Implementing the Comprehensive Open-architecture Space Mission Operations System (COSMOS) to Operate Multiple CubeSats
|
|
- Amos Harrington
- 5 years ago
- Views:
Transcription
1 Implementing the Comprehensive Open-architecture Space Mission Operations System (COSMOS) to Operate Multiple CubeSats Trevor C. Sorensen, Eric J. Pilger, Mark S. Wood, Miguel A. Nunes Hawaii Space Flight Laboratory University of Hawaii at Manoa 2014 California Polytechnic Institute San Luis Obispo, CA April 24, 2014
2 The mission of HSFL is to: promote innovative engineering and science research for terrestrial and planetary space missions 2 develop, launch, and operate small spacecraft from the Hawaiian Islands to accelerate the validation of new space technologies provide workforce training in all aspects of unmanned space missions promote synergistic collaborations between educational, governmental, and corporate institutions interested in space exploration
3 Major Project Elements Spacecraft Partner with NASA Centers and others to advance small spacecraft design. Design, build, launch, and operate kg small satellite for science and education tasks. Support technology validation missions as well as other University missions. Integration and Test Clean rooms in UH/POST will be used to assemble satellites. Systems integration Thermo-vac testing Vibration/shock testing Payload spin balancing Instruments The HSFL can call on a diverse group of instrument-developing faculty from HIGP and SOEST. A number of businesses in Hawaii also develop a wide array of instrumentation. The HSFL will partner with these organizations to provide technology demonstration opportunities. NASA Centers (Ames and JPL) are interested in joint technology missions. Launch Vehicle and Launch Support Pacific Missile Range Facility (PMRF) Local launch facility and mission support Modify existing S/C PMRF Systems launch pad for rail-fitted Avionics and modified VAFB Scout launcher. Power Telecom Kauai Test Facility Thermal (KTF)/ Sandia National Lab S/W Experience with H/W solid rockets and missile design. Use Super-Strypi launch vehicle. Can lift ~270 kg (594 pounds) to low-earth orbit (400 km). Heritage working with PMRF as on-site vehicle integrator and launch agent. Ground Station & Mission Operations UH/HSFL maintains UHF/VHF receiving stations with Kauai CC and Honolulu CC staff. Ground station provides command and control broadcast as well as data downlink capabilities. Mission Ops Center on POST 5 th floor under development with UH support. 3
4 COSMOS Purpose Comprehensive Open-architecture Space Mission Operations System (COSMOS)* Purpose: To develop a comprehensive open system of software and hardware tools that supports the design, testing, and operations of one or more spacecraft and is easily adaptable for adding spacecraft and porting to Mission Operations Centers (MOCs) at HSFL, NASA Ames Research Center, and other MOCs. COSMOS is being developed as a collaboration between HSFL and NASA Ames Research Center under a 3-year NASA EPSCoR grant ( ). * Note: COSMOS is being renamed to: Comprehensive Open-architecture Software for Mission Operations Systems 4
5 COSMOS Architecture - Background Explosive growth in micro and nano satellites. Industry need for comprehensive operations software toolkit Developing hardware concept of Plug-n-Play COSMOS combines Plug-n-Play, standard interfaces and protocols, and common coding practices COSMOS can be used across the spectrum, from conceptual design to mission operations 5
6 Features of COSMOS Set of software and hardware framework to support spacecraft and other vehicle mission operations Set of tools: Mission Planning & Scheduling Tool (MPST) Mission Operations Support Tool (MOST) Ground Segment Control Tool (GSCT) Data Management Tool (DMT) Flight Dynamics Tool (FDT) Analysis Tools Test Bed Control Tool (TBCT) Open architecture to enable modifications and adaptation to new missions and MOCs User-friendly interfaces and short learning curves for users and software integrators COSMOS editor Uses Qt under LGPL licensing helps ITAR issues Connections for COTS/GOTS and external tools 6
7 COSMOS Generalized Architecture Spacecraft Ground Stations UAVs Submersibles NODES Rovers Launch Vehicles COSMOS Monitor & Control Tools Agents 7
8 COSMOS Functional Architecture Ground Station Network COSMOS Schedule Mission Planning & Scheduling Pass Plan Orbit Ephemeris SC Uploads COSMOS GS Interface GS CMD SC R/T CMD GS Status SC SOH TLM Mission Anomaly State Contact Operations Process Data Management Mission Analysis Mission Analysis Resolution Projection P/L Data Post-Pass Reports Simulators & Testbed/Simulator Operational Testbed Ground Network Control Payload Operations Flight Dynamics System Management & Quality Assurance Mission Status Mission Data Operator Commands Mission Status Payload Data SC Engineers Reports Anomaly Resolution Request Tasking Requests COSMOS GUI Mission Operations Team Tasking Requests Payload Status Reports Payload Customers Reports 8
9 COSMOS Architecture - Elements Standards: Language: Posix compliant C++11 O/S: Linux MacOS Windows 7 Protocols and Environments: Qt JavaScript Object Notation (JSON) 9
