ASCENTIS: Planetary Ascent Vehicle FES Tool
|
|
- Eric Simon Wilkerson
- 6 years ago
- Views:
Transcription
1 ASCENTIS: Planetary Ascent Vehicle FES Tool Eugénio Ferreira, Thierry Jean-Marius Mission analysis & GNC teams 3rd International Workshop on Astrodynamics Tools and Techniques ESTEC, 4 October 2006 Page 1
2 Outline Simulation Tool objectives Architecture and models Simulator usage Simulation outcomes Conclusion Page 2
3 ASCENTIS objectives Developed within ESA TRP PAV GNC in partnership with Scisys Assess concept performances during ascent GNC algorithms integrated in closed loop Validation of GNC architecture & coupling effects 6-dof Non Real Time platform, built on Matlab/Simulink Representative: involves deviations on both vehicle & environment Operating modes: unitary cases / Monte-Carlo analysis Modular and expandable, Graphical User Interface Page 3 Based on ATPE framework Compatible with Real Time environment, existing Library modules used
4 Considered Missions & Vehicles Mars ascent phase, up to circular orbit 3 boosted phases 1 long coasting phase, before circularisation Mars Sample Return 500 km circular orbit 2-stages, liquid Mars Manned Mission km circular orbit 1½-stage, liquid 3rd Intl Workshop on Page 4
5 Top Level Architecture of the FES GNC Page 5
6 FES models Spacecraft Propulsion Engine Management Attitude Control System Thrust Vector Control Aerodynamics Each stage modelled Page 6 Mass and Inertia Evolution Centring and Inertia Fuel Sloshing Mass Evolution
7 FES models Dynamics & Environment 6-dof Dynamics Translational Dynamics Rotational Dynamics Mars Gravity Model Simple 3rd order Complex n th order gravitational harmonics based on JPL50c Page 7 Mars atmosphere Model Look-up tables from EMCD 3.1 EMCD 3.1 interface directly embedded in FES
8 FES models Sensors Inertial Measurement Unit 3-axis accelerometer 3-axis gyrometer Alignment Matrix Page 8
9 FES generic models management Ascent profile induces required dedicated management Page 9
10 FES models GNC GNC algorithms Alignement/Navigation Inertial Coast arcs Ascent Guidance trades-off Linear tg Pred-cor F(vel) Ascent Control Hinf LQG Eigen value placement Page 10 C-coded S-functions
11 GNC sequencing example 1 st Boost 2 nd Boost Coasting phase 3 rd Boost Coasting phase 1st Stage 2nd Stage Navigation Guidance TVC control Roll control Attitude control Page 11
12 ASCENTIS usage Page 12 Two ways to run Simulator: Command Line Simple init., navigate to simulator directory & edit set of scripts that manages simulation Plot and analyse results using command line plotting functions GUI Manages scripts in one place Gives selections of mission Loads mission specific files editing User may execute simulations Status displayed in command window Default plotting at the touch of a button
13 FES use example: Guidance trade-off Algorithms comparison through performance index Guidance scheme Implicit Predictor-corrector Explicit 20 m/s requirement 18.5% 86.2% 98.8% 95% value 48.2 m/s 66.7 m/s 1.7 m/s Page 13
14 ASCENTIS plots Default plots run from single script Script manages plotting functions, additional plotting can be added if desired Page 14
15 ASCENTIS plots: Monte-Carlo (1/2) + Guidance X Navigation Page 15 Orbital injection
16 ASCENTIS plots: Monte-Carlo (2/2) Deflection envelope Q.α envelope Page 16
17 Conclusion ASCENTIS is a standalone platform, compatible with both UNIX & WINDOWS environments Fully tested and validated, and RT compliant Easy to use interface GUI or Command driven Page 17 Useful platform to assess performances for a Planetary ascent phase
ATPE Simulator: Simulation Tool for Onboard GNC Development and Validation
ATPE Simulator: Simulation Tool for Onboard GNC Development and Validation Uwe Brüge Uwe Soppa Presented by Eugénio Ferreira GNC & On-board S/W Engineering 3rd ESA Workshop on Astrodynamics Tools and Techniques
More informationFlight-dynamics Simulation Tools
Flight-dynamics Simulation Tools 2 nd ESA Workshop on Astrodynamics Tools and Techniques ESTEC, September 13-15, 2004 Erwin Mooij Introduction (1) Areas of interest (not complete): Load analysis and impact-area
