CubeSat Flight Control Software
|
|
|
- Marlene Stokes
- 5 years ago
- Views:
Transcription
1 CubeSat Flight Control Software Senior Project Dan Turner Colin Myers
2 Project Description Flight Control Software for Vermont Techs CubeSat Scheduled to launch in September of 2013 Purpose: Test onboard subsystems & a SPARK implementation of GEONS Future Goal: Send a CubeSat to the moon to either orbit or land on it. The completed CubeSat design will be used to replicate additional CubeSats for future missions.
3 Student Involvement 2011 (Summer) Jeremy Audet & Matt Ward started the flight control software 2012 (Summer) Dan Turner picked up where Matt and Jeremy left off with the flight control software 2012 (Fall) Michael Collins and Colin Myers started working on the flight control software 2013 (Spring) India Beauregard helped develop the IMU board
4 Other Acknowledgements Carl Brandon- Principal Investigator Peter Chapin- Software Director Carl Wolf - Helped with designing the IMU board Oliver Piluski (LED Dynamics) - Helped with the development and printing of the IMU board Barry Trutor (Microstrain) - Helped with IMU integration Rob Devarney - Is currently assisting with the Ground Control
5 What is a CubeSat? "CubeSats are a class of research spacecraft called nanosatellites. The cube-shaped satellites are approximately four inches long, have a volume of about one quart and weigh about 3 pounds." --NASA
6
7 Hardware Requirements Hardware consist of: Camera Inertial Measurement Unit (IMU) GPS Power Supply Radio MSP430 processor SD Card Antenna
8 Software Requirements The Antenna must be deployed no sooner than 45 minutes after the CubeSat is ejected from the rocket The Radio must send a beacon every minute if there is no communication with the Ground Control The File System must store telemetry data, error logs, and images on a SD card The Camera, GPS and IMU must save telemetry data to the file system The Power Supply must report battery status when requested All Flight Control Software must be written in SPARK/Ada
9 Flight Control Software
10 What is SPARK/Ada? SPARK is a formally-defined computer programming language based on Ada, intended to secure and support the development of high integrity software used in applications where predictable and highly reliable operation is essential -- Wikipedia (SPARK programming language)
11 Why Use SPARK? If the software fails, we will lose the satellite Ada offers a greatly improved probability of error-free software when compared with C. Most other CubeSat projects use the C Programming Language. SPARK uses static analysis to prove our code free of run-time errors.
12
13 Software Development Process There is no Ada compiler for our Texas Instruments MSP430 series processor In order to resolve this dilemma we must convert our Ada code to ANSI C with AdaMagic.
14 Software Development Process Software is written in SPARK/Ada using AdaCore s GNAT Programming Studio (GPS) Checked with the Praxis High Integrity Systems SPARK Toolset Compiled and checked with AdaCore s GNAT Pro compiler Sofcheck s AdaMagic compiler front end is used to produce ANSI C as the intermediate code Rowley s Crossworks C cross compiler for Texas Instruments MSP430 CPU produces the object code
15 Software Development Process
16 System Design
17 System Design
18 System Design
19 Subsystems
20 Superloop/Subsystem Interaction
21 Superloop/Subsystem Interaction
22 Superloop/Subsystem Interaction
23 Superloop/Subsystem Interaction
24 Superloop/Subsystem Interaction
25 Superloop/Subsystem Interaction
26 Superloop/Subsystem Interaction
27 Superloop/Subsystem Interaction
28 Components: IMU Camera (with camera shutoff circuitry) GPS Antenna Hysteresis Rods Antenna I 2 C lines 6 headers of LEDs Custom IMU Board
29 Custom IMU Board
30 Custom IMU Board
31 Custom IMU Board
32 Custom IMU Board
33 Custom IMU Board
34 Custom IMU Board
35 Custom IMU Board
36 Software Completion
37 Software Completion
38 Spark Examinable Software
39 Current Status The CubeSat hardware is complete and has passed the ShakeN Bake Other than the GPS and some miscellaneous protocol procedures, the flight control system is done, although it could use more Spark testing. We're currently working on setting up a ground control station for our launch at the end of September.
