EMCS Facility Status Thomas Niedermaier. This document is the property of Astrium. It shall not be communicated to third parties without prior written.

Slides:



Advertisements
Similar presentations
June 26, 2002; Page: 1 ESOC (TOS-OGR) European Space Operations Centre Manfred Warhaut Ground Segment Manager TOS-OGR ROSETTA Ground Segment.
Advertisements

Software Quality Assurance Plan
Coasting Phase Propellant Management for Upper Stages Philipp Behruzi Hans Strauch Francesco de Rose.
Training Purposes Only JEM EPO 17A JMU (Ver. 1.0) 1 Notice : This technical data is furnished on the condition that it will be used by and.
AMS-02 Rebaselining Outbrief ISS PIA/ICD & SSP MIP/ICD ISS Payload Mission Integration & Planning/OZ2 Space Shuttle Mission & Cargo Integration Office/MO3.
Chapter 14 Network Design and Implementation. 2 Network Analysis and Design Aspects of network analysis and design Understanding the requirements for.
Training Purposes Only JEM PLT OV JMU (Ver. 1.0) 1 Notice : This technical data is furnished on the condition that it will be used by and.
1 GAIA System Level Technical Reassessment Study Final Presentation ESTEC, April 23rd 2002 Part 1b Development & AIV.
GLAST LAT ProjectLAT Engineering Meeting, April 1, 2003 GLAST Large Area Telescope: Performance & Safety Assurance Darren S. Marsh Stanford Linear Accelerator.
1 Software Testing and Quality Assurance Lecture 37 – Software Quality Assurance.
Chapter 8 : Transaction Management. u Function and importance of transactions. u Properties of transactions. u Concurrency Control – Meaning of serializability.
REAL-TIME SOFTWARE SYSTEMS DEVELOPMENT Instructor: Dr. Hany H. Ammar Dept. of Computer Science and Electrical Engineering, WVU.
COMP8130 and 4130Adrian Marshall 8130 and 4130 Test Design & Documentation Adrian Marshall.
GLAST LAT ProjectNovember 18, 2004 I&T Two Tower IRR 1 GLAST Large Area Telescope: Integration and Test One and Two Tower Integration Readiness Review.
Disaster Recovery and Business Continuity Ensuring Member Service in Times of Crisis.
Transaction. A transaction is an event which occurs on the database. Generally a transaction reads a value from the database or writes a value to the.
IV&V Facility Model-based Design Verification IVV Annual Workshop September, 2009 Tom Hempler.
LSU 10/09/2007System Design1 Project Management Unit #2.
Troubleshooting methods. Module contents  Avaya Wireless tools  Avaya Wireless Client Manager  Avaya Wireless AP Manager  Hardware indicators  Non.
LSU 01/18/2005Project Life Cycle1 The Project Life Cycle Project Management Unit, Lecture 2.
LSU 07/07/2004Communication1 Communication & Documentation Project Management Unit – Lecture 8.
Design Completion A Major Milestone System is Presented to Users and Management for Approval.
All rights reserved © Altec ExoMars 2018 Rover Operations Control Centre Available Tools for planning and Data Processing I. Musso.
CRASH AND BURN ARIANE 5 Kristen Hieronymus SYSM6309 Advanced Requirements Engineering
Belgian User Support & Operations Centre Ham Video On-orbit Functional Commissioning - B.USOC Contribution ARISS Workshop 3 – 5 April 2014 ESTEC.
D. McMahon Generation of Ground ODFs ESA ODF-CB 3-5 March 2004 Gerd Soellner (DLR/Col-CC) Co-author Nathalie Gérard.
Airbus Training Perspective
SSIART – Smart Sensor Inter-Agency Reference Test bench Activity Presentation October 2010 Jean-François Dufour ESA/ESTEC/TEC-EDD.
CREATE THE DIFFERENCE Back ups and Recovery Janet Francis/Geoff Leese January 2010.
Next Doc Project Team: xxxxx Spring TitlePage Scope Statement Mission Statement3 Business Need4 Project Description5-6 Project Lifecycle Approach7.
MG 1/10/01 1 PCS SMOV-3B Review Objectives Overview Activity Descriptions Requirements.
Multi-part Messages in KMIP John Leiseboer, QuintessenceLabs.
SPS policy – Information Presentation Presentation to ROS June 16, 2004.