10 Mission Operations Support Tool (MOST) Primary visualization and commanding tool of COSMOS designed specifically for supporting near-realtime operations. MOST functions: Spacecraft/payload monitor and control Mission Planning Simulations and testing Training and rehearsals Trending and analysis Anomaly resolution Designed initially to support HSFL s HawaiiSat-1 mission Adapted to support missions with multiple elements 10
11 MOST Background Based on legacy programs designed by Dr. Sorensen for the Naval Research Laboratory: UltraViolet Plume Instrument (UVPI) Encounter Manager for SDIO/LACE satellite encounter execution (1991) LUNOPS program used to monitor science mission operations during the Clementine lunar mission (1994) UVPI Encounter Manager Sample Screen LUNOPS on Left Screen in Clementine MOC 11
12 Mission Operations Support Tool (MOST) Stored Data Space Dynamics Engine R/T Data Data MOST FSW HW Operational Testbed Cmds R/T Data Cmds Cmds Flight Controller MODES R/T Extrapolated Simulated Archival OBCS/ C&DH EPS Telecom Orbit + others ADCS TCS Payloads FSW Payloads 12
13 Mission Operations Support Tool (MOST) 13
14 MOST Configured for 3U CubeSat 14
15 COSMOS Executive Operator (CEO) Provides Situational Awareness (Monitoring) of all Spacecraft Simultaneously Initial design supports up to 100 spacecraft Three different selectable levels of monitoring Low S/C ID, status of S/C, status of P/L, GS contact status Medium shows orbit position and data, day/umbra status (C/D T), GS contact status (C/D T), status of SS, S/C or ACS modes, etc. High Similar to main display of MOST giving detailed information MOST can be launched to provide detailed SS information or commanding capability for any spacecraft Displays orbit tracks of all spacecraft (filter to select specific s/c) Can handle actual and simulated spacecraft simultaneously Flight Dynamics Display shows relative positions of spacecraft Communications Display shows satellite communication crosslinks (ideal for constellation monitoring) 15
16 CEO Features (cont.) Provides Monitoring of Ground Stations Top-level status of all ground stations in network Can launch GSCT for more detailed monitoring and control Provides Management of MOC Operations Monitors allocation of COSMOS tools to spacecraft Monitors personnel resource utilization Access console logs (current or archived) Communicate with one or MOC positions Monitors COSMOS System Performance Monitors console computer performance and utilization Monitors status of COSMOS tools and data flow between the COSMOS elements Launch any COSMOS Tools MPST, MOST, GSCT, DMT, TBCT, Analysis Tools 16
17 CEO - Main Display (Design) Status of All Satellites Enlarged Status Displays UTC :43:07 MOC 08:43:07 CONTROL ALLOCATIONS Sat # Satellite Name MOST GSC Actual Actual Actual Actual Actual Actual Actual Actual Actual Actual 001 TinySat-1 Autonomous C S P S C P S C P S S C S P C P C S P C S P C S P C P C S P 002 TinySat-2 Autonomous TinySat-3 Autonomous Actual Actual Actual Actual Actual Actual Actual Actual Actual Actual C S P C S P C S P C S P C S P C S P C S P C S P C S P C S P 004 TinySat-4 Autonomous TinySat-5 Autonomous 006 TinySat-6 Autonomous Actual Actual Actual Actual Sim Sim C S P C S P C S P C S P 007 TinySat-7 Autonomous 008 TinySat-8 Autonomous TikiSat-1 Autonomous 010 TikiSat-2 Autonomous Autonomous HawaiiSat-1 Autonomous 012 HawaiiSat-2 SpaceCadet 1 SpaceCadet MightySat Manual ClearSat SpaceCadet 2 SpaceCadet KUD0Sat-1 Autonomous KUD0Sat-2 Autonomous 017 BoxSat-1 Autonomous 018 BoxSat-2 Autonomous BoxSat-3 Autonomous 020 BoxSat-4 Autonomous 021 BoxSat-6 Autonomous BoxSat-9 SpaceCadet 3 Autonomous 023 BoxSat-10 Autonomous BoxSat-11 SpaceCadet 3 SpaceCadet SimSat-A SpaceCadet 4 Manual Orbit View Actual SORT Sub-Sat View Resources PERSONNEL Controller Status MPST MOST GSCT DMT TBCT CEO Flight Director On 1 1 SpaceCadet 1 On 1 1 SpaceCadet 2 On 1 SpaceCadet 3 On 2 1 SpaceCadet 4 Off SpaceCadet 5 Off SpaceCadet 6 Off SpaceCadet 7 Off SpaceCadet 8 Sim 1 SpaceCadet 9 Off SpaceCadet 10 Off Trainee 1 Sim 1 Trainee 2 On 1 Trainee 3 On 1 Trainee 4 Off Actual Orbit View Actual Sub-Sat View Actual Orbit View Actual Orbit View CEO COSMOS Executive Operator Actual LocalT 14:43:07 MET 1234:09:32:27 Orbit HawaiiSat-1 MOST 12 HawaiiSat-2 MOST 13 MightySat MOST 14 ClearSat MOST 15 KUDOSat-1 MOST 16 KUDOSat-2 MOST 17 BoxSat-1 MOST 18 BoxSat-2 MOST 19 BoxSat-3 MOST 20 BoxSat-4 MOST Orbit View SELECT Actual Sub-Sat View Actual Sub-Sat View Actual Sub-Sat View Actual Ground Tracks (selectable) Lat N Long E Alt 0123 k Lat N Long E Alt 0489 k Lat S Long E Alt 0557 k Lat S Long E Alt 0623 k Lat N Long E Alt 7623 k Lat N Long E Alt 5523 k Lat N Long E Alt 0123 k Lat N Long E Alt 0489 k Lat S Long E Alt 0557 k Lat S Long E Alt 0623 k 45:03 Umbra Local Time 245:19:07:58 S/C State Nominal ADCS Mode LVLH Ground St ASF-1 22:10 AOS B C L EPS OBC ADC RF TCS + 26:58 Local Time 245:02:07:58 S/C State Nominal ADCS Mode IH2 Ground St SSC 08:15 LOS UHF, SBand B C L EPS OBC ADC RF RCS + 07:53 Umbra Local Time 245:07:07:58 S/C State Nominal ADCS Mode LVLH Ground St KCC 17:20 AOS CONTACT EPS OBC ADC RF TCS + 27:53 82:53 Umbra Local Time 245:09:07:58 Local Time 245:21:07:58 S/C State SAFE Ground St SCC 17:20 LOS ADCS Mode SAFE VHF, SBand Ground St KCC 37:20 AOS B C L CAR LCK RCS SM GNC CM1 CM2 EPS OBC ADC RF TCS + EPS OBC ADC COM TCS 82:53 