More informationReal-Time AOCS EGSE Using EuroSim and SMP2-Compliant Building Blocks
UNCLASSIFIED Nationaal Lucht- en Ruimtevaartlaboratorium National Aerospace Laboratory NLR Executive summary Real-Time AOCS EGSE Using EuroSim and SMP2-Compliant Building Blocks Environment control torque
More informationThe Evolution of Nano-Satellite Proximity Operations In-Space Inspection Workshop 2017
The Evolution of Nano-Satellite Proximity Operations 02-01-2017 In-Space Inspection Workshop 2017 Tyvak Introduction We develop miniaturized custom spacecraft, launch solutions, and aerospace technologies
More informationPterodactyl: Integrated Control Design for Precision Targeting of Deployable Entry Vehicles
Pterodactyl: Integrated Control Design for Precision Targeting of Deployable Entry Vehicles Dr. Sarah D Souza, Principal Investigator NASA Ames Research Center 15 th International Planetary Probe Workshop
More informationARDUINO BASED CALIBRATION OF AN INERTIAL SENSOR IN VIEW OF A GNSS/IMU INTEGRATION
Journal of Young Scientist, Volume IV, 2016 ISSN 2344-1283; ISSN CD-ROM 2344-1291; ISSN Online 2344-1305; ISSN-L 2344 1283 ARDUINO BASED CALIBRATION OF AN INERTIAL SENSOR IN VIEW OF A GNSS/IMU INTEGRATION
More informationModel Based AOCS Design and Automatic Flight Code Generation: Experience and Future Development
ADCSS 2016 October 20, 2016 Model Based AOCS Design and Automatic Flight Code Generation: Experience and Future Development SATELLITE SYSTEMS Per Bodin Head of AOCS Department OHB Sweden Outline Company
More informationSatellite Testing. Prepared by. A.Kaviyarasu Assistant Professor Department of Aerospace Engineering Madras Institute Of Technology Chromepet, Chennai
Satellite Testing Prepared by A.Kaviyarasu Assistant Professor Department of Aerospace Engineering Madras Institute Of Technology Chromepet, Chennai @copyright Solar Panel Deployment Test Spacecraft operating
More informationSPACE. (Some space topics are also listed under Mechatronic topics)
SPACE (Some space topics are also listed under Mechatronic topics) Dr Xiaofeng Wu Rm N314, Bldg J11; ph. 9036 7053, Xiaofeng.wu@sydney.edu.au Part I SPACE ENGINEERING 1. Vision based satellite formation
More informationGNC/AOCS DEVELOPMENT SYSTEM FOR RENDEZ-VOUS AND DOCKING MISSIONS AT SENER, AND ASSOCIATED TEST FACILITIES
. GNC/AOCS DEVELOPMENT SYSTEM FOR RENDEZ-VOUS AND DOCKING MISSIONS AT SENER, AND ASSOCIATED TEST FACILITIES Gonzalo Saavedra, Antonio Ayuso, Juan Manuel del Cura, Jose Maria Fernandez, Salvador Llorente,
More informationModule 2: Lecture 4 Flight Control System
26 Guidance of Missiles/NPTEL/2012/D.Ghose Module 2: Lecture 4 Flight Control System eywords. Roll, Pitch, Yaw, Lateral Autopilot, Roll Autopilot, Gain Scheduling 3.2 Flight Control System The flight control
More informationEVALUATION OF THE GENERALIZED EXPLICIT GUIDANCE LAW APPLIED TO THE BALLISTIC TRAJECTORY EXTENDED RANGE MUNITION
EVALUATION OF THE GENERALIZED EXPLICIT GUIDANCE LAW APPLIED TO THE BALLISTIC TRAJECTORY EXTENDED RANGE MUNITION KISHORE B. PAMADI Naval Surface Warfare Center, Dahlgren Laboratory (NSWCDL) A presentation
More informationOn the Guidance and Control System of Epsilon Solid Rocket Launcher
On the Guidance and Control System of Epsilon Solid Rocket Launcher Y. Morita, M. Tamura, N. Ishii, T. Yamamoto Japan Aerospace Exploration Agency H. Ohtsuka, Y. Segawa and K. Tanaka IHI Aerospace Abstract
More informationThe PROBA Missions Design Capabilities for Autonomous Guidance, Navigation and Control. Jean de Lafontaine President
The PROBA Missions Design Capabilities for Autonomous Guidance, Navigation and Control Jean de Lafontaine President Overview of NGC NGC International Inc (holding company) NGC Aerospace Ltd Sherbrooke,
More informationCapability in Complexity SHOAL-REPORT J590
Capability in Complexity SHOAL-REPORT-599-2017-J590 From Aerospace Futures to Employed (and back again) Nikita Sardesai & John Furness 13 July 2017 SHOAL-REPORT-599-2017-J590 Overview Introductions and
More informationHardware in the Loop Simulation for Unmanned Aerial Vehicles
