Pierre PRAT Progress the 12.10.2012 Michel DUPIEUX.

Slides:



Advertisements
Similar presentations
University of Kansas EPS of KUTEsat Pathfinder Leon S. Searl April 5, 2006 AE256 Satellite Electrical Power Systems.
Advertisements

Connector Board Meets customer need 6. Accept data from auxiliary external cameras and INS units Power Input Regulation Monitoring.
HK & LVPS for EUSO –TA / -Balloon G. Medina-Tanco, L. Santiago, H. Silva Lopez, F. Trillaud, C. Lopez, J. Rojas, A. De la Cruz, S. Guerrero, G. Leon.
- Purpose - Main sequences - Resources (manpower and GSE), including location -Main activities of the assembly and integration of the subsystems -Final.
End of phase A meeting CNES (Toulouse) 2/02/2012 Ph. Gorodetzky APC - Paris Diderot1 High Voltage power supplies HV Switches Design: J. Szabelski, J. Karcmarczyk,
- Grounding - Harness Shielding - PDM Electrical Architecture - DP Electrical Architecture EUSO-BALLOON DESIGN REVIEW, , CNES TOULOUSE Pierre.
EUSO-BALLOON CDR – Agenda (I). Internal interfaces overview Batteries and Low Voltage power Supplies PDM interfaces DP interfaces HK Interfaces List of.
Spring semester (4/2009) High Speed Signal Processing Board Design By: Nir Malka, Lior Rom Instructor: Mike Sumszyk הטכניון - מכון טכנולוגי לישראל הפקולטה.
- Battery Pack Technical Specifications - Battery Pack Design Descriptions - Battery Pack Connection Diagram - Battery Pack Architecture EUSO-BALLOON DESIGN.
EUSO BALLOON Battery Power Pack (PWP) RIKEN/UAH Héctor Prieto, Katsuhiko Tsuno, Marco Casolino.
Upgrade developments in Clermont-Ferrand Romeo Bonnefoy and François Vazeille Tilecal upgrade meeting (CERN, 13 June 2014) ● Handling tools ● Deported.
DESIGN OF THE HATCH OF THE INSTRUMENT BOOTH OF EUSO-BALLOON version v1.2 Writer : SYLVIE DAGORET- CAMPAGNE Final tests and Health tests1
Objectives How Microcontroller works
18-Jan-021W. Karpinski System Test Design verification of petals and interconnect boards and control links without detectors a)mechanics b)electrical.
- Where are the entry points of the instrument - Physical External links - Overview of the External Interfaces - Status - Conclusion EUSO-BALLOON DESIGN.
Selda HeavnerFIELDS iPDR – Antenna Electronics Board Solar Probe Plus FIELDS Instrument PDR Antenna Electronics Board Selda S. Heavner U.C. Berkeley
Electronics for PS and LHC transformers Grzegorz Kasprowicz Supervisor: David Belohrad AB-BDI-PI Technical student report.
MP Electronics 2 1IWF-EXP/ÖAW GRAZ  Power budget  Interface electronics: ~1.5 W  Probe electronics (standby): ~1.2 W  Heater power:~70 W  Power loss.
TE-MPE-EP, VF, 11-Oct-2012 Update on the DQLPU type A design and general progress. TE-MPE Technical Meeting.
Recommendation and actions EUSO EUSO-BALLOON FLIGHT REVIEW, , CNES TOULOUSE Guillaume Prévôt APC, Paris Wrap up previous actions.
Dimensions of the PDM frame: 167mm x 167mm x 28.7mm.
U.B. Presentation October Bernard COURTY L.P.C.C. College de France - Paris.
Main Board Status MB2 v1 for FATALIC & QIE 10/06/2015Roméo BONNEFOY - LPC Clermont1 Roméo BONNEFOY François Vazeille LPC Clermont-Ferrand.
EC front unit status. Outline Conclusions from mechanical prototype and actions taken Status of electrical prototype KIT’s work for TA Dev plan (tests)
PWI Meeting Kanazawa 25/03/2006 Active Measurement of Mercury’s Plasma, AM 2 P CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE Laboratoire de Physique et.
CaRIBOu Hardware Design and Status
The EC-UNIT P. Barrillon on behalf of JEM-EUSO collaboration EUSO-BALLOON Phase A review 2 nd February 2012, CNES, Toulouse.
The PDM-block M. Casolino on behalf of JEM-EUSO collaboration EUSO-BALLOON Phase A review 2 nd February 2012, CNES, Toulouse.
TRIO-CINEMA 1 UCB, 2/08/2010 Instrument Interface Board Dorothy Gordon CINEMA - EE Team Space Sciences Laboratory University of California, Berkeley.
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.
1 Chap. 3 Interface. 2 Interface  Physical connection between node and transceiver  Network interface card (NIC)  Physical connection between transceivers.
