Tracker Daniel Chen Yue Guo Luis Kalaff Jacob Mills Brenton Sirowatka.
Introduction Since the beginning of the oil crises, which remarkably influenced power development programs all over the world, massive technological and.
University of Kansas EPS of KUTEsat Pathfinder Leon S. Searl April 5, 2006 AE256 Satellite Electrical Power Systems.
Introduction to Space Systems and Spacecraft Design Space Systems Design Power Systems Design -I.
ECE 442 Power Electronics1 Step Up Converter Close the switch to store energy in the inductor L Open the switch to transfer the energy stored in L to the.
CR1000s are only one part of a data acquisition system. To get good data, suitable sensors and a reliable data retrieval method are required. A failure.
Chapter 8 Inverters AC Power • Inverters • Power Conditioning Units • Inverter Features and Specifications.
To develop a small scale solar powered system that will power a DC load, which incorporates power management techniques, DC-DC conversion and a user interface.
Abstract The purpose of this project is to build a clean self-sustained photovoltaic energy harvesting system. The system will accept input from multiple,
DC-DC Fundamentals 1.3 Switching Regulator
M OBILE P OWER S TATION A BSTRACT The Mobile Power Station (MPS) is a device that manages and stores solar energy in a lithium ion (Li-ion) battery pack.
Hybrid Wind & Solar Generation Project
LSU 06/04/2007Electronics 51 Power Sources Electronics Unit – Lecture 5 Bench power supply Photovoltaic cells, i.e., solar panel Thermoelectric generator.
AMSAT Fox-1 Overview AMSAT Engineering Team 2011 Space Symposium.
Power Supply Design J.SHANMUGAPRIYAN.
Department of Electronic Engineering 4th Year Electronic & Computer Final Year Project Presentation Supervisor: Dr Maeve Duffy Co- Supervisor: Dr Peter.
Energy Harvesting Thomas Vermeer 3/25/09 Embedded Systems.
KUMU A’O CUBESAT Amy Blas. Background 2 What is CubeSat?  10x10x10 centimeter cube  Launched in lower earth orbit (LEO)  The project started last.
Summer Projects Review: Current Status. ADCS ADCS calibrated in uniform magnetic field using support hardware to mimic the computer onboard the satellite.
Charge Controllers Regulating Battery Charging.
Morehead State University Morehead, KY Prof. Bob Twiggs Power Systems Design
Michael Ikerionwu 4 th year Electronic Engineering.
TRIO-CINEMA 1 UCB, 2/08/2010 Instrument Interface Board Dorothy Gordon CINEMA - EE Team Space Sciences Laboratory University of California, Berkeley.
Solar Power Array Management for the Solar Racing Team Mark Calotes Ginah Colón Alemneh Haile Nidhi Joshi Michael Lu School of Electrical and Computer.
EPS/Fault Management Software Jimmy Nguyen Electrical Power Subsystem Member 1.
Packing & Contents Box Size : 40 x 26 x 10 cm (15.8 x 10.2 x 3.9 in) Weight : 3.5 Kg (7.72lb)       W Inverter*1 (110V/220V) 7. Light ouch,
ECE 477 Senior Design Group 12  Spring 2006 Daniel da Silva Atandra Burman Eric Aasen Harsha Vangapaty.
Luigi Schirone professor of Electronics Aerospower Laboratory Managed by:
TRIO-CINEMA 1 UCB, 2/08/2010 Solar Array Kevin Jenkins Mechanical Engineering Space Sciences Laboratory University of California, Berkeley.
TA Station Power Team Meeting, 11/10/2015. Autonomous Power System – In the field Why Lithium? -Significant weight and volume savings (41.9Wh/lb vs 21.25Wh/lb)
Hybrid Power Controller (HPC) Final Presentation Senior Design II.
CUER Electrical System
TRIO-CINEMA 1 UCB, 8/10/2010 CINEMA Project Update Thomas Immel UCB/SSL Space Sciences Laboratory University of California, Berkeley.
Component Selection and PCB Fabrication Supervisor: Dr. Peter Driessen Presenter: Justin Curran.
TRIO-CINEMA 1 UCB, 2/08/2010 CINEMA Solar Array Design Review Yashraj Khaitan David Glaser Kevin Jenkins Chris Pasma Space Sciences Laboratory University.
1 LAPPD Team meeting 6/10/2010 Ossy Siegmund, Experimental Astrophysics Group, Space Sciences Laboratory, U. California at Berkeley Integration of Front-End.
TRIO-CINEMA 1 UCB, 2/08/2010 LVPS & Switching Dave Curtis UCB/SSL Space Sciences Laboratory University of California, Berkeley.
TRIO-CINEMA 1 UCB, 2/08/2010 Integration and Test Program Dave Curtis UCB/SSL Space Sciences Laboratory University of California, Berkeley.
ARISSat-1 Critical Design Review Orlando, Feb 15, 2010 Maximum Peak Power Point Tracker (MPPT) John Charais / Jerry Zdenek
Solar Mobile Charger Name: S.R.Akshay Kumar, RollNo:13L103, Dept of ECE, PSG College of Technology, Coimbatore. 1 PSG College of Technology.
VK-PA-Pico Power Analyzer Picoammeter Mode - Operating Principle to Measure Short Circuit Current (I sc ) of Solar Cell + - Solar Cell To Analog to Digital.
Solar Patio Umbrella Final Presentation May 3 rd, 2016 Team #37 ECE 445 – Spring 2016.
Self-Sustainable Electric Golf Bag Final Presentation Group 19 Jon Kinney, Cory Edwards, Harrison Kantner 30 April 2013.
Abbott Technologies Presents DC To AC Inverters. DC To AC Power Inverters change direct current (DC) to Alternating current (AC).
TRIO-CINEMA 1 UCB, 2/08/2010 System Design Dave Curtis UCB/SSL Space Sciences Laboratory University of California, Berkeley.
SEC598F16 Photovoltaic Systems Engineering Session 12 PV System Components Inverters Balance of Systems (BOS) October 04, 2016.
Solar Energy Generator: Design Rendering Description
Satellite Electrical Power System (EPS) Design Review
EagleSat’s Electronic Power Subsystem
Power Board for IlliniSat-2 Project
Preliminary PCB Design
Flight Software – EPS Module
By: Raed Wa’el Ennab & Raja Sa’ed Anabtawi
SELF-SUSTAINABLE SOLAR STREET LIGHT CHARGING
Day 5: Energy Applications - Energy Conversion and Management Silicon
Development of a MPPT System for Solar Lighting Applications
Graduation Project-II submitted to:
How to avoid catching things on fire.
RV Solar Panel Installation
EagleSat 2 – Electrical Power Subsystem Development
Regulating Battery Charging
Model Output Current Battery Life BATPSU VDC 2A 1.2Ah BATPSU VDC 2.3Ah
Series 5300 Lithium Cell Formation System
Solar Powered Power Bank
Presentation transcript:

TRIO-CINEMA 1 UCB, 2/08/2010 ClydeSpace Electronic Power System Yashraj Khaitan Space Sciences Laboratory University of California, Berkeley

TRIO-CINEMA 2 UCB, 2/08/2010 ClydeSpace EPS Agenda AGENDA Requirements Overview Alternatives Features Testing

TRIO-CINEMA 3 UCB, 2/08/2010

TRIO-CINEMA 4 UCB, 2/08/2010 Overview 3 Battery Charge Regulators (BCRs) on 6 solar array sections Independent operation even without battery backup Maximum Power Point Tracking

TRIO-CINEMA 5 UCB, 2/08/2010 Alternatives BCRs could have been designed using switch mode regulator ICs at a much lower cost Efficiencies could have increased by conducting MPPT for each solar array

TRIO-CINEMA 6 UCB, 2/08/2010 Features BCR uses Single Ended Primary Inductor Converter (SEPIC) for high efficiency power conversion 5V and 3.3V regulators use BUCK converters at 90% efficiency Over-current protection switches to protect CUBESAT circuitry Telemetry and Telecommands interface via I2C digital interface 0.1W system quiescent power consumption Peak Power Tracking using the CubeSat EPS Peak Power Tracker Mass = 80g The 32 ADC channels on the board can be used to track the temperature, current and voltage of all solar arrays, buses, and the batteries.

TRIO-CINEMA 7 UCB, 2/08/2010 Testing and Precautions The conversion efficiency of the BCRs can be tested by interfacing to a solar panel, USB connector or a 8V current limited power supply Shorting the batteries to ground while they are connected to the EPS instantly fries the board The charging source should be connected to the batteries only after closing the pull pin connection, else at least one BCR is damaged Each battery pack is composed of 2 Lithium Ion cells. Batteries should be stored within a voltage rating of 6.4V to 7.6V at -4  F to 68  F and charged periodically to prevent permanent damage

TRIO-CINEMA 8 UCB, 2/08/2010 Development Plans Test the board and verify charging efficiencies Familiarize with the board’s firmware to collect working data on performance of batteries, buses, and solar panels Test over-current protection circuitry Test EPS output under a variety of illumination conditions to ensure that worse case 3W output is achieved even under longest shadow conditions

TRIO-CINEMA 9 UCB, 2/08/2010 Thank you