40 Maybe some pictures and stuff
41
42 Maybe some pictures and stuff
43 Dan Turner Colin Myers Questions?
11 th Annual CubeSat Developers Workshop
11 th Annual CubeSat Developers Workshop NearSpace Launch, Inc. Satellite Globalstar Products: Technology, Service, and Education TSAT Communication First Results EyeStar: A Paradigm Shift 25 // 04 //
RAPTR SAT-X. University of Northern Colorado. Conceptual Design Review. Shiely, Woods, Aken, Adamson 10/4/2011
RAPTR SAT-X Conceptual Design Review University of Northern Colorado Shiely, Woods, Aken, Adamson 10/4/2011 Mission Overview - Mission Statement The RAPTR SAT-X team intends to develop a highly reliable,
Simple attitude visualization tool for satellite operations
Simple attitude visualization tool for satellite operations Franck M. Chatel * and Herbert Wuesten DLR - GSOC, Wessling, 82234, Germany Gabriel Mihail LSE, Darmstadt, 64293, Germany The attitude data delivered
(Capstone-High Altitude Balloon) EE 476
CAP-HAB (Capstone-High Altitude Balloon) EE 476 Jad Lutfi Andrew Prosory Rob Hough Rob Conant Rob Hough High Altitude Research Balloon Overview Project Overview Problem Statement System Diagram Design
Absolute Horizontal Accuracies of Pictometry s Individual Orthogonal Frame Imagery
A Pictometry International, Corp White Paper Absolute Horizontal Accuracies of Pictometry s Individual Orthogonal Frame Imagery Michael J. Zoltek VP, Surveying & Mapping Pictometry International, Corp
Development of Generic Ground Systems by the Use of a Standard Modeling Method. Takahiro Yamada JAXA/ISAS March 1, 2005
Development of Generic Ground Systems by the Use of a Standard Modeling Method Takahiro Yamada JAXA/ISAS March 1, 2005 1 Purpose of This Presentation To explain how spacecraft can be virtualized by using
mypocketqub.com an open source nano-satellite project Michael Johnson 2010 CubeSat Developers Summer Workshop
mypocketqub.com an open source nano-satellite project Michael Johnson michael@mypocketqub.com 2010 CubeSat Developers Summer Workshop a JA initiative in association with Logan, Utah, USA August 7-8, 2010
'Smartphone satellite' developed by Surrey space researchers
Press Release 24th January 2011 'Smartphone satellite' developed by Surrey space researchers Space researchers at the University of Surrey and Surrey Satellite Technology Limited (SSTL) have developed
OCSD-A / AeroCube-7A Status Update
OCSD-A / AeroCube-7A Status Update Darren Rowen Richard Dolphus Patrick Doyle Addison Faler April 20, 2016 2016 The Aerospace Corporation Agenda Concept of Operations Overview Spacecraft Configuration
Boeing s CubeSat TestBed 1 Attitude Determination Design and On Orbit Experience. Michael Taraba Primary Author, Former Employee of the Boeing Company
SSC9 X 6 Boeing s CubeSat TestBed 1 Attitude Determination Design and On Orbit Experience Michael Taraba Primary Author, Former Employee of the Boeing Company Christian ; Senior Embedded Software Engineer
GSAW The Earth Observing System (EOS) Ground System: Leveraging an Existing Operational Ground System Infrastructure to Support New Missions
GSAW 2016 The Earth Observing System (EOS) Ground System: Leveraging an Existing Operational Ground System Infrastructure to Support New Missions David Hardison NASA Goddard Space Flight Center Johnny
New Space, small and pocket spacecraft
New Space, small and pocket spacecraft Chris Brunskill 01 July 2016 What is New Space? Nano and microsatellites provide easy access to space, trading reduced costs for greater risks Cost reduction The
A Constrained Attitude Control Module for Small Satellites
A Constrained Attitude Control Module for Small Satellites Henri Kjellberg and E. Glenn Lightsey The University of Texas at Austin Small Satellite Conference Logan, Utah August 14, 2012 Motivation for
Remote Programming. Michaël Friess Technical Sales Manager. Ada-Europe 2006, Porto June 6,
Presentation cover page EU Remote Programming Michaël Friess Technical Sales Manager Ada-Europe 2006, Porto June 6, 2006 www.adacore.com From Servers to Clients 1 server shared by several users (sequential)
Example of Technology Development Program
Example of Technology Development Program SSTDM 2014 IISC, Bangalore, India April 1, 2014 Dr. Marco Villa CANEUS Small Satellites Director Tyvak VP Space Vehicle Systems Ground rules Power and Volume are