Umbra Local Time 245:21:07:58 Ground St SCC 17:20 LOS VHF, SBand B C L RCS SM GNC CM1 CM2 EPS OBC ADC COM TCS 45:03 Umbra Local Time 245:19:07:58 S/C State Nominal ADCS Mode LVLH Ground St ASF-1 22:10 AOS B C L EPS OBC ADC RF TCS + 26:58 Local Time 245:02:07:58 S/C State Nominal ADCS Mode IH2 Ground St SSC 08:15 LOS UHF, SBand B C L EPS OBC ADC RF RCS + 07:53 Umbra Local Time 245:07:07:58 S/C State Nominal ADCS Mode LVLH Ground St KCC 17:20 AOS CONTACT EPS OBC ADC RF TCS + 27:53 Local Time 245:09:07:58 S/C State SAFE ADCS Mode SAFE Ground St KCC 37:20 AOS CAR LCK EPS OBC ADC RF TCS + 21 BoxSat-6 MOST 22 BoxSat-9 MOST 23 BoxSat-10 MOST 24 BoxSat-11 MOST 25 SimSat-1 MOST 26 SimSat-2 MOST Sub-Sat View Actual Orbit View Actual Sub-Sat View Actual Sub-Sat View Actual Orbit View Simulation Orbit View Simulation Lat S Long E Alt 0123 k Lat N Long E Alt 0123 k Lat S Long E Alt 0123 k Lat S Long E Alt 0123 k Lat S Long E Alt 1123 k Lat S Long E Alt 0723 k 45:03 Umbra Local Time 245:19:07:58 S/C State Nominal ADCS Mode LVLH Ground St ASF-1 22:10 AOS B C L EPS OBC ADC RF TCS + 26:58 Local Time 245:02:07:58 S/C State Nominal ADCS Mode IH2 Ground St SSC 08:15 LOS UHF, SBand B C L EPS OBC ADC RF RCS + 07:53 Umbra Local Time 245:07:07:58 S/C State Nominal ADCS Mode LVLH Ground St KCC 17:20 AOS CONTACT EPS OBC ADC RF TCS + 27:53 07:53 Umbra Local Time 245:09:07:58 Local Time 245:07:07:58 S/C State SAFE S/C State Nominal ADCS Mode SAFE ADCS Mode LVLH Ground St KCC 37:20 AOS Ground St KCC 17:20 AOS CAR LCK CONTACT EPS OBC ADC RF TCS + EPS OBC ADC RF TCS + 07:53 Umbra Local Time 245:07:07:58 S/C State Nominal ADCS Mode LVLH Ground St KCC 17:20 AOS CONTACT EPS OBC ADC RF TCS + MOC Computers Status CPU MEM DISK #1 #2 #3 #4 #5 #6 #7 #8 #9 #10 MC1 MC2 MC3 OTB1 OTB2 MC5 MC6 MC7 MC8 MC9 10% NODE #1 (MC1) STATUS KCC UHF Ground St Band Local Tm 009 Azimuth Sat # Elevation Max Elev AUTO AOS Mode LOS CONTACT 245:07:07: :38:37 [+05:30] 19:47:27 [-04:20] KCC ASF-1 ASF-2 SCC-1 SCC-2 UHF S-B S-B UHF S-B OPER STBY OPER DOWN STBY ABC DEF-1 DEF-2 DEF-3 GHI-2 C-B S-B S-B X-B Ku-B LNK STBY OPER OPER OFF HMC3-1 HMC3-2 NMC3-1 NMC3-2 SMC3-1 UHF S-B UHF S-B UHF STBY OPER STBY STBY OFF SMC3-2 BMC3-1 BMC3-2 WPGS ARC-1 VHF S-B UHF S-B UHF OFF OPER OPER LNK DOWN ARC-2 ARC-3 ARC-4 ARC-5 UHF UHF S-B S-B OPER OPER STBY OPER Ground Segment Monitor MSG 17
18 CEO - Main Display (Current) Ground Tracks (selectable) Status Displays (8) Ground Segment Monitor 18
19 CEO FD Display (Current) 19
20 COSMOS Multi-satellite Architecture 20
21 COSMOS Multi-satellite Architecture Data can be collected from multiple nodes that live in the same network In the case of multiple satellites, each satellite is a node Nodes are COSMOS-aware Nodes execute COSMOS agents Each agent complies with the COSMOS namespace Multiple ground stations can collect the data and forward the data using COSMOS agents The Mission Operations Center Servers Synchronize the data Parse the data into usable formats COSMOS Tools Visualize the data in archival mode or real time Command and Control scripts 21
22 Mahalo! Dr. Trevor C. Sorensen
Comprehensive Open-architecture Solution for Mission Operations Systems
Comprehensive Open-architecture Solution for Mission Operations Systems Dr. Trevor C. Sorensen January, 2016 COSMOS Purpose Original Purpose: To develop a comprehensive open system of software and hardware
More informationSpace Mission Development Capabilities
Space Mission Development Capabilities HSFL Overview Presentation Updated January 6, 2017 HSFL Contact Email: info@hsfl.hawaii.edu Phone: 808-956-3138 (Hawaii Space Grant) Demand for Small Space August
More informationThe E-SAIL programme. 10th IAA Symposium on Small Satellites for Earth Observation April 20-24, 2015 Berlin LuxSpace s.à.r.
The E-SAIL programme 10th IAA Symposium on Small Satellites for Earth Observation April 20-24, 2015 Berlin LuxSpace s.à.r.l An OHB company Contents LuxSpace Background Consortium Spacecraft Specific issues
More informationSciBox, a Proven Automated Planning and Commanding System
SciBox, a Proven Automated Planning and Commanding System Teck Choo, Edward Russell, Michael Kim February 25, 2014 2014 by The Johns Hopkins University/Applied Physics Laboratory. Published by The Aerospace
More informationHARP CubeSat An innovative Hyperangular Imaging Polarimeter for Earth Science Applications
HARP CubeSat An innovative Hyperangular Imaging Polarimeter for Earth Science Applications J. Vanderlei Martins, Tim Nielsen, Chad Fish, Leroy Sparr, Roberto Fernandez-Borda, Mark Schoeberl, Lorraine Remer
More informationDARE Mission and Spacecraft Overview
DARE Mission and Spacecraft Overview October 6, 2010 Lisa Hardaway, PhD Mike Weiss, Scott Mitchell, Susan Borutzki, John Iacometti, Grant Helling The information contained herein is the private property
More informationOTSUKIMI Moon-sighting Satellite Kyushu Institute of Technology. 3 rd Mission Idea Contest UNISEC Global
OTSUKIMI Moon-sighting Satellite Kyushu Institute of Technology 3 rd Mission Idea Contest UNISEC Global The Idea We want to take image for the moon phases as seen from Earth Why? Introduction 1.6 billion,23.4%
More informationThe time period while the spacecraft is in transit to lunar orbit shall be used to verify the functionality of the spacecraft.