Hardware proposal for the L2  trigger system detailed description of the architecture mechanical considerations components consideration electro-magnetic.
HOUSEKEEPING HK at Balloon-EUSO 10 th JEM-EUSO meeting from December 5 th to 10 th at RIKEN, Tokyo By G. Medina-Tanco*, A. Zamora, L. Santiago Cruz**,
EC_ASIC drawing (1) ASIC BASIC FASIC D 68 pi ns ASIC A 68 pi ns ASIC C ASIC E 120 pins ABCDEF 68 pi ns 68 pi ns 68 pi ns 68 pi ns.
ITAR Restricted Data THEMIS Power Subsystem CDR Peer Review 6/14/04 Probe and Probe Carrier Harness Dave Manges (301)
By: Uriel Barron Matan Schlanger Supervisor: Mony Orbach Final Review March 2015.
Acquisition Crate Design BI Technical Board 26 August 2011 Beam Loss Monitoring Section William Vigano’ 26 August
HK-status. RS422 (diff) RS232 SPI Trigger rate Analog(V,T) >=4 Analog(V,T)
- Overview of the subsystems - The Photodetector Module and its components - The Data Processing and its components - The Power Pack - Summary of subsystems.
P. Aspell CERN April 2011 CMS MPGD Upgrade …. Electronics 2 1.
Specifications Asic description Constraints Interface with PDM board Schedule Summary.
Prox-0.3 Georgia Institute of Technology Kiichiro DeLuca Richard Zappulla Matt Uhlman Ian Chen 1.
EUSO BALLOON Battery Power Pack (PWP) RIKEN/UAH Héctor Prieto, Katsuhiko Tsuno, Marco Casolino 1.
Mathias Reinecke AHCAL Main Meeting Electronics Integration - Status Mathias Reinecke for the AHCAL developers.
Anomalies &/or differences with the configuration Explanations, analyzes, impacts Updates EUSO-BALLOON, Flight review 04/06/2014 Guillaume Prévôt (APC)
STEREO IMPACT SEP Critical Design Review 2002-Nov-21/22 TvR1 SEP Mechanical Design Sandy Shuman, GSFC ) Tycho.
CERN – 7 Oct 04 1 LHCb Muon Grounding Anatoli Katchouk CERN Alessandro Balla, Paolo Ciambrone, Maurizio Carletti, Giovanni Corradi, Giulietto Felici, Rosario.
Ch. 6 Digital Data Communication Techniques. 6.1Asynchronous & Synchronous Transmission Asynchronous Transmission: transmission in which each information.
MICROCONTROLLER INTERFACING WITH STEPPER MOTOR MADE BY: Pruthvirajsinh Jadeja ( ) COLLEGE:DIET BRANCH:EC.
T HE PDM INTEGRATION P. Barrillon (LAL) & G. Prévôt (APC) On behalf of the PDM crew (Simon, Lech, Philippe, Sylvie B) EUSO-SPB/MiniEUSO progress meeting,
SeaPerch Electrical System. Electrical System Overview Assemble the control box. Make the Cat5 connector. Wire the motors to the tether. Wire the control.
Data Processor Status Hardware Giuseppe Osteria INFN Napoli Paris, October 12, 2012 Euso Balloon 8th progress meeting Giuseppe Osteria INFN Sezione di.
FSP progress update & camera concept Contents: Mechanical structure System components CCD sensor and circuit examples Hybrid concept IIC concept and tasks.
Michel DUPIEUX IRAP Progress Meeting LAL 02/03/ EC interface with PDM.
HVPS Configurations JEM EUSO Balloon Pierre Prat 17/09/2012.
Specifications Asic description Constraints Interface with PDM board Planning Summary.
Backplanes for Analog Modular Cameras EVO meeting. March 14 th,
EC electronic status. Outline Reminders History EC-front unit status EC_ASIC status What next ? 2.
Controls Crate. Mains Power Supply (x2) The 24 VDC generated by this module supplies all the power needed for the controls electronics. The 24 VDC generated.
Inductively Coupled Charging System Requirements –Operating Depth:5000m (16,400 ft) –Supply Power
Introduction of the EUSO-BALLOON 9th Progress Meeting Naples, November the 9th, 2012 Guillaume Prévôt, Sylvie Dagoret and Peter von Ballmoos 1 EUSO-BALLOON,
IR CAMERA EUSO BALLOON SPAS-UAH team S. Pérez Cano, H. Prieto, L. Del Peral & M. D. Rodríguez-Frías ORBITAL AeroSpace Company L. Ramírez JEM-EUSO Balloon.
SeaPerch Electrical System
Double Star: Table of Contents
Double Star: Table of Contents
Meeting on Services and Power Supplies
High-Voltage Supply Requirements Review
GLAST Large Area Telescope:
Overview of T1 detector T1 is composed by 2 arms
SeaPerch Electrical System
Presentation transcript:

Pierre PRAT Progress the Michel DUPIEUX

Grounding Design is now stable after Johan Panh’s Remarks

Grounding principles In order to avoid ground loops: Use of galvanically isolated DC/DC converters Primary grounds (28V Battery) shall be connected on Mechanical ground of PWP Secondary grounds of DC/DC converters shall be connected on a single point on Mechanical ground of sub-equipments (DP, PDM) Mechanical grounds connected together Differential links (LVDS) between HK, CCB and PDM_Board, HVPS- 1

Harness shielding According to the recommendations of Johan Panh: Primary power supplies : twisted pairs, not shielded Secondary power supplies : LVPS-PDM PDM_Board : twisted pairs, shielded, with shielding connected to mechanical ground (360°) on each sides (HF immunity) HVPS-1 HVPS-2 : twisted pairs, shielded, with shielding connected to mechanical ground on HVPS-1 side and open on load (BF immunity) LVPS-HK, LVPS1-DP, LVPS2-DP HK, CCB, CLKB, GPSR, CPU, DST: twisted pairs, not shielded (TBC: internal connection of DP) Differential digital links: twisted pairs, shielded, with the shielding connected to mechanical ground (360°) on each side

HK 1 2 BAT_RET (P) 28V_BAT (P) GND_28V (S) GND_3.3V (S) 28V (S) 3.3V (S) GND_M HVPS-1 would have DC/DC converters to isolate the powers GND_M V STATUS ON/OFF 3 DAC 6 Differential signals (LVDS) ( x2 = 18 wires) between HK and HVPS-1 4 differential transmitters 2 differential receivers CS_DAC CS_IO HVPS-1 MISO MOSI SCK MOS I 6 bidirectional signals 6 status signals I/O expander s 4 differential receivers MISO Interrupt SCK Interrupt HVPS-1 - HVPS-2 - HK - PDM-Board Interface Synoptic : 1 st flight version D-Sub 15 F D-Sub 15 M 6 C-W D-Sub 9 F D-Sub 9M BATTERY 3 C-W 6 x 14 HV lines 3 x 14 HV lines STATUS 3 ON/OFF V GND_M HVPS-2 CS_DAC SCK MOS I CS_OUT 6 DAC 6 D-SUB 25 F D-SUB 25 M D-Sub 9 F D-Sub 9M 24 wires PDM_Board Micro-D 9 F Micro-D 9 M 4 differential receivers 4 differential transmitters 4 Differential signals (LVDS) ( x2 = 8 wires) between PDM_Board and HVPS-1 4 SWITCH COMMANDS 2 differential transmitters

HVPS Architecture and I/F are now stable: 2 HVPS boxes in PDM box: HVPS-1: 2 CV DC/DC (28V & 3.3V) for ground isolation SPI I/F with HK, LVDS I/F with PDM-Board (switch pulses), 3 DACs (HV tuning), 3 Cockcroft-Walton Converters. HVPS-2: 6 DACs (HV tuning), 6 Cockcroft-Walton Converters.

Electrical Interfaces are clearly defined (connectors, pinout Ok) Subd25 or 37? Subd25 or µSubd9?