Inserting Core Flight System
Lockheed Martin Space Systems Company Inserting Core Flight System Ryan Slabaugh Michael Phillips Andrew Wobido Rob Chambers October 2015 2015 Lockheed Martin Corporation. All Rights Reserved. 1 Outline
Team A.E.M.B.L. Critical Design Review
Critical Design Review Members: Nick Bradley, Matt Lenda, Emil Reinovsky, Spencer Sator (Student Leader), Kevin Weber GPS System Designer and Team Leader: Stephan Esterhuizen 23 March 2006 Image from http://www.pparc.ac.uk/nw/comet_hi.jpg
TOPOGRAPHY - a LIDAR Simulation
Title TOPOGRAPHY - a LIDAR Simulation Grade Level(s): 9-12 Estimated Time: 1.5 hours Discussion of Technology: Appendix A Construction Details: Appendix B MSDE Indicator(s) Goal 1: Skills and Processes
Enabling technologies for downstream services. Steve Greenland Clyde Space Ltd
Enabling technologies for downstream services Steve Greenland Clyde Space Ltd Clyde Space view: needs of downstream developers 1. Standardised, modular, and reusable building blocks for satellite development
Responsive Flight Software Development & Verification Techniques for Small Satellites
Responsive Flight Software Development & Verification Techniques for Small Satellites Darren Rowen The Aerospace Corporation Vehicle Systems Division 9 November 2012 The Aerospace Corporation 2012 Overview
The Geostationary Operational Satellite R Series (GOES-R) SpaceWire Implementation
The Geostationary Operational Satellite R Series (GOES-R) SpaceWire Implementation Session: SpaceWire Missions and Applications William H. Anderson NASA Goddard Space Flight Center/MEI Technologies E-mail:
SEMWO 2014 Vilnius / Lithuania Inflatable Shape Changing Colonies Assembling Versatile Smart Space Structures
Image Source: NASA SEMWO 2014 Vilnius / Lithuania Inflatable Shape Changing Colonies Assembling Versatile Smart Space Structures Slide 1 Inflatable Shape Changing Colonies Assembling Versatile Smart Space
S-1Rocket Program. ~the final stage in 2011~ Team Kansai Rocket Club. Team Kansai Rocket Club since 2009 ~Striving for Space & People~
S-1Rocket Program ~the final stage in 2011~ Team Kansai Rocket Club Contents Summary of the S-1 Rocket Program Result and analysis of experiments Conclusion Summary of the S-1 Rocket Program Propose of
Introducing ubo 1. Build your ubo 5. Parts List Build Guide - 7-8
Welcome To SPACE Introducing ubo 1 Build your ubo 5 Parts List Build Guide - 7-8 Introducing The ubo kit is a satellite you can build yourself. This guide will give you all the information you need to
Design of Telemetry in Student Imaging Satellite
Design of Telemetry in Student Imaging Satellite Dinesha H A, Dr.V.K Agrawal Dept. of Information Science and Engineering, PESIT, Bangalore, India-560085 Dept. of Information Science and Engineering, PESIT,
Mission Overview Cal Poly s Design Current and future work
Click to edit Master title style Table Click of to Contents edit Master title style Mission Overview Cal Poly s Design Current and future work 2 Mission Click to Overview edit Master title style Main Mission:
Added support for version matching between DJI Assistant 2 and flight control system.
Date : 2017.01.18 DJI GO App Version : ios V 3.1.2, Android V 3.1.1 DJI Assistant 2 Version : 1.0.9-2 Flight Controller Firmware Version : 1.7.0.0 Added support for version matching between DJI Assistant
CelestLabX: CelestLab s extension module
ScilabTEC CelestLabX: CelestLab s extension module Alain Lamy, CNES Alain.Lamy@cnes.fr 16 May 2014 Space Flight Dynamics mission design at CNES Agenda What tools for mission design? -> What makes Scilab
Phantom 2 Reference Guide
Phantom 2 Reference Guide Contents Section 1: Operation and Preparing for Flight. 2 Transmitter introduction 2 Controlling the Drone 2 Turning on the Transmitter 3 Range Extender 3 Basic Drone Parts 4
Nanosatellite Communication Constellation Testbed for Autonomous Scheduling Algorithms to Enable Mission Performance Analysis and Demonstration
SSC17-S2-07 Nanosatellite Communication Constellation Testbed for Autonomous Scheduling Algorithms to Enable Mission Performance Analysis and Demonstration Alonzo E. Jenkins, Peter J. Yoo, and Cherry Y.
