Low Voltage Power Supply & Power Controller Board

Slides:



Advertisements
Similar presentations
Greg Beau SerajAnanya. Outline  Project overview  Project-specific success criteria  Block diagram  Component selection rationale  Packaging design.
Advertisements

555 Timer ©Paul Godin Updated February Oscillators ◊We have looked at simple oscillator designs using an inverter, and had a brief look at crystal.
Understanding Power Supply Basics and Terminology
GoetzFIELDS iPDR – I&T SPP/FIELDS Integration and Test Preliminary Design Review Keith Goetz University of Minnesota 1.
Selda HeavnerFIELDS iPDR – Antenna Electronics Board Solar Probe Plus FIELDS Instrument PDR Antenna Electronics Board Selda S. Heavner U.C. Berkeley
MonsonPeer Review – 24 October 2013 SPP/FIELDS LNPS PEER REVIEW Steven Monson University of Minnesota 1.
THEMIS-SCM THM – SCM – CDR – 08-April-2004 in Velizy
DESIGN OF THE NEPTUNE NODE CONVERTER Vatché Vorpérian Jet Propulsion Laboratory.
MonsonPeer Review – 5 December 2014 SPP/FIELDS LNPS PEER REVIEW Steven Monson University of Minnesota 1.
D. GordonFIELDS iCDR – DCB Solar Probe Plus FIELDS Instrument CDR DCB Dorothy Gordon Space Sciences Lab, UC Berkeley 1.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW I-PER 21 January EFW Test Plan Michael Ludlam Space Sciences Laboratory.
1 Dec SPP-Fields Antenna Electronics Board (AEB) Concept Status Report J.W.Bonnell, S. Harris, S. Heavner Space Sciences Laboratory UC Berkeley.
GLAST LAT ProjectDelta PDR/Baseline Review July 29-August 1, 2002 Section 7.3 AntiCoincidnce Detector Technical Status 1 GLAST Large Area Telescope: AntiCoincidence.
THEMIS Mission PDR/CAR 1 UCB, November 12-14, 2003 Search Coil Magnetometer (SCM) Mission PDR/CAR Alain Roux CETP-Velizy Co-i: O.Le Contel Technical Manager:
THEMIS Instrument CDR 1 UCB, April 19-20, 2004 Boom Electronics Board (BEB) Engineering Peer Review Apr. 20, 2004 Hilary Richard.
N A S A G O D D A R D S P A C E F L I G H T C E N T E R I n t e g r a t e d D e s i g n C a p a b i l i t y / I n s t r u m e n t S y n t h e s i s & A.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW Boom PER 30 June RBSP EFW Spin Plane Booms Greg Dalton Space Sciences.
THEMIS Instrument CDR 1 UCB, April 19-20, 2004 Boom Electronics Board (BEB) Engineering Peer Review Apr. 20, 2004 Hilary Richard.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes 3-4 Sept. 2008EFW INST+SOC PDR217 RBSP Electric Field and Waves Instrument (EFW) Instrument.
Sept. 2008EFW INST+SOC PDR IDPU Chassis Mechanical Design and Development Bill Donakowski Mechanical Engineer UCB/SSL
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW I-PER 21 January EFW Overview and Status Keith Goetz University of Minnesota.
MonsonFIELDS iPDR – LNPS SPP/FIELDS Low Noise Power Supply Preliminary Design Review Steve Monson University of Minnesota 1.
THEMIS SUITE PRE-ENVIRONMENTAL REVIEW 1 UCB May 2, 2005 THEMIS Pre-Environmental Review Instrument Verification Overview Ellen Taylor University of California.
SDR 7 Jun Associated Electronics Package (AEP) Curtis Ingraham.
THEMIS IDPU PDR I&T REQUIREMENTS- 1 UCB, October 16, 2003 I&T REQUIREMENTS Ellen Taylor University of California - Berkeley.
THEMIS INSTRUMENT CDR Peer ReviewSYSTEM- 1 UCB, April 19, 2004 TITLE: Test Flow RFA CODE: UCB-10 REQUESTED BY: Preble SPECIFIC REQUEST: We recommend that.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW CDR /30-10/1 213 Low Voltage Power Supply & Power Controller Board Peter.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes LVPS+PCB Peter BergRBSP/EFW CDR /30-10/1 IDPU LVPS AND PCB Critical Design Review.