Pinout and connectors need to be checked and update very soon CPUCCBCLKbGPSrHKLVPS1LVPS2LVPS3PDLVPSPDMPWPSIRENTLS CPU- MDM DB9 - DB9 + DB9 DB RJ45- CCB MDM DB9 - MDM DB15 -DB15-DB9-- MDM DB CLKb MDM DB9 MDM DB15 - MDM DB9 DB15-DB GPSr-- MDM DB9 -DB15-DB HK DB9 + DB9 DB15 - MDM DB15 -DB9?3 x DB9 LVPS1DB DB9-- LVPS2-DB9 DB DB9-- LVPS3----DB PDLVPS----DB PDM- MDM DB51 --DB15--- DEMM9S DB9+DB PWP-----DB9 --?- SIRENRJ45---DB TLS3 x DB9-

LVPS-PDM Pinout and connectors between PDM_Board and EC_Asic are checked GND_5V_EC (S) 5V_EC (S) EC-ASIC 3.3Vd_EC (S) 1.5V_EC (S) GND_1.5V_EC (S) GND_3.3Vd_EC (S) 3.3Va_EC (S) GND_3.3Va_EC (S) FPGA GND_M Connector PDM-LVPS GND_5V_PDMB (S) 5V_PDMB (S) PDM BOARD TES V Regulator 1.5V GND_M 3.3V EC_ASIC 1 FPGA ground should be linked to the GND_M GND_1.5V_EC should be linked to the gnd of the FPGA 1V 1.8V Connector PDM_EC_ASIC

Kapton cable Fixation screw MAPMT ASIC BASIC FASIC D 68 pins68 pins ASIC A 68 pins68 pins ASIC C ASIC E 120 pins ABCDEF 68 pins68 pins 68 pins68 pins 68 pins68 pins 68 pins68 pins EC_HV Interfaces with:  CCB µSubd51  HVPS µSubd9  HK µSubd9? Subd25 on HK?  POWER Subd9

PWP2-Outside Power 22W?? Which dimensions PWP1-Inside Power 250 W ?? All connectors on a single side PWP-outside PWP-Inside 9 pins Sub-D connector To IR-CAM To LVPS-DP1 LVPS-DP2 LVPS-PDM LVPS-HK HVPS1 Plus two additional

Battery Cells, Connectors and Cables Cells Connectors Cables Option I: In case of 90W power consumption it will be necessary 20 cells of Saft G62/1.2 Option II: In case of 250W power consumption it will be necessary 50 Cells of Saft G62/1.2 The Connectors we are going to use are 9 pins D-Sub connectors for all interfaces and subsystems. The Cables we are going to use are THERMAX MIL-DTL-22759/91,92 for all interfaces and subsystems.

InterfacePower Consumption IR Camera22W High Voltage Power Supply2W LVPS DP17.2W LVPS DP27.2W Housekeeping6W LVPS-PDM2.4W CPU14.4W CCB5W Data Storage18W GPS1.2W CLK3.6W Additional Spare15W HeatersTBC Total: 111.2W+20% of security Margin = 133.4W Additional Heaters and backup = 70W (150+60)+20% of security Margin = 243.6W This version should be discussed 250W Interface Power Consumption IR Camera22W High Voltage Power Supply + Switches 2W Housekeeping6W CCB5W LVPS DP17.2W LVPS DP27.2W LVPS-PDM2.4W Additional Spare15W Total Power Budget: 74W+20% of Security Margin = 90W 90W - Which congiuration for Baseline? - Which power for Pack2 for IR Camera?

Short circuit risk? - Femeale connector on power side - PinOut of External Power - Common Ground or Ground Switching ? - Pinout Compatibility with LVPSs and HVPS1 ? - IR Camera the same way with separate Battery? - Who Provides Material and cables? Femeale connector?

Secondary subassembly Main Component Secondary subassembly Battery Pack Assembly Tests Battery Pack Packing CABLING FUSES Riken Institute Battery Pack +Fuse, switch and cabling integration SWITCHE S INTEGRATION WITH MECHANICS Post-integration tests Battery Pack Riken Institute Battery Pack assembly sequence

Electrical Interfaces are clearly defined (connectors, pinout Ok) HK DP 232/422

Who provide cables between:  HK and SIREN ?  HK and DP ?  PDM and DP ?  DP and SIREN ?  PWP_1 and LVPS (4)?  PWP_1 and HVPS_1?  LVPS_PDM and PDM?  HK et HVPS_1?  PDM_and HVPS_1?  CCB and PDM_board?  HK et PDM Board?  IR Camera ?

 Which Power budget PWP_1 ?  Clarify Power Pack interfaces.  Who provides Batteries (PowerPack 1 and Power Pack 2 ?  Clarify internal and external interfaces for DP (update Synoptic).  Define cables, providers ?  Use in general Femeale connector on Fixed on boxes exept for power side to avoid short circuit risk!!!  Documentation