New Tools for Spacecraft Simulator Development
New Tools for Spacecraft Simulator Development March. 2007 Page 1 Why use Simulators? Replace the Spacecraft Support to design Support to testing replacement of real equipment in destructive or expensive
Spacecraft Communications Payload (SCP) for Swampworks
Spacecraft Communications Payload (SCP) for Swampworks Joseph A. Hauser Praxis, Inc. 2550 Huntington Avenue Suite 300 Alexandria, VA 22303 phone: (703) 682-2059 fax: (703) 837-8500 email: hauserj@pxi.com
Terrestrial GPS setup Fundamentals of Airborne LiDAR Systems, Collection and Calibration. JAMIE YOUNG Senior Manager LiDAR Solutions
Terrestrial GPS setup Fundamentals of Airborne LiDAR Systems, Collection and Calibration JAMIE YOUNG Senior Manager LiDAR Solutions Topics Terrestrial GPS reference Planning and Collection Considerations
Practical Development of Safe, Secure, Reliable Embedded Software
ARM TechCon 2017 Practical Development of Safe, Secure, Reliable Embedded Software Pat Rogers rogers@adacore.com Why Safe, Secure, or Reliable? Your car could crash Your flight could crash Your medical
Patching Flight Software on Mars
Patching Flight Software on Mars Ed Benowitz / Mark Maimone MSL Flight Software Developers NASA/Jet Propulsion Laboratory California Institute of Technology Copyright 2015 California Institute of Technology.
WELCOME Mobile Applications Testing. Copyright
WELCOME Mobile Applications Testing 1 Mobile Applications Testing List of MUST HAVE to survive this class Required Google Drive account Google email Flash Drive Mobile Phone (iphone/android) Desired Have
KhalifaSat: Mission Overview
KhalifaSat: Mission Overview 1 Introduction to EIAST Emirates Institution for Advanced Science and Technology Government entity based in Dubai, UAE Established in 2006 Vision To be recognized globally
Digital electronics & Embedded systems
FYS3240 PC-based instrumentation and microcontrollers Digital electronics & Embedded systems Spring 2017 Lecture #10 Bekkeng, 30.1.2017 Embedded systems An embedded system is a special-purpose system designed
KUMU A O CUBESAT TELECOMMUNICATION SUBSYSTEM INTEGRATION AND TESTING
KUMU A O CUBESAT TELECOMMUNICATION SUBSYSTEM INTEGRATION AND TESTING Dennis D. Dugay Department of Electrical Engineering University of Hawai i at Mānoa Honolulu, HI 96822 ABSTRACT The Kumu A o CubeSat
ALL STAR Payload Interface Control Document Outline ALL STAR-SYS.402.3
1 ALL STAR Payload Interface Control Document Outline ALL STAR-SYS.402.3 Revision Date Authored By Description 0 7/9/10 Jessica Brown Initial Release 1 1/4/11 Jessica Brown Riley Pack Additional Details
STRAST. UPMSat-2 On-board computers. Grupo de Sistemas de Tiempo Real y Arquitectura de Servicios Telemáticos Universidad Politécnica de Madrid.