NATIONAL 1 AEROSPACE LABORATORIES BANGALORE-560 017 INDIA CSIR-NAL Hardware in the Loop Simulation for Unmanned Aerial Vehicles Shikha Jain Kamali C Scientist, Flight Mechanics and Control Division National
More informationSPASIM: A SPACECRAFT SIMULATOR
SPASIM: A SPACECRAFT SIMULATOR Carlos A. Liceaga NASA Langley Research Center 8 Langley Blvd., M/S 328 Hampton, VA 23681-0001 c.a.liceaga@larc.nasa.gov ABSTRACT The SPAcecraft SIMulator (SPASIM) simulates
More informationVery Affordable Precision Projectile System and Flight Experiments
Very Affordable Precision Projectile System and Flight Experiments Chris Stout Analysis & Evaluation Technology Division, FPAT ARDEC Frank Fresconi, Gordon Brown, Ilmars Celmins, James DeSpirito, Mark
More informationKey Areas for Collaboration
Planetary Robotics & Autonomy - current and future collaborations with China Dr. Yang Gao Head of AI & Autonomy Group Lecturer in Spacecraft Autonomy Surrey Space Centre University of Surrey, United Kingdom
More informationESA PREPARATION FOR HUMAN LUNAR EXPLORATION. Scott Hovland European Space Agency, HME-HFH, ESTEC,
ESA PREPARATION FOR HUMAN LUNAR EXPLORATION Scott Hovland European Space Agency, HME-HFH, ESTEC, Scott.Hovland@esa.int 1 Aurora Core Programme Outline Main goals of Core Programme: To establish set of
More informationAsteroid Redirect Mission and Human Exploration. William H. Gerstenmaier NASA Associate Administrator for Human Exploration and Operations
Asteroid Redirect Mission and Human Exploration William H. Gerstenmaier NASA Associate Administrator for Human Exploration and Operations Leveraging Capabilities for an Asteroid Mission NASA is aligning
More informationFlight control system for a reusable rocket booster on the return flight through the atmosphere
Flight control system for a reusable rocket booster on the return flight through the atmosphere Aaron Buysse 1, Willem Herman Steyn (M2) 1, Adriaan Schutte 2 1 Stellenbosch University Banghoek Rd, Stellenbosch
More informationPlatform Independent Launch Vehicle Avionics
Platform Independent Launch Vehicle Avionics Small Satellite Conference Logan, Utah August 5 th, 2014 Company Introduction Founded in 2011 The Co-Founders blend Academia and Commercial Experience ~20 Employees
More informationFLCS V2.1. AHRS, Autopilot, Gyro Stabilized Gimbals Control, Ground Control Station
AHRS, Autopilot, Gyro Stabilized Gimbals Control, Ground Control Station The platform provides a high performance basis for electromechanical system control. Originally designed for autonomous aerial vehicle
More informationAIRCRAFT CONTROL AND SIMULATION
AIRCRAFT CONTROL AND SIMULATION AIRCRAFT CONTROL AND SIMULATION Third Edition Dynamics, Controls Design, and Autonomous Systems BRIAN L. STEVENS FRANK L. LEWIS ERIC N. JOHNSON Cover image: Space Shuttle
More informationvstasker 6 A COMPLETE MULTI-PURPOSE SOFTWARE TO SPEED UP YOUR SIMULATION PROJECT, FROM DESIGN TIME TO DEPLOYMENT REAL-TIME SIMULATION TOOLKIT FEATURES
REAL-TIME SIMULATION TOOLKIT A COMPLETE MULTI-PURPOSE SOFTWARE TO SPEED UP YOUR SIMULATION PROJECT, FROM DESIGN TIME TO DEPLOYMENT Diagram based Draw your logic using sequential function charts and let
More informationLeveraging Simulation to Create Better Software Systems in an Agile World. Jason Ard Kristine Davidsen 4/8/2013
Leveraging Simulation to Create Better Software Systems in an Agile World Jason Ard Kristine Davidsen 4/8/2013 Copyright 2013 Raytheon Company. All rights reserved. Customer Success Is Our Mission is a
More informationUniversity of Kentucky Space Systems Laboratory. Jason Rexroat Space Systems Laboratory University of Kentucky
University of Kentucky Space Systems Laboratory Jason Rexroat Space Systems Laboratory University of Kentucky September 15, 2012 Missions Overview CubeSat Capabilities Suborbital CubeSats ISS CubeSat-sized
More informationTHE GNC MEASUREMENT SYSTEM FOR THE AUTOMATED TRANSFER VEHICLE
THE GNC MEASUREMENT SYSTEM FOR THE AUTOMATED TRANSFER VEHICLE Yohann ROUX (1), Paul DA CUNHA (1) (1 ) EADS Space Transportation, 66 route de Verneuil 78133 Les Mureaux Cedex, France E-mail:Yohann.roux@space.eads.net
More informationARTES 33 ESA Telecommunication Public Private Partnership