SpaceOps Stockholm Page 1 SpaceOps 2012 Stockholm Col-CC Voice System Migration During On-Going Operations Thomas Mueller, DLR,
THE PROJECT LIFE CYCLE PROJECT MANAGEMENT LIFE CYCLE LSU 01/18/2005 PROJECT LIFE CYCLE 1.
NERC Project S ystem Protection Coordination - PRC-027​ Presentation to the NSRS Conference Call August 17, 2015 Sam Francis Oncor Electric Delivery.
Wiimote/Kinect Lab Midterm Update Senior Design December 2011, Group 16 Adviser: Dr. Tom Daniels Brenton Hankins Rick Hanton Harsh Goel Jeff Kramer.
CCSDS SOIS Working Group Meeting – Berlin, Germany 14th of October 2008 Prototyping of CCSDS SOIS services on 1553 Bus Sev Gunes-Lasnet, Olivier Notebaert.
Fundamentals of Workflow Analysis and Process Redesign Unit Process Change Implementation and Evaluation.
Dosrad – Application Case Web:
Managing Challenging Projects Presented to the class of: Dr. Jane Mackay M.J. Neely School of Business.
Multi-part Messages in KMIP John Leiseboer, QuintessenceLabs.
GLAST LAT ProjectCDR/CD-3 Review May 12-16, 2003 Document: LAT-PR Section 5 IOC Subsystem 1 GLAST Large Area Telescope: IOC Subsystems WBS: 4.1.B.
SwCDR (Peer) Review 1 UCB MAVEN Particles and Fields Flight Software Critical Design Review Peter R. Harvey.
1 MINUS EIGHTY DEGREE LABORATORY FREEZER FOR ISS (MELFI) MSFC Briefing February 2005 John Cornwell
1 NOTICE: This document includes information that is proprietary to Composite Technology Development, Inc., and is for the sole use the U. S. Government.
MSFC Payload Training bs/kh/ExpPldsTST#1/ 3/18/2016 Page 1 Astroculture-8 (ADVASC) TST #1 April 27, 1998 DTM/Beth Skidmore NASA/MSFC Training Branch Voice.
NASA MSFC Mission Operations Laboratory MSFC NASA MSFC Mission Operations Laboratory Execute Tailored Procedures (XTP) Status POIWG – July 2015 Lamar Stacy.
Note: Glacier is launched unpowered and hardmounted in EXPRESS Rack 6 on Flight ULF2. For the following three weeks after activation or transfer, two 2-hour.
Note: The first status check should occur on the launch flight day prior to crew pre-sleep. This is the only feedback the Glacier team has that the Glacier.
OC Team Ops Notes. Jenn Whitworth I2 PRO What are Ops Notes? Ops notes are the OC team’s (OC, Paycom, PRO, CPO)
NASA MSFC Mission Operations Laboratory MSFC NASA MSFC Mission Operations Laboratory Obsolescence Driven Avionics Redesign (ODAR) Status POIWG #31, January.
ESA UNCLASSIFIED – For Official Use Experiment Development and Integration Process Philippe Schoonejans, Head of Robotics and Future Projects Office ESA.
EO10-PPO-020 OCR emcs /15/14 PARC/C. Traylor Crew Additional Activities Unattended EMCS Facility Cleanup Post Gravi-2 Ops EMCS-GASRMV MOD-RPL :20.
ACES User Interface Workshop #1 Prototype Inspection 22. November 2011.
Microgravity User Support Center (MUSC) Payload Overview POIWG, July Chart 1> MUSC Payload Overview > Patrick Hambloch POIWG > July 2013.
ESA Payload Operations Overview: MSL August 07, 2009 / POIC-MSFC.
This document is the property of EADS SPACE. It shall not be communicated to third parties without prior written agreement.Its content shall not be disclosed.
Powerpoint Templates Data Communication Muhammad Waseem Iqbal Lecture # 07 Spring-2016.
NASA MSFC Mission Operations Laboratory MSFC NASA MSFC Mission Operations Laboratory POIWG 23 Increment 17 Payload Operations Status Patricia Patterson.
OC Team Ops Notes. Jenn Whitworth I2 PRO What are Ops Notes? Ops notes are the OC team’s (OC, Paycom, PRO, CPO)
Double Star: Experiment Activities
Failure of Process / Failure of Mission
AMS Summary 16:00 on Fri 12 Apr 2019 (GMT 102) To
AMS Summary 16:00 on Thu 11 Apr 2019 (GMT 101) To
M. Kezunovic (P.I.) S. S. Luo D. Ristanovic Texas A&M University
<Your Team # > Your Team Name Here
Project Management Unit #2
AMS Summary 16:00 on Tue 9 Jul 2019 (GMT 190) To
Chapter 13: I/O Systems “The two main jobs of a computer are I/O and [CPU] processing. In many cases, the main job is I/O, and the [CPU] processing is.
Presentation transcript:

EMCS Facility Status Thomas Niedermaier

This document is the property of Astrium. It shall not be communicated to third parties without prior written agreement. Its content shall not be disclosed. Astrium Space Transportation 19/12/2006Page 2 EMCS Facility  EMCS was launched with ULF1.1 in July 2006 under terms of a Barter Agreement between NASA and ESA  It was operational for 171 days on orbit  Relocation from Destiny to Columbus was performed during 1J/A joint ops

This document is the property of Astrium. It shall not be communicated to third parties without prior written agreement. Its content shall not be disclosed. Astrium Space Transportation 19/12/2006Page 3 EMCS Experiments  TROPI Successful execution in EMCS. Science presented last month at the “Life in Space for Life on Earth” conference at Angers, France.  GRAVI-1: Adaptation of science protocol needed to be implemented due to SSPCM trip on ER3. Science presented at Angers.  MULTIGEN-1: Unexpected dry out due to operational issues, temporary loss of picture acquisition, partial recovery of science. Science presented at Angers.  CW/RW: The experiment containers could not be hydrated properly. Some science could be recovered.

This document is the property of Astrium. It shall not be communicated to third parties without prior written agreement. Its content shall not be disclosed. Astrium Space Transportation 19/12/2006Page 4 Technical Issues The major technical issues/problems are:  Experiment Containers not hydrating properly  Video Processing Unit (VPU) locking up  Unexpected shutdown of EMCS subsystems  Temporary loss of TM packets

This document is the property of Astrium. It shall not be communicated to third parties without prior written agreement. Its content shall not be disclosed. Astrium Space Transportation 19/12/2006Page 5 Experiment Containers Not Hydrating Properly During the CW/RW experiment it was not possible to hydrate JAXA’s Experiment Containers (ECs) as planned. Only 3 of 8 could be watered finally after several trouble shooting measures on orbit, from which only 1 EC produced enough plant material for the planned fixation, the other plants were recovered dried out. A fault tree analysis was prepared and used as baseline for trouble shooting on orbit and for development of a test plan for EMCS items to be returned. With the 1J flight 1 RBLSS Module (|), 2 Water Reservoirs (|), and 2 ECs (|) were returned. Tests are currently ongoing. The first findings indicate that the problem is at the interface between the Water Reservoir and the RBLSS Module.

This document is the property of Astrium. It shall not be communicated to third parties without prior written agreement. Its content shall not be disclosed. Astrium Space Transportation 19/12/2006Page 6 Video Processing Unit (VPU) Locking Up During the MULTIGEN-1 experiment the movements of the stem and the leaves of Arabidopsis thaliana were recorded. Approx. 32,000 images were taken and analysed for frequency and types of movement. At several occasions the VPU failed to communicate with the EMCS SPLC leading to a loss of images and to the need to perform ground commanding to restart the VPU and/or the SPLC, i.e., a proven workaround is in place if the loss of individual pictures is acceptable. An analysis of the software involved revealed that the VPU driver running on the SPLC is causing the problem. An updated interim version of this driver showed significant improvement of its robustness against loss of communication. It is proposed to update the VPU driver and - if necessary - of the EMCS application/basic software before the 2J/A flight.

This document is the property of Astrium. It shall not be communicated to third parties without prior written agreement. Its content shall not be disclosed. Astrium Space Transportation 19/12/2006Page 7 Unexpected Shutdown of EMCS Subsystems During MULTIGEN-1 EMCS H/W safety circuit switched off the EMCS subsystems due to spikes on the signal of the ACS O 2 safety sensor. After a workaround (i.e., decrease the O 2 level to 21 % if above) no more triggering occurred during MULTIGEN-1. After the move to Columbus no more spikes on the O 2 signal could be found but one more switch off with identical sequence occurred. During the 55 days of the CW/RW experiment two additional shutdowns due to loss of communication between the TCS and the SPLC occurred. All incidents are under investigation. No similar events happened with the ground model. The impact on science is the loss of lights and artificial gravity until restart of the EMCS subsystems.

This document is the property of Astrium. It shall not be communicated to third parties without prior written agreement. Its content shall not be disclosed. Astrium Space Transportation 19/12/2006Page 8 Temporary Loss of TM Packets A temporary loss of EMCS TM packets occurred during the EMCS operation in EXPRESS Rack 3. The TM is “going in and out” and transmission stabilizes by itself after minutes up to hours. In this state all commands were successfully received and executed by EMCS and it is proven that EMCS is producing TM because the outgoing TM queues are being filled up. However, it is not clear where between EMCS and the EXPRESS Rack Interface Computer the packets are being lost. Further analysis can be performed by connecting a SPLC ground model to the EXPRESS Suitcase Simulator. An impact on science may be caused by the temporary loss of TM including image transmission. In critical experiment phases realtime video could be used as an option.

This document is the property of Astrium. It shall not be communicated to third parties without prior written agreement. Its content shall not be disclosed. Astrium Space Transportation 19/12/2006Page 9 Next Steps  Analysis of hydration problem, fix and reverification of EMCS items on ground shall be completed until end of September  Performance of the postponed “EMCS clean-up after CW/RW” by the crew after the necessary EMCS resupply items have been launched.  On-orbit verification of the hydration feature.  Resume performance of experiments.

This document is the property of Astrium. It shall not be communicated to third parties without prior written agreement. Its content shall not be disclosed. Astrium Space Transportation 19/12/2006Page 10 Acronyms and Abbreviations ACSAtmosphere Control System CW/RWCell Wall/Resist Wall ECExperiment Container EMCSEuropean Modular Cultivation System EREXPRESS Rack RBLSSRotor Based Life Support System SPLCStandard Payload Computer SSPCMSolid State Power Controller Module TCSTemperature Control System TMTelemetry VPUVideo Processing Unit