On-board computers Grupo de Sistemas de Tiempo Real y Arquitectura de Servicios Telemáticos Universidad Politécnica de Madrid dit UPM Computers in spacecraft Computers are used on board of spacecraft for
Implementation of a Middleware Based Ground System March 2, 2005, GSAW2005 Conference
Implementation of a Middleware Based Ground System March 2, 2005, GSAW2005 Conference Presented By Everett Cary Emergent Space Technologies, Inc. Teammates NASA GMSEC NASA SSMO Honeywell Technology Solutions,
UCSD AUVSI Unmanned Aerial System Team. Joshua Egbert Shane Grant
UCSD AUVSI Unmanned Aerial System Team Joshua Egbert Shane Grant Agenda Project background and history System design overview Gimbal Stabilization Target Recognition Lessons Learned Future Work Q&A UCSD
Building High Integrity Applications with Spark
Building High Integrity Applications with Spark Software is pervasive in our lives. We are accustomed to dealing with the failures of much of that software restarting an application is a very familiar
JEM Internal Ball Camera (Int-Ball)
JEM Internal Ball Camera (Int-Ball) July 14, 2017 Japan Aerospace Exploration Agency 1 Objective of Project Currently, when working in the Japanese Experiment Module ( Kibo ), the crew (astronaut) often
Communications on Board (COB):
Communications on Board (COB): Turn-Key Command, Data Handling, and Communications. Andrew Strange,Taylor University Faculty Advisor: Dr. Will Holmes 20 th Annual AIAA/USU Conference on Small Satellites
Development of Formation Flight and Docking Algorithms Using the SPHERES Testbed
Development of Formation Flight and Docking Algorithms Using the Testbed Prof. David W. Miller MIT Allen Chen, Alvar Saenz-Otero, Mark Hilstad, David W. Miller Introduction : Synchronized Position Hold
CCSDS and NASA Standards for Satellite Control Network Interoperability
InterPlanetary Network & Information Systems Directorate CCSDS and NASA Standards for Satellite Network Interoperability Peter Shames Jet Propulsion Laboratory California Institute of Technology The Fundamental
ARCHITECTURE STUDY FOR FUTURE AIR FORCE SATELLITE CONTROL NETWORK
ARCHITECTURE STUDY FOR FUTURE AIR FORCE SATELLITE CONTROL NETWORK -PRELIMINARY INVESTIGATION- GSAW February, 2001 Prepared By CARL SUNSHINE, TIEN M. NGUYEN, JOHN C. CHIANG, AND YOGI KRIKORIAN THE AEROSPACE
APPLICATION OF AERIAL VIDEO FOR TRAFFIC FLOW MONITORING AND MANAGEMENT
Pitu Mirchandani, Professor, Department of Systems and Industrial Engineering Mark Hickman, Assistant Professor, Department of Civil Engineering Alejandro Angel, Graduate Researcher Dinesh Chandnani, Graduate
Satellite Attitude Determination
Satellite Attitude Determination AERO4701 Space Engineering 3 Week 5 Last Week Looked at GPS signals and pseudorange error terms Looked at GPS positioning from pseudorange data Looked at GPS error sources,
A Packet Utilisation Standard (PUS) Model
A Packet Utilisation Standard (PUS) Model This is a simulation model of the European Space Agency (ESA) Packet Utilisation Standard (PUS) in an operational environment linking a satellite with ground stations.
Enabling technologies for downstream services. Steve Greenland Clyde Space Ltd
Enabling technologies for downstream services Steve Greenland Clyde Space Ltd CubeSats: from expensive hands-on training through useful science to killer (downstream) applications? Hands-on training Useful
State of the Satellite Industry Report
State of the Satellite Industry Report August 2011 Sponsored by the Prepared by Futron Corporation SIA Member Companies as of August 2011 2 Study Overview The SIA s 14 th annual comprehensive study of
UKube-1: A Multi-Payload Technology Demonstration Platform. Ritchie Logan, Steve Greenland, Clyde Space Ltd
UKube-1: A Multi-Payload Technology Demonstration Platform Ritchie Logan, Steve Greenland, Clyde Space Ltd Outline 1. Timeline and functional overview 2. Payload Details & Management 3. Enabling Rapid
ROSCOSMOS. Current State of the Russian Space Program and National Space Industry
Current State of the Russian Space Program and National Space Industry October 2016 Key Events Defining the Future of National Spaceflight July 13 th, 2015: The Law on Roscosmos State Corporation is signed
RAPID RECONNAISSANCE AND RESPONSE (R 3 ) THERMAL ALGORITHMS. Nathalie Vedie. Technical documentation to support the detailed design of:
RAPID RECONNAISSANCE AND RESPONSE (R 3 ) THERMAL ALGORITHMS by Nathalie Vedie Technical documentation to support the detailed design of: R 3 Mission Center for Space Systems Georgia Institute of Technology
Developing onboard software 400 miles from the cleanroom
Developing onboard software 400 miles from the cleanroom Component-based reusable software for UKube-1 Peter Mendham and Mark McCrum UKube-1 United Kingdom Universal Bus Experiment 3U CubeSat Five payloads
Improving a Satellite Mission System by means of a Semantic Grid Architecture
Improving a Satellite Mission System by means of a Semantic Grid Architecture Manuel Sánchez-Gestido 1, María S. Pérez-Hernández 2, Rafael González-Cabero 3, Asunción Gómez-Pérez 3 1 Deimos Space S.L.,
K. E. G. S. KOMPUTER ENTHUSIASTS OF GREATER SEATTLE
April, 2013 Volume 17, Issue 04 TAPPING THE K. E. G. S. KOMPUTER ENTHUSIASTS OF GREATER SEATTLE Prez Says: We are now into April and with it hopefully the beginning of things being drier and warmer. So
EXPERIMENTAL VALIDATION OF STAR-CCM+ FOR LIQUID CONTAINER SLOSH DYNAMICS
EXPERIMENTAL VALIDATION OF STAR-CCM+ FOR LIQUID CONTAINER SLOSH DYNAMICS Brandon Marsell a.i. solutions, Launch Services Program, Kennedy Space Center, FL 1 Agenda Introduction Problem Background Experiment
Optimizing Bandwidth Utilization in Packet Based Telemetry Systems
Optimizing Bandwidth Utilization in Packet Based Telemetry Systems Jeffrey R. Kalibjian Lawrence Livermore National Laboratory Keywords bandwidth utilization, intelligent telemetry processing Abstract
Appendix Q. Modelling of complex satellite manoeuvres with ESATAN-TMS. Nicolas Bures (ITP Engines UK Ltd, United Kingdom)
227 Appendix Q Modelling of complex satellite manoeuvres with ESATAN-TMS Nicolas Bures (ITP Engines UK Ltd, United Kingdom) 228 Modelling of complex satellite manoeuvres with ESATAN-TMS Abstract Requirements
Bet & MathWorks By Bet Herrera Sucarrat Application Engineer MathWorks
Bet & MathWorks By Bet Herrera Sucarrat Application Engineer MathWorks 2015 The MathWorks, Inc. 1 Researchers Test Control Algorithms for NASA SPHERES Satellites with a MATLAB Based Simulator Challenge
Satellite Tracking System using Amateur Telescope and Star Camera for Portable Optical Ground Station
Satellite Tracking System using Amateur Telescope and Star Camera for Portable Optical Ground Station Hyosang Yoon, Kathleen Riesing, and Kerri Cahoy MIT STAR Lab 30 th SmallSat Conference 8/10/2016 Hyosang
The EDSN Intersatellite Communications Architecture
EDSN - Edison Demonstration for SmallSat Networks The EDSN Intersatellite Communications Architecture Sunday, August 2 nd, 2014 John Hanson Deputy PM/FSW Lead James Chartres Lead Systems Engineer Hugo
DJI MATRICE 600 PRO Release Notes
Date : 2017.10.24 Aircraft Firmware : V 1.0.1.65 DJI GO App : ios V 3.1.18, Android V 3.1.11 DJI Assistant 2 : V 1.1.6 Aircraft Firmware: Increased flight safety. Fixed issue of output error when F channel
IAA-CU Authenticated uplink for the small, low-orbit student satellite NUTS
IAA-CU-13-13-01 Authenticated uplink for the small, low-orbit student satellite NUTS Bram Bezem & Per Kristian J. Fjellby, Roger Birkeland, Stig F. Mjølsnes Norwegian University of Science and Technology
More processing power - Driving requirements
Software More processing power - Driving requirements Autonomy Task based commanding / resource management rather than timeline remote control E.g. planetary rovers drive from A B, look out for interesting
Project and Diploma Thesis Topics in DAAS
Intermediate Project (P) Engineering Diploma Thesis (E) Master Diploma Thesis (M) Project and Diploma Thesis Topics in DAAS - 2018 Prof Janusz Narkiewicz Below there are areas of topics to be clarified
Advanced On-board Control Procedure
1 Overview The Advanced On-Board Control Procedure (AOBCP) product is one of a set of technologies that allows to implement cost effective operation and control of a spacecraft. Together these technologies
Space Mission Communications Security
Space Mission Communications Security Nick Shave, Gavin Kenny Logica UK Limited Howard Weiss SPARTA Inc James Stanier DERA GSAW 2001 1 Presentation Overview Background and Security Issues Space Mission
Mohammed Bin Rashid Space Centre.