A complete DC/DC converter ASIC for LHC upgrades S. Michelis, F. Faccio, G. Blanchot, I. Troyano CERN PH-ESE S.Saggini University of Udine, Italy Twepp.
NameFIELDS iPDR – Subject Solar Probe Plus FIELDS Instrument PDR Antenna Electronics Box Selda S. Heavner U.C. Berkeley 1.
THEMIS MISSION PDRINSTRUMENT OVERVIEW- 1 UCB, November, 2003 THEMIS INSTRUMENT PAYLOAD SYSTEM OVERVIEW Dr. Ellen Taylor University of California - Berkeley.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes 3-4 Sept. 2008EFW INST+SOC PDR447 Command, Telemetry, and Ground Support Equipment (CTG)
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW I-PER 21 January EFW Instrument Testing to Date Michael Ludlam for EFW.
109-IDPU-Chassis-Donakowski 1 30 Sep – 01 Oct 2009DRAFT RBSP EFW ICDR 109-IDPU-Chassis-Donakowski IDPU Chassis Mechanical Design and Development Bill Donakowski.
THEMIS Instrument CDR 1 UCB, April 19-20, 2004 EFI Preamp Sensor G.T. Delory, A. Hull, D. Schickele, J. Bonnell & The EFI Team University of California.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW CDR /30-10/1 535 IDPU Chassis Bill Donakowski Mechanical Engineer UCB/SSL.
STEREO IMPACT Critical Design Review 2002 November 20,21,22 P.Berg1 STEREO IMPACT POWER SUPPLIES Peter Berg, UC Berkeley Space Sciences Lab,
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW CDR /30-10/1 Thermal Design Christopher Smith RBSP Thermal Engineer Space.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW I-PER 21 January EFW Systems Engineering Michael Ludlam Space Sciences.
20-1 MAVEN iPSR Oct 30-31, 2012 Particles and Fields Package Pre-Ship Review October 30-31, PFDPU D. Gordon, W. Donakowski & PFDPU Team Mars.
Power Electronics and Switch Mode Power Supply
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes Sept 30 – Oct RBSP EFW ICDR1 Integration and Test Michael Ludlam (EFW Systems Engineer)
Status 1 5/07/08 UCB RBSP EFW STATUS 5/07/08. Status 2 5/07/08 UCB Agenda Project Stuff Monthly Report Submitted Schedule Submitted  Milestones Upcoming.
TITLE: 555 Timer OM INSTITUTE OF TECHNOLOGY Subject: Analog Electronics ( ) Semester: 03 Prepared By:
THEMIS IDPU PDRPCB- 1 UCB, October 16, 2003 IDPU Power Control Board (PCB) Peter Berg University of California - Berkeley.
BonnellFIELDS iCDR – AEB Solar Probe Plus FIELDS Instrument CDR Antenna Electronics Board AEB J. Bonnell, D. Seitz UC Berkeley, SSL
Power Philip Luers NASA/GSFC Code 561 August 16-17, 2005.
FIELDS MEP Thermal Vacuum Cycling iPER
Particles and Fields Package (PFP) SWEA Pre-CDR Peer Review
Acronyms 3-4 Sept DRAFT EFW INST+SOC PDR 483
FGM CDR FGM Electronics (FGE) Ronald Kroth MAGSON GmbH Berlin Germany.
EFW Instrument Testing to date
INSTRUMENT DATA PROCESSING UNIT (IDPU) REQUIREMENTS
Calorimeter Mu2e Development electronics Front-end Review
Bill Donakowski Mechanical Engineer UCB/SSL
INSTRUMENT DATA PROCESSING UNIT (IDPU)
(EFW Systems Engineer) University of California, Berkeley
Block Diagram Transmitter Receiver × 2 Transmitter Power Supply ADC
Electric Field and Waves Instrument (EFW)
Instrument Data Processing Unit (IDPU)
Mars Atmosphere and Volatile EvolutioN (MAVEN) Mission
Solar Probe Plus – FIELDS Verification Instrument mini-PER (V5)
Boom Electronics Board (BEB) EFW-EMFISIS E-Field I/F (EFW-EMF)
Boom Electronics Board (BEB)
Preliminary Design Review
Radiation Belt Storm Probes Electric Field and Waves Instrument
THEMIS FM4/FM5 INSTRUMENT SUITE
University of California, Berkeley
CRaTER Pre-Environmental Review (I-PER) Engineering Requirements/Design Updates Bob Goeke September 10-11, 2008.
SMPS POWER PLANT SMR 48V/25A SALIENT FEATURES
Presentation transcript:

Low Voltage Power Supply & Power Controller Board Peter Berg University of California - Berkeley

Overview Overview Requirements Specification Design Mass and Power Test Schedule Issues

Overview CHANGES SINCE PDR FREQUENCY OF PWM SUPPLIES CHANGED TO 200KHZ ACCOMODATION FOR MSK INRUSH CURRENT

Design Drivers SUPPLY DESIGNED TO RBSP_EFW_LVPS_001 INPUT IS 28 VOLT POWER (22-35 VOLTS NOMINAL) PRIMARIES ARE CURRENT LIMITED SUPPLIES SYNCHRONIZED TO 799KHZ FLOATING SUPLIES RUN AT 399.5KHZ, OTHERS AT 199.75KHZ SUPPLY IS SOFT STARTED TO MINIMIZE TURN-ON STRESSES – INPUT CURRENT CONTROLLED REGULATION – 1% ON DIRECTLY REGULATED VOLTAGES AND 5% ON AUXILLARY VOLTAGES ISOLATED SECONDARIES BEB OUTPUTS INDEPENDENT OF IDPU OUTPUTS  225V SUPPLY AND FLOATING  15V SUPPLIES FILTERED TO 14μV RMS 10Hz-10KHz, AND 0.4μV RMS 10KHz-100KHz

Requirement Body or Section Heading Requirements ID Req. Title Subject Priority Requirement Body or Section Heading Implementation EFW-61 EFW Power Control Each EFW IDPU shall contain circuitry to open SPB and AXB doors and deploy sensors Implemented on PCB portion EFW-62 EFW Low Voltage Conversion contain circuitry to provide voltages to IDPU boards using the S/C-provided 28Volts Impemented using PWM converters EFW-63 EFW Main Power Allocation Each EFW Suite not exceed the total power of 11.16 W from the EFW Main 28V Service Verified on Flight Unit EFW-64 EFW Main Power In-Rush Each IDPU not exceed ICD values as follows: 10A for 100 usec; 5A for 100us to 1ms 2.5A after 1ms Implemented using soft start EFW-65 EFW Main Power Max Voltage tolerate without damage a maximum input voltage of 40V indefinitely as defined in the ICD Parts sufficiently derated EFW-75 EFW IDPU Operational Temp Range The EFW IDPU perform as designed from -25 to +55C Parts chosen are -55 to 125C EFW-78 EFW IDPU Survival Temp Range survive without damage from -30 to +60C EFW-88 EFW IDPU ICD Compliance comply with the requirements and constraints imposed by all relevant instrument-to-spacecraft interface control documents (ICDs). Verified by Instrument CPT EFW-98 EFW Illegal Power States not be damaged by the application of boom power while the Main power is Off. By design, verified by test EFW-99 EFW SPB Deployment Enable not deploy SPB booms or fire SPB actuators without the SPB and Main power ON.

Requirements EFW-100 EFW AXB Deployment Enable The EFW IDPU shall not deploy AXB booms or fire AXB actuators without the AXB and Main power ON. By design, verified by test EFW-101 EFW Boom Pair Redundancy have separate supplies for each preamp boom axis. By design EFW-102 EFW Safing by subsystem continue to provide EMFISIS with E-Field signals on failure of DCB or DFB EFW-131 EFW Initial Power On/Reset State power up in a nominal condition for measuring E-Fields without processor intervention. EFW-133 EFW Compliance with EM Environment Control Plan The EFW Suite comply with the requirements and constraints imposed by the RBSP Electromagnetic Environment Control Plan, APL document no. 7417-9018. Verified by Instrument CPT and EMC test EFW-136 Instrument Compliance with Environmental Design and Test Requirements Document Each EFW Instrument comply with the requirements and constraints imposed by the RBSP Environmental Design and Test Requirements Document, APL document no. 7417-9019. Verified as per RBSP_EFW_TE_001 EFW-137 EFW Quality Assurance comply with the RBSP Performance Assurance Implementation Plan, as modified by the Compliance Matrix Verified as per RBSP_EFW_PA_010