ARTES 33 ESA Telecommunication Public Private Partnership November 13 th, 2012 Juan Carlos Munoz-Delgado Rationale for ESA Telecom PPPs 1. What is a PPP? a. The Public-Private Partnership is a business
More informationSimulation of GPS-based Launch Vehicle Trajectory Estimation using UNSW Kea GPS Receiver
Simulation of GPS-based Launch Vehicle Trajectory Estimation using UNSW Kea GPS Receiver Sanat Biswas Australian Centre for Space Engineering Research, UNSW Australia, s.biswas@unsw.edu.au Li Qiao School
More informationA Methodology for Effective Reuse of Design Simulators in Operational Contexts: Lessons Learned in European Space Programmes
A Methodology for Effective Reuse of Design Simulators in Operational Contexts: Lessons Learned in European Space Programmes 11th International Workshop on Simulation & EGSE facilities for Space Programmes
More informationAn Explore Mars BE BOLD technical project. Sanford Morton Emily Briere Cassidy Chan
An Explore Mars BE BOLD technical project 1 Sanford Morton Emily Briere Cassidy Chan Agenda 2 Mission Overview Why? How? What? Technology Walkthrough A deep dive into our systems Inspira:on in Ac:on Ac@ve
More informationDesign of Multidimensional Space Motion Simulation System For Spacecraft Attitude and Orbit Guidance and Control Based on Radar RF Environment
2016 Sixth International Conerence on Instrumentation & Measurement, Computer, Communication and Control Design o Multidimensional Space Motion Simulation System For Spacecrat Attitude and Orbit Guidance
More informationSofting TDX ODX- and OTX-Based Diagnostic System Framework
Softing TDX ODX- and OTX-Based Diagnostic System Framework DX (Open Diagnostic data exchange) and OTX (Open Test sequence exchange) standards are very well established description formats for diagnostics
More informationNanosat Deorbit and Recovery System to Enable New Missions
SSC11-X-3 Nanosat Deorbit and Recovery System to Enable New Missions Jason Andrews, Krissa Watry, Kevin Brown Andrews Space, Inc. 3415 S. 116th Street, Ste 123, Tukwila, WA 98168, (206) 342-9934 jandrews@andrews-space.com,
More informationCubeSat Proximity Operations Demonstration (CPOD) Mission Update Cal Poly CubeSat Workshop San Luis Obispo, CA
CubeSat Proximity Operations Demonstration (CPOD) Mission Update Cal Poly CubeSat Workshop San Luis Obispo, CA 04-22-2015 Austin Williams VP, Space Vehicles ConOps Overview - Designed to Maximize Mission
More information2 a Shade one more square to make a pattern with just one line of symmetry.
GM2 End-of-unit Test Rotate the shape 80 about point P. P 2 a Shade one more square to make a pattern with just one line of symmetry. b Shade one more square to make a pattern with rotational symmetry
More informationDesign of a Remote-Cockpit for small Aerospace Vehicles
Design of a Remote-Cockpit for small Aerospace Vehicles Muhammad Faisal, Atheel Redah, Sergio Montenegro Universität Würzburg Informatik VIII, Josef-Martin Weg 52, 97074 Würzburg, Germany Phone: +49 30
More informationANTENNA ELEMENTS INTEGRATED INTO THE PARACHUTES OF PLANETARY ENTRY PROBES
WORKSHOP ANTENNA ELEMENTS INTEGRATED INTO THE PARACHUTES OF PLANETARY ENTRY PROBES Carlos Corral van Damme Maarten van der Vorst Rodolfo Guidi Simón Benolol GMV, 2006 Property of GMV All rights reserved
More informationCanadian Activities in Intelligent Robotic Systems - An Overview
In Proceedings of the 8th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2004' ESTEC, Noordwijk, The Netherlands, November 2-4, 2004 Canadian Activities in Intelligent Robotic
More informationHopper Spacecraft Simulator. Billy Hau and Brian Wisniewski
Hopper Spacecraft Simulator Billy Hau and Brian Wisniewski Agenda Introduction Flight Dynamics Hardware Design Avionics Control System Future Works Introduction Mission Overview Collaboration with Penn
More informationSTK Missile Defense. Introduction: Scenario Storyline:
Introduction: STK Missile Defense STK provides missile defense professionals with an environment for performing system-level analysis of threats, sensors, communications, intercept engagements, and defense
More informationThe Analysis Module of ESA s Space Trajectory Analysis software