ASE 379L Group #2: Homework #4 James Carlson Due: Feb. 15, 2008 Henri Kjellberg Leah Olson Emily Svrcek Requirements The spacecraft shall be launched to Earth orbit using a launch vehicle selected by the
More informationPROBA 1. F. Teston ESA/ESTEC D/TEC-EL
PROBA 1 F. Teston ESA/ESTEC D/TEC-EL Frederic.Teston@esa.int PROBA 1 launch PROBA 1 has been launched on 21 October 2001 Orbital parameters: Altitude: 681-561 km Near polar (inclination of 97.9 ) Sun-synchronous
More informationFigure 1. View of ALSAT-2A spacecraft
ALSAT-2A TRANSFER AND FIRST YEAR OPERATIONS M. Kameche (1), A.H. Gicquel (2), D. Joalland (3) (1) CTS/ASAL, 1 Avenue de la Palestine, BP 13, Arzew 31200 Oran, Algérie, email:mo_kameche@netcourrier.com
More informationMETHODS OF BALLISTIC SUPPORT AND SUPERVISION OF RESEARCH AND TECHNOLOGICAL EXPERIMENTS OF FOTON SC
METHODS OF BALLISTIC SUPPORT AND SUPERVISION OF RESEARCH AND TECHNOLOGICAL EXPERIMENTS OF FOTON SC Jury. M. Ustalov RSC TsSKB-Progress, Samara, Russia Abstract A wide range of research and technological
More informationPolish Student Activities in Space Research and Education
Polish Student Activities in Space Research and Education Warsaw University of Technology: Student Astronautical Group Student Space Engineering Scientific Group Radiolocation and Digital Signal Processing
More informationmy_epp External Payload Platform
my_epp External Payload Platform A new Cubesat testbed and payload hosting platform on the International Space Station with reliable fast-track and low-cost mission scenario Dr. P. C. Steimle*, K. Kuehnel**,
More informationCHAPTER 3 PERFORMANCE
PERFORMANCE 3.1 Introduction The LM-3A performance figures given in this chapter are based on the following assumptions: Launching from XSLC (Xichang Satellite Launch Center, Sichuan Province, China),
More informationHerschel Science/Instrument Planning and Scheduling. Jon Brumfitt (ESAC) SCIOPS September 2013
Herschel Science/Instrument Planning and Scheduling Jon Brumfitt (ESAC) SCIOPS-2013 11 September 2013 Herschel Space Observatory Far infrared & sub-mm Telescope diameter Instruments Launch date End of
More informationLunar Flashlight Project
ABSTRACT Recent observations of the Moon with the Moon Mineralogy Mapper (M3), Lunar Crater Observation and Sensing Satellite (LCROSS), the Lunar Reconnaissance Orbiter (LRO) and other evidence suggest
More informationBUILDING LOW-COST NANO-SATELLITES: THE IMPORTANCE OF A PROPER ENVIRONMENTAL TESTS CAMPAIGN. Jose Sergio Almeida INPE (Brazil)
BUILDING LOW-COST NANO-SATELLITES: THE IMPORTANCE OF A PROPER ENVIRONMENTAL TESTS CAMPAIGN Jose Sergio Almeida INPE (Brazil) 1 st International Academy of Astronautics Latin American Symposium on Small
More informationEurope to the Moon. BHF 10 Feb 2005 SPC
Europe to the Moon V162 lift-off on 27 September 2003 at 23:14:39 UTC The launch was perfect SMART-1 separated at 23:56:03 into a GTO (656 x 35,881 km): perfect injection 100 s later telemetry was received
More informationmstar: Space-Time Asymmetry Research
mstar: Space-Time Asymmetry Research Testing Lorentz Invariance in Low-Earth Orbit Abdulaziz Alhussien for the mstar team November 15 th, 2013 1 Kinematic Approach to LIV Is the CMB a preferred frame?
More informationGravitational & Planetary Research Program
2012 Gravitational & Planetary Research Program Goals Why? Relativity, Gravitational Waves, Geodesy, Aeronomy Space Technology Education and Training: STEM Team Who? NASA Universities Industry Foreign
More informationAIR BEARING ADCS TEST BED. Daniel E. Wukelic College of Engineering University of Hawai i at Mānoa Honolulu, HI ABSTRACT INTRODUCTION
AIR BEARING ADCS TEST BED Daniel E. Wukelic College of Engineering University of Hawai i at Mānoa Honolulu, HI 96822 ABSTRACT The Hawai i Space Flight Laboratory (HSFL) designs, tests and builds small
More informationNew Worlds Observer Operations Concept NEW WORLDS OBSERVER OPERATIONS CONCEPT (OPSCON)
NEW WORLDS OBSERVER OPERATIONS CONCEPT (OPSCON) 1 Table of Contents 1.0 Mission Overview... 1 1.1 NWO scope... 1 2.0 System Overview... 2 2.1 System constituents... 2 2.2 system functional architecture...