Specifications Electro-Mechanical Specifications Connectors ENCLOSURE KA80.1/127CPFC10TABH Mate/Demate Cycles >500 Allows use of commercial backplanes for testing Front Panel 9 Pin Male, 62 Pin Female ENCLOSURE Spacing is .75” above, .25” below Electrically shielded

Design

Design Packaging

Design

Design Design Considerations Grounds Voltage Capabilities 2 Digital 2 Analog 6 Floating Voltage Capabilities Worst Case Floating Voltages  240V Primary to Secondary Isolation >1000V Current Capabilities Worst Case Current Req – Actuators @ 2.25A Pin Capabilities – SDD Series: 5 amps nominal

Design SAMPLE PWM REGULATOR TO FLOATING SUPPLIES

Design MKS INRUSH MITIGATION MSK INRUSH MITIGATION TIMER

Design DUAL  FLOATING SUPPLY

Floating Supply Testing Design Floating Supply Testing

Design Power Control Section BYTE 1 MHZ LATCHES CMD CLEARS DECODERS WITH POWER ON Power Control Section

Design INPUT (FRONT PANEL) POWER SECTION (BACKPLANE) POWER CONTROL SECTION (FRONT PANEL)

Mass & Power Mass Power 824 Grams CBE (BOARD WITH FRONT PANEL) Shielding Mass held by IDPU Chassis Growth/Uncertainty Margin is 5% Power

TEST Sample Tester

STATUS WORKING SUPPLY TESTED WITH IDPU TESTED WITH EMFISIS FLOATER EFFICIENCY 80% OVERALL EFFICIENCY IS ~50% VERIFIED 1% REGULATION

INRUSH TEST Inrush Profile

SCHEDULE TASK COMPLETION DATE TEST PCB PORTION OF LVPS SEPT 30 NEW ETU LAYOUT RECEIVED OCT 2 EFFICIENCY BUILD NEW ETU OCT 23 SYNC SEQUENCE OCT 27 LINE REGULATION OCT 30 LOAD REGULATION CROSS REGULATION MSK INRUSH DEFEAT CIRCUIT RIPPLE MEASUREMENTS CURRENT TRIP THRESHOLDS NOV 6 MONITOR GAINS CONDUCTED EMISSIONS THERMAL TEST NOV 13 FLIGHT LAYOUT NOV 27 BUILD FIRST FLIGHT UNIT DEC 15 TEST FIRST FLIGHT UNIT JAN 8

PEER REVIEW RFAs TITLE DESCRIPTION RESPONSE Stress Analysis Ensure stress analysis done on all boards by CDR Parts chosen at design to accommodate stress margins PCB Switch Dissipation Look at thermal dissipation of FET switches on PCB, is heat sinking necessary? No additional heat sinking is necessary. Two of the higher dissipation FETS have new part numbers and the temp rise of the highest is less than 3°C. LVPS Thermal Vacuum Test Check hot and cold operation of LVPS in Thermal Vacuum, in particular sync operation, soft start, in rush times, 1526 startup, floater and 225 supply outputs. Verify at hot that parts do not exceed rated temperatures. Post CDR on complete ETU Measure LVPS Efficiency Measure efficiency of all supplies Total efficiency of supplies is presently ~ 50% Measure LVPS Cross Regulation Verify that cross regulation of supplies meets 5% goal Will test asap, perhaps on new ETU (post CDR) LVPS Free-run Frequency Verify that free run frequency of 1526 does not go above 90% of sync frequency Currently, set point is 95% of sync frequency. LVPS Soft start capacitors Include soft start capacitors in schematics Will be included where needed Implement temporary current limiting on IDPU supply Allow high inrush on the IDPU supply, but safe instrument in case of short To be implemented with timed increase of overcurrent threshold on new ETU (post CDR).

Issues CONSUMPTION NOISE Improve efficiency Reduce amplitude of tone at 200 kHz