The Analysis Module of ESA s Space Trajectory Analysis software Ana Margarida Teixeira Pinto Raposo Instituto Superior Técnico, Portugal, December 2010 Abstract- The use of simulation software has proven
More informationTime-of-Flight and Ranging Experiments on the Lunar Laser Communication Demonstration
Time-of-Flight and Ranging Experiments on the Lunar Laser Communication Demonstration M. L. Stevens, R. R. Parenti, M. M. Willis, J. A. Greco, F. I. Khatri, B. S. Robinson, D. M. Boroson Stanford PNT Symposium
More informationCubeSat Proximity Operations Demonstration (CPOD) Vehicle Avionics and Design
CubeSat Proximity Operations Demonstration (CPOD) Vehicle Avionics and Design August CubeSat Workshop 2015 Austin Williams VP, Space Vehicles CPOD: Big Capability in a Small Package Communications ADCS
More informationUnmanned on-orbit servicing (OOS), ROKVISS and the TECSAS mission
In Proceedings of the 8th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2004' ESTEC, Noordwijk, The Netherlands, November 2-4, 2004 On-Orbit Servicing (OOS), ROKVISS and
More informationNautical Autonomous System with Task Integration (Code name)
Nautical Autonomous System with Task Integration (Code name) NASTI 10/6/11 Team NASTI: Senior Students: Terry Max Christy, Jeremy Borgman Advisors: Nick Schmidt, Dr. Gary Dempsey Introduction The Nautical
More informationImproving Lunar Return Entry Footprints Using Enhanced Skip Trajectory Guidance
Improving Lunar Return Entry Footprints Using Enhanced Skip Trajectory Guidance Z. R. Putnam * and R. D. Braun Georgia Institute of Technology, Atlanta, GA, and S. H. Bairstow and G. H. Barton Charles
More informationDynamics and Operations of an Orbiting Satellite Simulation. Requirements Specification 13 May 2009
Dynamics and Operations of an Orbiting Satellite Simulation Requirements Specification 13 May 2009 Christopher Douglas, Karl Nielsen, and Robert Still Sponsor / Faculty Advisor: Dr. Scott Trimboli ECE
More informationIridium NEXT SensorPODs: Global Access For Your Scientific Payloads
Iridium NEXT SensorPODs: Global Access For Your Scientific Payloads 25 th Annual AIAA/USU Conference on Small Satellites August 9th 2011 Dr. Om P. Gupta Iridium Satellite LLC, McLean, VA, USA Iridium 1750
More informationJoint Australian Engineering (Micro) Satellite (JAESat) - A GNSS Technology Demonstration Mission
Journal of Global Positioning Systems (2005) Vol. 4, No. 1-2: 277-283 Joint Australian Engineering (Micro) Satellite (JAESat) - A GNSS Technology Demonstration Mission Werner Enderle Cooperative Research
More informationCYLICAL VISITS TO MARS VIA ASTRONAUT HOTELS
CYLICAL VISITS TO MARS VIA ASTRONAUT HOTELS Presentation to the NASA Institute of Advanced Concepts (NIAC) 2000 Annual Meeting by Kerry T. Nock Global June 7, 2000 Global TOPICS MOTIVATION OVERVIEW SIGNIFICANCE
More informationMomo Software Context Aware User Interface Application USER MANUAL. Burak Kerim AKKUŞ Ender BULUT Hüseyin Can DOĞAN
Momo Software Context Aware User Interface Application USER MANUAL Burak Kerim AKKUŞ Ender BULUT Hüseyin Can DOĞAN 1. How to Install All the sources and the applications of our project is developed using
More informationPrinciples of the Global Positioning System Lecture 20" Processing Software" Primary research programs"
12.540 Principles of the Global Positioning System Lecture 20" Prof. Thomas Herring" Room 54-820A; 253-5941" tah@mit.edu" http://geoweb.mit.edu/~tah/12.540 " Processing Software" Examine basic features
More informationInnoSat and MATS An Ingenious Spacecraft Platform applied to Mesospheric Tomography and Spectroscopy
Niclas Larsson N. Larsson, R. Lilja (OHB Sweden), M. Örth, S. Söderholm (ÅAC Microtec), J. Köhler, R. Lindberg (SNSB), J. Gumbel (MISU) SATELLITE SYSTEMS InnoSat and MATS An Ingenious Spacecraft Platform
More informationAutomation & Robotics (A&R) for Space Applications in the German Space Program
B. Sommer, RD-RR 1 Automation & Robotics (A&R) for Space Applications in the German Space Program ASTRA 2002 ESTEC, November 2002 1 2 Current and future application areas Unmanned exploration of the cold