Mohammed Bin Rashid Space Centre Introduction to MBRSC Started as Emirates Institution for Advanced Science and Technology (EIAST) which was established in February 2006. On April 18th, 2015: a decree
Alexi Glover & Juha-Pekka Luntama SSA Programme Space Weather Segment, OPS-L ESA/ESAC, Madrid, Spain
Alexi Glover & Juha-Pekka Luntama SSA Programme Space Weather Segment, OPS-L ESA/ESAC, Madrid, Spain Presentation Outline 1. SSA Programme short introduction 2. SWE Service Domains 3. Precursor Services
SINGLE MODULAR ON-BOARD COMPUTER FOR SPACE APPLICATIONS
APPLICATIONS Jonathan William de Holanda, jholanda@equatorialsistemas.com.br Benjamin Gilles Nicolas Boglietti, bboglietti@equatorialsistemas.com.br Sidney L. A. Carrara, scarrara@equatorialsistemas.com.br
Overview of the Trimble TX5 Laser Scanner
Overview of the Trimble TX5 Laser Scanner Trimble TX5 Revolutionary and versatile scanning solution Compact / Lightweight Efficient Economical Ease of Use Small and Compact Smallest and most compact 3D
INITIAL RESULTS OF A LOW-COST SAR: YINSAR
INITIAL RESULTS OF A LOW-COST SAR: YINSAR Richard B. LUNDGREEN, Douglas G. THOMPSON, David V. ARNOLD, David G. LONG, Gayle F. MINER Brigham Young University, MERS Laboratory 459 CB, Provo, UT 84602 801-378-4884,
r bulletin 96 november 1998 bull
Figure 1. The XMM spacecraft the xmm simulator The XMM Simulator - The Technical Challenges H. Côme Simulation Section, ESA Directorate of Technical and Operational Support, ESOC, Germany M. Irvine Vega
NASA s Laser Communications Terminal Technologies for 2017 and Beyond. David Israel, LCRD Principal Investigator NASA Goddard Space Flight Center
NASA s Laser Communications Terminal Technologies for 2017 and Beyond David Israel, LCRD Principal Investigator NASA Goddard Space Flight Center 1 2 2013: NASA s First, Historic Lasercom Mission The Lunar
Blue Canyon Technologies XB1 Enabling a New Realm of CubeSat Science. George Stafford BCT Range St, Suite 200 Boulder, CO 80301
Blue Canyon Technologies XB1 Enabling a New Realm of CubeSat Science George Stafford BCT 720.458.0703 1600 Range St, Suite 200 Boulder, CO 80301 About BCT Blue Canyon Technologies is a small business founded
The Space Generation Congress 2010: Perspectives from University Students and Young Professionals in the Space Sector
The Space Generation Congress 2010: Perspectives from University Students and Young Professionals in the Space Sector The Space Generation Advisory Council in Support of the UN programme on Space Applications
1/8/2013. Not one, single technology, rather a convergence of several technologies Systems for:
Tracking Technologies Priscilla ill Grantham, Esq. Sr. Research Counsel National Center for Justice and the Rule of Law Copyright 2012 Priscilla Grantham & National Center for Justice and the Rule of Law
NanoPower BPX. Datasheet High-capacity battery pack for nano-satellites
NanoPower BPX Datasheet High-capacity battery pack for nano-satellites 1 Table of Contents 1 TABLE OF CONTENTS... 2 2 OVERVIEW... 3 2.1 HIGHLIGHTED FEATURES... 3 2.2 CUSTOMIZATION OPTIONS... 3 2.3 MEASUREMENTS...