More informationMULTI PURPOSE MISSION ANALYSIS DEVELOPMENT FRAMEWORK MUPUMA
MULTI PURPOSE MISSION ANALYSIS DEVELOPMENT FRAMEWORK MUPUMA Felipe Jiménez (1), Francisco Javier Atapuerca (2), José María de Juana (3) (1) GMV AD., Isaac Newton 11, 28760 Tres Cantos, Spain, e-mail: fjimenez@gmv.com
More informationLAUNCH SYSTEMS. Col. John Keesee. 5 September 2003
LAUNCH SYSTEMS Col. John Keesee 5 September 2003 Outline Launch systems characteristics Launch systems selection process Spacecraft design envelope & environments. Each student will Lesson Objectives Understand
More informationPRELIMINAJ3.:( 6/8/92 SOFTWARE REQUIREMENTS SPECIFICATION FOR THE DSPSE GUIDANCE, NAVIGATION, AND CONTROL CSCI. Prepared by
PRELIMINAJ3.:( SOFTWARE REQUIREMENTS SPECIFICATION FOR THE DSPSE GUIDANCE, NAVIGATION, AND CONTROL CSCI Prepared by Space Applications Corporation 6/8/92.. 1 SCOPE 1.1 IDENTIFICATION 1.2 OVERVIEW This
More informationLOW-COST LUNAR COMMUNICATION AND NAVIGATION
LOW-COST LUNAR COMMUNICATION AND NAVIGATION Keric Hill, Jeffrey Parker, George H. Born, and Martin W. Lo Introduction Spacecraft in halo orbits near the Moon could relay communications for lunar missions
More informationCHAPTER 3 PERFORMANCE
PERFORMANCE 3.1 Introduction The LM-3B performance figures given in this chapter are based on the following assumptions: Launching from XSLC (Xichang Satellite Launch Center, Sichuan Province, China),
More informationAn Agile Multi-Use Nano Star Camera for Constellation Applications
An Agile Multi-Use Nano Star Camera for Constellation Applications Scott Palo 1,2, George Stafford 2 and Alan Hoskins 1 1 University of Colorado 2 Blue Canyon Technologies Partnership The BCT technical
More informationSP-1291 June Mars Express. The Scientific Investigations
SP-1291 June 2009 Mars Express The Scientific Investigations Operations and Archiving Mars Express Science Planning and Operations R. Pischel & T. Zegers ESA/ESTEC, Research and Scientific Support Department,
More informationUsing the International Space Station as an Engineering Technology Research Laboratory for Space Based Telescopes
Using the International Space Station as an Engineering Technology Research Laboratory for Space Based Telescopes David W. Miller Director, Professor, MIT Dept. of Aeronautics and Astronautics Javier de
More informationSystem engineering approach toward the problem of required level of in-orbit autonomousoperation of a LEO microsatellite mission
System engineering approach toward the problem of required level of in-orbit autonomousoperation of a LEO microsatellite mission H.Bonyan Amirkabir University of Technology (AUT) H.Bonyan@dena.aut.ac.ir
More informationLunar Precursor Robotics Program
National Aeronautics and Space Administration SCIENCE & MISSION SYSTEMS Lunar Precursor Robotics Program Michael J. Wargo, Sc.D. Chief Lunar Scientist for Exploration Systems Larry Hill LRO Mission Manager
More information9 Aug 04 Getting Technology to Space for the Warfighter
1 SMC Detachment 12 - The Dirty Dozen Space Test Program-1 (STP-1) First of its Kind! Major Ray Galik STP-1 Program Manager 9 Aug 2004 Overview STP-1 Mission summary STP-1 Firsts Manifest Changes Space
More information483 Lecture. Space Mission Requirements. February11, Definition Examples Dos/ Don ts Traceability
483 Lecture Space Mission February11, 2012 Photo Credit:: http://www.spacewallpapers.info/cool-space-wallpaper What s a Requirement? ification? Requirement A concept independent statement of a mix of needs,
More informationYour Partner in Environment Monitoring
Your Partner in Environment Monitoring Radiation Environment in Space The ionizing radiation in space represents one of the most severe environmental loads to space hardware and can cause a large number
More informationExploration Carriers UPC-Orion Launch Opportunities for Lunar Missions. presented to The Joint Annual Meeting of LEAG-ICEUM-SRR
Exploration Carriers UPC-Orion Launch Opportunities for Lunar Missions presented to The Joint Annual Meeting of LEAG-ICEUM-SRR Bruce Milam and Ruthan Lewis, Ph.D. NASA Goddard Space Flight Center October
More informationWISE Science Data System Single Frame Position Reconstruction Peer Review: Introduction and Overview
WISE Science Data System Single Frame Position Reconstruction Peer Review: Introduction and Overview R. Cutri and the WSDC Team @ IPAC 1 Review Panel Rachel Akeson (IPAC/MSC) Gene Kopan (IPAC retired)
More informationBRITE One Year in Orbit
BRITE One Year in Orbit O. Koudelka, M.Unterberger, P.Romano Graz University of Technology W.Weiss, R.Kuschnig University of Vienna 1 Contents Scientific Goals Mission Description Commissioning Science
More informationProspector-1: A Low-Cost Commercial Asteroid Mission Grant Bonin SmallSat 2016
Prospector-1: A Low-Cost Commercial Asteroid Mission Grant Bonin SmallSat 2016 About DSI A space technology and resources company Vision to enable the human space development by harvesting asteroid materials
More informationOperational Aspects of Space Weather-Related Missions
Operational Aspects of Space Weather-Related Missions Richard G. Marsden, ESA/SCI-SH Outline SOHO: Example of Near-Earth Observatory-class Mission Ulysses: Example of Deep Space Monitor-class Mission Solar
More informationMISSION ENGINEERING SPACECRAFT DESIGN
MISSION ENGINEERING & SPACECRAFT DESIGN Alpbach 2007 - D.J.P. Moura - CNES MISSION ENGINEERING (1) OVERALL MISSION ENGINEERING IS A COMPLEX TASK SINCE AT THE BEGINNING THE PROBLEM IS GENERALLY BADLY EXPRESSED
More informationSatellite communications and the environment of space. V 1.1 Swiss Space Summer Camp 2016 Images: NASA 1
Satellite communications and the environment of space Swiss Space Summer Camp 2016 Images: NASA 1 Can you name these satellites? Sputnik The first man made satellite Launched in 1957 by The USSR Mass 84kg,