More informationA Unified Space Vision
A Unified Space Vision Buzz Aldrin LEAG Laurel, MD October 24, 2014 Prepared by The Unified Space Vision Institute UNIFIED SPACE VISION OBJECTIVES Set Mars settlement as the pre-eminent US policy goal
More informationARL Fall 2017 Meetings
ARL Fall 2017 Meetings Miguel Nunes Assistant Specialist, Hawaii Institute of Geophysics and Planetology (HIGP) and Hawaii Space Flight Laboratory (HSFL) Autonomous Docking with Small Satellites Overview
More informationUAV CRAFT CRAFT CUSTOMIZABLE SIMULATOR
CRAFT UAV CRAFT CUSTOMIZABLE SIMULATOR Customizable, modular UAV simulator designed to adapt, evolve, and deliver. The UAV CRAFT customizable Unmanned Aircraft Vehicle (UAV) simulator s design is based
More informationA Guidance, Navigation and Control (GN&C) Implementation of Plug-and-Play for Responsive Spacecraft
AIAA infotech@aerospace 2007 Conference and Exhibit AIAA 2007-2911 A Guidance, Navigation and Control (GN&C) Implementation of Plug-and-Play for Responsive Spacecraft Paul Graven Microcosm, Inc.
More informationPredictions of the GOCE in-flight performances with the End-to-End System Simulator. Third International GOCE User Workshop
Predictions of the GOCE in-flight performances with the End-to-End System Simulator Page 1 Giuseppe Catastini, Stefano Cesare, Simona De Sanctis, Massimo Dumontel, Manlio Parisch, Gianfranco Sechi Alcatel
More informationThe Global Exploration Roadmap International Space Exploration Coordination Group (ISECG)
The Global Exploration Roadmap International Space Exploration Coordination Group (ISECG) Kathy Laurini NASA/Senior Advisor, Exploration & Space Ops Co-Chair/ISECG Exp. Roadmap Working Group FISO Telecon,
More informationPioneering Partnership Performance
Pioneering Partnership Performance Born for In-Field Testing Impaq Elite is a portable 4 channel real-time analyzer that is built for advanced noise and vibration test in the field. Unique features like
More information3DM-GX4-45 LORD DATASHEET. GPS-Aided Inertial Navigation System (GPS/INS) Product Highlights. Features and Benefits. Applications
LORD DATASHEET 3DM-GX4-45 GPS-Aided Inertial Navigation System (GPS/INS) Product Highlights High performance integd GPS receiver and MEMS sensor technology provide direct and computed PVA outputs in a
More informationResilient and Accurate Autonomous Vehicle Navigation via Signals of Opportunity
Resilient and Accurate Autonomous Vehicle Navigation via Signals of Opportunity Zak M. Kassas Autonomous Systems Perception, Intelligence, and Navigation (ASPIN) Laboratory University of California, Riverside
More informationCover. DLR-ESA Workshop on ARTES-11. SGEO: Implementation of of Artes-11. Dr. Andreas Winkler
Cover DLR-ESA Workshop on ARTES-11 SGEO: Implementation of of Artes-11 Dr. Andreas Winkler June June29, 29, 2006 2006 Tegernsee, Tegernsee, Germany Germany Slide 1 Table Table of of Contents - Introduction
More informationActive Vibration Isolation of an Unbalanced Machine Tool Spindle
Active Vibration Isolation of an Unbalanced Machine Tool Spindle David. J. Hopkins, Paul Geraghty Lawrence Livermore National Laboratory 7000 East Ave, MS/L-792, Livermore, CA. 94550 Abstract Proper configurations
More informationRAX: The Radio Aurora explorer
RAX: Matt Bennett University of Michigan CubeSat Workshop Cal Poly, San Luis Obispo April 22 nd, 2009 Background Sponsored by National Science Foundation University of Michigan and SRI International Collaboration
More information2009 ESMD Space Grant Faculty Project
2009 ESMD Space Grant Faculty Project 1 Objectives Train and develop the highly skilled scientific, engineering and technical workforce of the future needed to implement space exploration missions: In
More informationIntegrating Advanced Payload Data Processing in a Demanding CubeSat Mission. Mark McCrum, Peter Mendham
Integrating Advanced Payload Data Processing in a Demanding CubeSat Mission Mark McCrum, Peter Mendham CubeSat mission capability Nano-satellites missions are increasing in capability Constellations Distributed
More informationOn January 14, 2004, the President announced a new space exploration vision for NASA