Building Software Architecture using Architectural Design Patterns
Building Software Architecture using Architectural Design s U.V.R. Sarma Department of CSE CVR College of Engg. Ibrahimpatan(M), R.R. District, A.P., India Neelakantam Pavani Department of IT CVR College
Telemetry Processing and Display Ground System
The MPCS Multimission Telemetry Processing and Display Ground System Its Use in the Mars Science Laboratory Mission and Beyond Josh Choi, Lloyd Deforrest, Marti DeMore Jet Propulsion Laboratory California
Implementing Onboard Data Compression for the Van Allen Probes
Implementing Onboard Data Van Allen Probes Compression for the Van Allen Probes Mark Reid Johns Hopkins University, Applied Physics Lab Mark.Reid@jhuapl.edu 1 Agenda Introduction Rationale for Adding Compression
Moses Jones Application Note ECE 480 Design Team 7 Programming Altimeters. Using MSP 430 Launch Pad 11/8/2013
Moses Jones Application Note ECE 480 Design Team 7 Programming Altimeters Executive Summary Using MSP 430 Launch Pad 11/8/2013 This document will provide a guide of how to use the MSP 430 Launch Pad while
A Reference Architecture for Payload Reusable Software (RAPRS)
SAND2011-7588 C A Reference Architecture for Payload Reusable Software (RAPRS) 2011 Workshop on Spacecraft Flight Software Richard D. Hunt Sandia National Laboratories P.O. Box 5800 M/S 0513 Albuquerque,
SPARKSkein A Formal and Fast Reference Implementation of Skein
SPARKSkein A Formal and Fast Reference Implementation of Skein Rod Chapman, Altran Praxis Copyright Altran Praxis Agenda The big idea What is Skein? Coding SPARKSkein Results The release Conclusions and
On-Orbit Testing of Target-less TriDAR 3D Rendezvous and Docking Sensor
On-Orbit Testing of Target-less TriDAR 3D Rendezvous and Docking Sensor Stephane Ruel, Tim Luu, Andrew Berube* *Neptec Design Group, Canada e-mail: sruel@neptec.com Abstract TriDAR is a vision system developed
Visual Land V TOUCH PRO
Visual Land V TOUCH PRO Information in this manual are subject to change without notice. FEATURES 2.8 inch wide touch screen, 320X240 dot matrix full color high speed TFT screen Support MP3, WMA, RA, WAV
Deep Impact. Project Data Management Plan
Deep Impact Project Data Management Plan Document Number D - 21386 Jet Propulsion Laboratory California Institute of Technology Pasadena, California 91109-8099 Deep Impact Project Data Management Plan
SICON Smart Sensors Role in Integrated System Health Management
SICON 2005 Smart Sensors Role in Integrated System Health Management Jose M Perotti, Instrumentation Group Lead Command, Monitoring and Control Branch Spaceport Engineering &Technology Directorate, Kennedy
OrigamiSat GHz Downlink Data Format. (English version)
OrigamiSat-1 5.84GHz Downlink Data Format (English version) Document# OP-S1-0117 Revision Ver. 1.1 Date 2019/01/11 Name Tokyo Tech OrigamiSat-1 project team 1 Revision history Date Version Content 2019/01/11
Heliophysics Python Plan
Heliophysics Python Plan Russell A. Stoneback Center for Space Sciences Photon Audio Lab The University of Texas at Dallas 27 July 2018 Snakes on a Spaceship: The Return of the Python Motivation Developing
GOES-R Update Greg Mandt System Program Director
GOES-R Update Greg Mandt System Program Director GOES User Conference 3 Nov 2009 1 Continuity of Geostationary Operational Satellite Programs Calendar Year As of October 30, 2009 07 08 09 10 11 12 13 14
Small Satellite Conference 2014 Using Rules-based Statecharts to Automate Satellite Behaviors
Using Rules-based Statecharts to Automate Satellite Behaviors Kenneth Center, PhD Director of Advanced Software Technologies PnP Innovations Ken.Center@PnPInnovations.com Outline Background (AMM and Aspire)
The potential uses of UAV-based remote sensing in the Great Lakes
The potential uses of UAV-based remote sensing in the Great Lakes Ben Vander Jagt Doug Alsdorf Satellite Hydrology and Remote Sensing The Ohio State University Great Lakes Workshop Series on Remote Sensing
Sanitizing Sensitive Data: How to get it Right (or at least Less Wrong ) Roderick Chapman, 22nd September 2017
Sanitizing Sensitive Data: How to get it Right (or at least Less Wrong ) Roderick Chapman, 22nd September 2017 Contents The problem Technical issues Design goals Language support A policy for sanitization
Mesh Network Architecture for Enabling Inter-Spacecraft Communication
SSC17-VII-10 Mesh Network Architecture for Enabling Inter-Spacecraft Communication Christopher Becker, Garrick Merrill NASA Marshall Space Flight Center Mail Stop EV42, Huntsville, AL 35812 chris.becker@nasa.gov