More informationPlanning, Simulation, and Assessment of Various Missions from Wallops Flight Facility using Satellite Toolkit (STK)
Planning, Simulation, and Assessment of Various Missions from Wallops Flight Facility using Satellite Toolkit (STK) Mitchell 1 Mission Planning Lab, Wallops Flight Facility, Wallops Island, VA, 23337 Satellite
More informationScience planning and operations for Mars Express
Science planning and operations for Mars Express René Pischel and Tanja Zegers ESA/ESTEC, Research and Scientific Support Department, Postbus 299, 2200 AG Noordwijk, The Netherlands I. Introduction The
More informationVicky Chu, Jer Ling, Tom Lin, Joe Fong, Feng-Tai Huang, Guey-Shin Chang. April 15, 2011
FORMOSAT-7/COSMIC-2 Overview Vicky Chu, Jer Ling, Tom Lin, Joe Fong, Feng-Tai Huang, Guey-Shin Chang April 15, 2011 Program Status AIT-TECRO Agreement on FORMOSAT-7/COSMIC-2 joint program has been signed
More informationDevelopment of the Space Debris Sensor (SDS) Joe Hamilton SDS Principal Investigator January
Development of the Space Debris Sensor (SDS) Joe Hamilton SDS Principal Investigator January 31. 2017 Outline Background Orbital Debris Measurement Coverage What is SDS? Detection Principles Example 0.4
More informationStanford, Space Gravity Research Group
Stanford, Space Gravity Research Group John W. Conklin, Sasha Buchman, and Robert Byer Gravitational science Earth observation: Geodesy, aeronomy Gravity-waves 1 Space Gravity Technology Development Drag-free
More informationBRINGING YOUR EXPERIMENT INTO SPACE
BRINGING YOUR EXPERIMENT INTO SPACE Science Service Division SSC - Swedish Space Corporation Space exploration with ESA: opportunities within the ESA programme E3P Stockholm, 13 November 2018 SWEDISH SPACE
More informationSpace Frequency Coordination Group
Space Coordination Group THE SFCG Recommendation SFCG 32-2R1 COMMUNICATION FREQUENCY ALLOCATIONS AND SHARING IN THE LUNAR REGION CONSIDERING a. that a regional communication network at the Moon can be
More informationFIREBIRD and SSEL Space Weather Missions
Space Science and Engineering Laboratory FIREBIRD and SSEL Space Weather Missions Ehson Mosleh Systems Engineer Space Science and Engineering Laboratory Montana State University CubeSat Developers Workshop
More informationLaunches and On-Orbit Performance
Launches and On-Orbit Performance An Update on Nanosatellite Missions at the UTIAS Space Flight Laboratory Daniel D. Kekez,, Robert E. Zee, Freddy M. Pranajaya Space Flight Laboratory University of Toronto
More informationGG studies at TAS-I: state of the art
GG studies at TAS-I: state of the art A. Anselmi INRIM, 24-10-2014 83230350-DOC-TAS-EN-002 GG@ThalesAleniaSpace! 1996 Early experiment concept presented to ESA HQ! Industrial support on satellite & drag-free
More informationLRO Lunar Reconnaissance Orbiter
LRO Lunar Reconnaissance Orbiter Launch Date: June 18, 2009 Destination: Earth s moon Reached Moon: June 23, 2009 Type of craft: Orbiter Intended purpose: to map the moon like never before, add additional
More informationESSE Payload Design. 1.2 Introduction to Space Missions
ESSE4360 - Payload Design 1.2 Introduction to Space Missions Earth, Moon, Mars, and Beyond Department of Earth and Space Science and Engineering Room 255, Petrie Science and Engineering Building Tel: 416-736
More informationThermal Vacuum Test: Plans and Procedures
GLAST Large Area Telescope Gamma-ray Large Area Space Telescope Pre-Shipment Review Thermal Vacuum Test: Plans and Procedures Jesse Armiger Thermal Vacuum Test Director Thermal Vacuum Test Stanford Linear
More informationPredicting Long-Term Telemetry Behavior for Lunar Orbiting, Deep Space, Planetary and Earth Orbiting Satellites
Predicting Long-Term Telemetry Behavior for Lunar Orbiting, Deep Space, Planetary and Earth Orbiting Satellites Item Type text; Proceedings Authors Losik, Len Publisher International Foundation for Telemetering
More informationSVOM Science Ground Segment
SVOM Science Ground Segment Maohai Huang National Astronomical Observatories, CAS on behalf of the SVOM Ground Segment team 2016-10-11 Hotwiring the Transient Univserse V, Villanova, M. Huang 1 GRB Mission
More informationCelestia Development Status
Celestia Development Status Chris Laurel claurel@gmail.com 3 rd ESA Workshop on Astrodynamics Tools and Techniques 2-5 October 2006 ESTEC, Noordwijk, The Netherlands Contents Introducing Celestia Development
More informationTROPOMI. Sentinel 5 Precursor instrument for air quality and climate observations. R. Voors Dutch Space. ICSO, 11 October 2012
TROPOMI Sentinel 5 Precursor instrument for air quality and climate observations R. Voors Dutch Space ICSO, 11 October 2012 Sentinel 5 precursor and the TROPOMI payload Climate and Air quality Precursor
More informationThe Space-based Telescopes for Actionable Refinement of Ephemeris (STARE) mission
LLNL-PRES-641541 Performance Measures x.x, x.x, and x.x SSC13-XI-11 The Space-based Telescopes for Actionable Refinement of Ephemeris (STARE) mission Vincent Riot, Willem de Vries, Lance Simms, Brian Bauman,
More informationSPD QM Thermal Vacuum Testing
SPD 10003 QM Thermal Vacuum Testing Document Author(s): Seongwhan Lee swhan@khu.ac.kr Responsible Engineer(s): Seongwhan Lee Jungho Lee swhan@khu.ac.kr overthewater@khu.ac.kr Page 1/23 Revision History
More informationPuerto Rico CubeSat NanoRock2 PR-CuNaR2
Puerto Rico CubeSat NanoRock2 PR-CuNaR2 Dr. Amilcar Rincon-Charris Mechanical Engineering Department 2018 Outline Introduction PR-CuNaR2 Components Avionics and Payload Facilities Future work http://bayamon.inter.edu