Exploration Conference January 31, 2005 President s Vision for U.S. Space Exploration On January 14, 2004, the President announced a new space exploration vision for NASA Implement a sustained and affordable
More informationDetailed Pattern Computations of the UHF Antennas on the Spacecraft of the ExoMars Mission
Detailed Pattern Computations of the UHF Antennas on the Spacecraft of the ExoMars Mission C. Cappellin 1, E. Jørgensen 1, P. Meincke 1, O. Borries 1, C. Nardini 2, C. Dreyer 2 1 TICRA, Copenhagen, Denmark,
More informationRBC (BLT) and canvas use for metro system testing and simulation
RBC (BLT) and canvas use for metro system testing and simulation EuroTCL 2017 conference - Adrien Peulvast - 1 1) RBC use for Odometry data display The story starts with a metro signalling system supplier,
More informationClassical Control Based Autopilot Design Using PC/104
Classical Control Based Autopilot Design Using PC/104 Mohammed A. Elsadig, Alneelain University, Dr. Mohammed A. Hussien, Alneelain University. Abstract Many recent papers have been written in unmanned
More informationARCHITECTURE AND MODEL OF DATA INTEGRATION BETWEEN MANAGEMENT SYSTEMS AND AGRICULTURAL MACHINES FOR PRECISION AGRICULTURE
ARCHITECTURE AND MODEL OF DATA INTEGRATION BETWEEN MANAGEMENT SYSTEMS AND AGRICULTURAL MACHINES FOR PRECISION AGRICULTURE W. C. Lopes, R. R. D. Pereira, M. L. Tronco, A. J. V. Porto NepAS [Center for Teaching
More informationMethodology for Software-in-the-Loop Testing of Low-Cost Attitude Determination Systems
SSC17-WK-09 Methodology for Software-in-the-Loop Testing of Low-Cost Attitude Determination Systems Stephanie Wegner, Evan Majd, Lindsay Taylor, Ryan Thomas and Demoz Gebre Egziabher University of Minnesota
More informationHELISIM SIMULATION CREATE. SET. HOVER
SIMULATION HELISIM CREATE. SET. HOVER HeliSIM is the industry-leading high-end COTS for creating high-fidelity, high-quality flight dynamics simulations for virtually any rotary-wing aircraft in the world
More informationVibration Control of Flexible Spacecraft Using Adaptive Controller.
Vol. 2 (2012) No. 1 ISSN: 2088-5334 Vibration Control of Flexible Spacecraft Using Adaptive Controller. V.I.George #, B.Ganesh Kamath #, I.Thirunavukkarasu #, Ciji Pearl Kurian * # ICE Department, Manipal
More informationAaron J. Dando Principle Supervisor: Werner Enderle
Aaron J. Dando Principle Supervisor: Werner Enderle Australian Cooperative Research Centre for Satellite Systems (CRCSS) at the Queensland University of Technology (QUT) Aaron Dando, CRCSS/QUT, 19 th AIAA/USU
More informationA New Simulator for Botball Robots
A New Simulator for Botball Robots Stephen Carlson Montgomery Blair High School (Lockheed Martin Exploring Post 10-0162) 1 Introduction A New Simulator for Botball Robots Simulation is important when designing
More informationIntroduction to Revolve - A Glass
Introduction to Revolve - A Glass Design & Communication Graphics 1 Object Analysis sheet Design & Communication Graphics 2 Prerequisite Knowledge Previous knowledge of the following commands are required
More informationSYSTEMS INTEGRATION AND STABILIZATION OF A CUBESAT
SYSTEMS INTEGRATION AND STABILIZATION OF A CUBESAT Tyson Kikugawa Department of Electrical Engineering University of Hawai i at Manoa Honolulu, HI 96822 ABSTRACT A CubeSat is a fully functioning satellite,
More informationESA UNCLASSIFIED - Releasable to the Public. ESA Workshop: Research Opportunities on the Deep Space Gateway
ESA Workshop: Research Opportunities on the Deep Space Gateway Prepared by James Carpenter Reference ESA-HSO-K-AR-0000 Issue/Revision 1.1 Date of Issue 27/07/2017 Status Issued CHANGE LOG ESA Workshop:
More informationTactical and Strategic Missile Guidance
Israel Association for Automatic Control 5 Day Course 10-14 March 2013 Hotel Daniel, Herzliya Tactical and Strategic Missile Guidance Fee: 5000 NIS/participant for participants 1-20 from the same company
More informationSPAN Data Logging for Inertial Explorer
APN-076 ev C SPAN Data Logging for Inertial Explorer Page 1 November 16, 2017 Overview This document provides an overview of the OEM6 and OEM7 SPAN logs used for post-processing in Inertial Explorer (IE)