More informationINTER-AGENCY SPACE DEBRIS COORDINATION COMMITTEE (IADC) SPACE DEBRIS ISSUES IN THE GEOSTATIONARY ORBIT AND THE GEOSTATIONARY TRANSFER ORBITS
INTER-AGENCY SPACE DEBRIS COORDINATION COMMITTEE (IADC) SPACE DEBRIS ISSUES IN THE GEOSTATIONARY ORBIT AND THE GEOSTATIONARY TRANSFER ORBITS Presented to: 37-th Session of the SCIENTIFIC AND TECHNICAL
More informationFIBER OPTIC GYRO-BASED ATTITUDE DETERMINATION FOR HIGH- PERFORMANCE TARGET TRACKING
FIBER OPTIC GYRO-BASED ATTITUDE DETERMINATION FOR HIGH- PERFORMANCE TARGET TRACKING Elias F. Solorzano University of Toronto (Space Flight Laboratory) Toronto, ON (Canada) August 10 th, 2016 30 th AIAA/USU
More informationAn Astrophysics Mission of Opportunity on the International Space Station
GSFC 1 An Astrophysics Mission of Opportunity on the International Space Station Science: Understanding ultra-dense matter through observations of neutron stars in the soft X-ray band Launch: October 2016,
More informationThe Challenge is to Define: System Engineering. System Engineering Components. Functional Requirements
The Challenge is to Define: System Engineering What it is supposed to do How well it must do it It s constituant parts and how they play together We are not prepared for detail design, assembly and test
More informationGLAST Large Area Telescope Monthly Mission Review
GLAST Large Area Telescope Monthly Mission Review Gamma-ray Large Area Space Telescope LAT Flight Software Status May 2, 2007 Jana Thayer Stanford Linear Accelerator Center 1 FSW Status B0-10-1 available
More informationCHAPTER 22 GEOGRAPHIC INFORMATION SYSTEMS
CHAPTER 22 GEOGRAPHIC INFORMATION SYSTEMS PURPOSE: This chapter establishes the administration and use of to improve the quality and accessibility of Department s spatial information and support graphical
More informationA Systems Engineering Approach to Design, Fabrication, and Characterization of a Modern Spacecraft to Study Impact Patterns of Space Debris
A Systems Engineering Approach to Design, Fabrication, and Characterization of a Modern Spacecraft to Study Impact Patterns of Space Debris Ann Dietrich, Sheldon Clark, Mark Werremeyer, and Dr. Norman
More informationExpanding Science with SmallSats/CubeSats
National Aeronautics and Space Administration Expanding Science with SmallSats/CubeSats Outer Planets Analysis Group John D. Baker 2/2/2016 2016, Government Sponsorship Acknowledged National Aeronautics
More informationOrbital Debris Mitigation
Orbital Debris Mitigation R. L. Kelley 1, D. R. Jarkey 2, G. Stansbery 3 1. Jacobs, NASA Johnson Space Center, Houston, TX 77058, USA 2. HX5 - Jacobs JETS Contract, NASA Johnson Space Center, Houston,
More informationM i c r o - C o i l B o a r d A s s e m b l y
M i c r o - C o i l B o a r d A s s e m b l y To meet future space environmental reliability requirements, Jackson and Tull (J&T) is currently developing micro-coil board assembly technology for advanced
More informationLeonid Meteor Observer in LEO: A Proposal for a University Microsatellite for the 2001 Leonids
Leonid Meteor Observer in LEO: A Proposal for a University Microsatellite for the 2001 Leonids Kazuya Yoshida* Hajime Yano** *Tohoku University **Institute of Space and Astronautical Science (ISAS) JAPAN
More informationAUTOMATED FLIGHT DYNAMICS SYSTEM FOR THAICHOTE SATELLITE
IAA-AAS-DyCoSS2-14-11-07 AUTOMATED FLIGHT DYNAMICS SYSTEM FOR THAICHOTE SATELLITE Manop Aorpimai, * Pornthep Navakitkanok and Sujate Jantarang INTRODUCTION In this paper, we present the development of
More informationToshinori Kuwahara*, Yoshihiro Tomioka, Yuta Tanabe, Masato Fukuyama, Yuji Sakamoto, Kazuya Yoshida, Tohoku University, Japan
Toshinori Kuwahara*, Yoshihiro Tomioka, Yuta Tanabe, Masato Fukuyama, Yuji Sakamoto, Kazuya Yoshida, Tohoku University, Japan The 3 rd Nano-Satellite Symposium Micro/Nano Satellite & Debris Issues December
More informationRESERVE THALES ALENIA SPACE CHANGE RECORDS ISSUE DATE DESCRIPTION OF CHANGES AUTHOR
ISSUE : 1 Page : 2/35 CHANGE RECORDS ISSUE DATE DESCRIPTION OF CHANGES AUTHOR 1 03/10/07 Initial issue (MTG-TAF-SA-RS-39) J. VIEILLOT 1 20/09/10 Updated version for kick off : L.OUCHET New reference (MTG-TAF-SA-SS-0039)
More informationPico-Satellite Orbit Control by Vacuum Arc Thrusters as Enabling Technology for Formations of Small Satellites
1/25 Pico-Satellite Orbit Control by Vacuum Arc Thrusters as Enabling Technology for Formations of Small Satellites Igal Kronhaus, Mathias Pietzka, Klaus Schilling, Jochen Schein Department of Computer
More informationA Regional Microsatellite Constellation with Electric Propulsion In Support of Tuscan Agriculture
Berlin, 20 th - 24 th 2015 University of Pisa 10 th IAA Symposium on Small Satellites for Earth Observation Student Conference A Regional Microsatellite Constellation with Electric Propulsion In Support
More informationOptElec: an Optimisation Software for Low-Thrust Orbit Transfer Including Satellite and Operation Constraints
OptElec: an Optimisation Software for Low-Thrust Orbit Transfer Including Satellite and Operation Constraints 7th International Conference on Astrodynamics Tools and Techniques, DLR, Oberpfaffenhofen Nov
More informationChallenging Decisions from a Career in Aerospace. AIAA Huntsville Section Michael D. Griffin 8 August 2017
Challenging Decisions from a Career in Aerospace AIAA Huntsville Section Michael D. Griffin 8 August 2017 Delta 183/Delta Star DoD/SDIO mission to capture phenomenology of rocket plumes on Soviet launch
More informationLunar Discovery and Exploration program
Lunar Discovery and Exploration program Space Policy Directive-1 (December 11, 2017) amends the National Space Policy to include the following paragraph: Lead an innovative and sustainable program of exploration