More informationPORTUGUESE ASSOCIATION OF SPACE INDUSTRIES
PORTUGUESE ASSOCIATION OF SPACE INDUSTRIES 1 Proespaço is a non-profit organization whose Mission is to promote Portuguese Industry Space activities, within National authorities and next to Major International
More informationDefense Technical Information Center Compilation Part Notice
UNCLASSIFIED Defense Technical Information Center Compilation Part Notice ADPO10954 TITLE: INS/GPS for Strike Warfare Beyond the Year 2000 DISTRIBUTION: Approved for public release, distribution unlimited
More informationProximity Operations Nano-Satellite Flight Demonstration (PONSFD) Overview
Proximity Operations Nano-Satellite Flight Demonstration (PONSFD) Overview April 25 th, 2013 Scott MacGillivray, President Tyvak Nano-Satellite Systems LLC 15265 Alton Parkway, Suite 200 Irvine, CA 92618-2606
More informationAerospace Sensor Suite
Aerospace Sensor Suite ECE 1778 Creative Applications for Mobile Devices Final Report prepared for Dr. Jonathon Rose April 12 th 2011 Word count: 2351 + 490 (Apper Context) Jin Hyouk (Paul) Choi: 998495640
More informationGuidance, Navigation and Control of High-Altitude Airships
Guidance, Navigation and Control of High-Altitude Airships White Paper by Joseph Mueller Princeton Satellite Systems, Inc. 33 Witherspoon Street Princeton, NJ 08542-3207 Small Business C Class Corporation,
More informationRecent Progress on Wearable Augmented Interaction at AIST
Recent Progress on Wearable Augmented Interaction at AIST Takeshi Kurata 12 1 Human Interface Technology Lab University of Washington 2 AIST, Japan kurata@ieee.org Weavy The goal of the Weavy project team
More informationSatellite Technology for Future Applications
Satellite Technology for Future Applications WSRF Panel n 4 Dubai, 3 March 2010 Guy Perez VP Telecom Satellites Programs 1 Commercial in confidence / All rights reserved, 2010, Thales Alenia Space Content
More informationFlight Dynamics AE426
KING FAHD UNIVERSITY Department of Aerospace Engineering AE426: Flight Dynamics Instructor Dr. Ayman Hamdy Kassem What is flight dynamics? Is the study of aircraft motion and its characteristics. Is it
More informationDesign of Accurate Navigation System by Integrating INS and GPS using Extended Kalman Filter
Design of Accurate Navigation System by Integrating INS and GPS using Extended Kalman Filter Santhosh Kumar S. A 1, 1 M.Tech student, Digital Electronics and Communication Systems, PES institute of technology,
More informationAutonomous and Autonomic Systems: With Applications to NASA Intelligent Spacecraft Operations and Exploration Systems
Walt Truszkowski, Harold L. Hallock, Christopher Rouff, Jay Karlin, James Rash, Mike Hinchey, and Roy Sterritt Autonomous and Autonomic Systems: With Applications to NASA Intelligent Spacecraft Operations
More informationGesture Identification Using Sensors Future of Interaction with Smart Phones Mr. Pratik Parmar 1 1 Department of Computer engineering, CTIDS
Gesture Identification Using Sensors Future of Interaction with Smart Phones Mr. Pratik Parmar 1 1 Department of Computer engineering, CTIDS Abstract Over the years from entertainment to gaming market,
More informationFuture technologies for planetary exploration within the European Exploration Envelope Programme at the European Space Agency
Future technologies for planetary exploration within the European Exploration Envelope Programme at the European Space Agency Jorge Alves, Ludovic Duvet, Sanjay Vijendran Exploration Preparation, Research
More informationAirbus DS ESA Phase-0 L5 Spacecraft/Orbital Concept Overview. Emanuele Monchieri 6 th March 2017
Airbus DS ESA Phase-0 L5 Spacecraft/Orbital Concept Overview Emanuele Monchieri 6 th March 2017 Airbus DS ESA Phase-0 L5 Spacecraft/Orbital Concept Overview Contents L5 Mission Outline Mission Concept
More informationESTEC-CNES ROVER REMOTE EXPERIMENT
ESTEC-CNES ROVER REMOTE EXPERIMENT Luc Joudrier (1), Angel Munoz Garcia (1), Xavier Rave et al (2) (1) ESA/ESTEC/TEC-MMA (Netherlands), Email: luc.joudrier@esa.int (2) Robotic Group CNES Toulouse (France),
More information