More informationArtificial Intelligence at the Jet Propulsion Laboratory. Jakub Hajic AI Seminar I., MFF UK
Artificial Intelligence at the Jet Propulsion Laboratory Jakub Hajic 3. 12. 2013 AI Seminar I., MFF UK Talk outline Included: Overview of JPL Current planning systems ASPEN (batch) CASPER (continuous)
More informationStrategic Planning of Tuvalu Meteorological Service
WMO Regional Seminar on Enhancing Service Delivery by National Meteorological & Hydrological Services (NMHSs( NMHSs) ) in RA V Kuala Lumpur, Malaysia, 2 6 April 2007 Strategic Planning of Tuvalu Meteorological
More informationINCA. Ionospheric Neutron Content Analyzer. New Mexico State University University NanoSat-8. CubeSat Workshop Presentation August 2, 2014; Logan, UT
INCA Ionospheric Neutron Content Analyzer New Mexico State University University NanoSat-8 CubeSat Workshop Presentation August 2, 2014; Logan, UT Presentation Outline Mission Overview Mission Relevance
More informationINCA. Ionospheric Neutron Content Analyzer. New Mexico State University University NanoSat-8. CubeSat Workshop Presentation August 2, 2014; Logan, UT
INCA Ionospheric Neutron Content Analyzer New Mexico State University University NanoSat-8 CubeSat Workshop Presentation August 2, 2014; Logan, UT Mission Overview Mission Relevance ConOps INCA Payload
More informationOverview of JAXA Activities on Sustainable Space Development and Space Situational Awareness
Overview of JAXA Activities on Sustainable Space Development and Space Situational Awareness 26 February 2015 Shizuo YAMAMOTO Vice President, JAXA CONTENTS 1. Japan s Space Activities Structure 2. JAXA
More informationSpace mission environments: sources for loading and structural requirements
Space structures Space mission environments: sources for loading and structural requirements Prof. P. Gaudenzi Università di Roma La Sapienza, Rome Italy paolo.gaudenzi@uniroma1.it 1 THE STRUCTURAL SYSTEM
More informationSpace Telescopes Asteroid Mining Space Manufacturing. Wefunder.com/SpaceFab
Space Telescopes Asteroid Mining Space Manufacturing Wefunder.com/SpaceFab Business Road Map Cost efficient high value space telescopes Unique business model Deployable optics technology Asteroid mining
More informationPAYLOAD ORBITAL DELIVERY SYSTEM (PODS) The Payload Orbital Delivery System (PODS) enables frequent, cost-effective access to near GEO for SmallSats
PAYLOAD ORBITAL DELIVERY SYSTEM (PODS) The Payload Orbital Delivery System (PODS) enables frequent, cost-effective access to near GEO for SmallSats /sslmda PAYLOAD ORBITAL DELIVERY SYSTEM (PODS) Mission
More informationMars Sample Return Mission
Mars Sample Return Mission Ryan Supler Saylor.org: SSE101 MSRM Project April 15, 2014 2 Table of Contents The Scoping Elements of the Mars Sample Return Mission page 3 The High-Level Concept of Operations
More informationSub-millimeter size debris monitoring system with IDEA OSG 1
Sub-millimeter size debris monitoring system with IDEA OSG 1 Masahiko Uetsuhara, Mitsunobu Okada, Yasunori Yamazaki, Astroscale Pte. Ltd. Toshiya Hanada Kyushu University ABSTRACT The 20-kg class microsatellite
More informationORBITA.PRO COMPLEX ITERATIVE DESIGN OF SPACE SYSTEMS
ORBITA.PRO COMPLEX ITERATIVE DESIGN OF SPACE SYSTEMS In 2016, more than 200 spacecrafts weighing less than 50 kg were sent into orbit. Google, SpaceX, OneWeb, and Iridium already develop and deploy constellations
More informationHow to Improve Small Satellite Missions in Two Easy Steps:
How to Improve Small Satellite Missions in Two Easy Steps: Adopting Space Debris Mitigation Guidelines and Improving Space Surveillance Network Tracking Support G. Taft DeVere Jason C. Randolph Headquarters
More informationTracking the Relative Motion of Four Space Payloads Launched from a Sub- Orbital NASA Rocket
Tracking the Relative Motion of Four Space Payloads Launched from a Sub- Orbital NASA Rocket Hugh Martell Waypoint Consulting Inc. Barton Bull NASA Goddard Space Flight Center BIOGRAPHIES Mr. Martell is
More informationThe 2007 CubeSat Developers' Workshop SwissCube Project
SwissCube Project (http://swisscube.epfl.ch) The 2007 CubeSat Developers' Workshop SwissCube Project Guillaume Roethlisberger Mechanical System Engineer Space Center EPFL guillaume.roethlisberger@epfl.ch
More informationLong-wave infrared imaging spectroscopy from small satellite and UAV platforms
Long-wave infrared imaging spectroscopy from small satellite and UAV platforms Robert Wright, Paul Lucey, Sarah Crites, Mark Wood, Harold Garbeil, Eric Pilger Hawai'i Institute of Geophysics and Planetology,
More informationLOTNAV. A Low-Thrust Interplanetary Navigation Tool: The Trajectory Reconstruction Module
LOTNAV A Low-Thrust Interplanetary Navigation Tool: The Trajectory Reconstruction Module Juan Luis Cano González Mission Analysis Division Deimos Space S.L. -1- The LOTNAV Tool The Low-Thrust Interplanetary
More informationPlanetary Science Big Data
Planetary Science Big Data Michael H. New, Ph.D. Planetary Data System Program Scientist 16 Feb 2016 NASA Ad Hoc Big Data Task Force 1 PSD Data Policies All science data returned from NASA missions are
More informationThe Interstellar Boundary Explorer (IBEX) Mission Design: A Pegasus Class Mission to a High Energy Orbit
The Interstellar Boundary Explorer (IBEX) Mission Design: A Pegasus Class Mission to a High Energy Orbit Ryan Tyler, D.J. McComas, Howard Runge, John Scherrer, Mark Tapley 1 IBEX Science Requirements IBEX
More informationOperational Support by ESOC s GRAS Ground Support Network - Status and Outlook
ESA UNCLASSIFIED Releasable to the public Operational Support by ESOC s GRAS Ground Support Network - Status and Outlook R. Zandbergen, F.Wollenweber, C.Marquardt, W. Enderle and the ESOC and EUMETSAT
More information