The Use of Short-Arc Angle and Angle Rate Data for Deep-Space Initial Orbit Determination and Track Association

Size: px
Start display at page:

Download "The Use of Short-Arc Angle and Angle Rate Data for Deep-Space Initial Orbit Determination and Track Association"

Transcription

1 The Use of Short-Arc Angle and Angle Rate Data for Deep-Space Initial Orbit Determination and Track Association Dr. Moriba Jah (AFRL) Mr. Kyle DeMars (UT-Austin) Dr. Paul Schumacher Jr. (AFRL)

2 Background/Motivation High-value assets near GEO within a population of sparsely observed or never-seen-before objects Insufficient resources for uninterrupted/persistent tracking of each object Need for automated, near real-time, and robust methods of initial orbit determination to support catalog development and follow-on maintenance

3 Methodology for Angles Only Photon counting device provides dense angles measurements for an apparent number of objects Topocentric Right Ascension and Declination at 500 Hz Measured angles are smoothed over a specified time (e.g. 20 seconds) One pair of angles is used in conjunction with several hypotheses to initiate the process Hypothesize object distances (range magnitude since angles provide range direction) Hypothesize object velocity vector magnitude and direction Multiple Hypothesis Filter is initialized based on ad hoc discretized region in 4-dimensional parameter space N-objects and M-hypotheses per object yields NxM initially equallyweighted individual Unscented Kalman Filters running simultaneously

4 Methodology for Angles and Rates Photon counting device provides dense angles measurements for an apparent number of objects Topocentric Right Ascension and Declination at 500 Hz Measured angles are smoothed over a specified time (e.g. 20 seconds) and angle rates are appropriately derived One pair of angles and associated rates are used to form the 2- dimensional admissible region of range and range-rate for each apparent object The admissible region is constrained on maximum and minimum range as well as energy (via a semi-major axis constraint) The constrained admissible region is discretized into regions of hypotheses to be tested Multiple Hypothesis Filter is initialized based on discretized and constrained 2-dimensional admissible region N-objects and M-hypotheses per object yields NxM initially equally-weighted individual Unscented Kalman Filters running simultaneously

5 Methodology

6 Admissible Region

7 Admissible Region

8 Sigma-Point (Unscented) Estimation

9 Methodology

10 Methodology

11 Methodology

12 Simulated Scenario Estimated Parameters A Priori Uncertainty (1 ) Remarks Position (O) 1000 kilometers Each hypothesis initialized with uncertainty based upon admissible region discretization and/or other factors Velocity (O) 1000 meters/sec Each hypothesis initialized with uncertainty based upon admissible region discretization and/or other factors Data Parameters Data Weights (1 ) Remarks Right Asc./Declination 0.4 arcseconds Data noise assumed to be at 20 sec sampling rate Right Asc./Declination Rate 0.07 arcseconds/sec Data noise assumed to be at 20 sec sampling rate

13 True RSO Epoch State Vectors

14 True Topocentric Angular RSO Positions

15 Simulation Results: Angles-Only

16 Simulation Results: Angles and Angle- Rate

17 Conclusions/Summary A method has been implemented which exploits the concept of the range/range-rate admissible region to initialize a set of hypotheses for autonomous and near real-time multiple-object initial orbit determination from short-arc optical measurements While the state errors are rather large after 10 minutes of observations (~ 0.7% of the full orbit arc), the method results in an encouraging discrimination of multiple objects having different orbits and yields state vectors with associated covariances (~ 40 arcminutes in FOV) suitable to hand-off to follow-on sensors. Previous work has shown that if the tracks are updated several hours later with an equivalent short-arc, the trajectory is sufficiently determined to yield successful track correlation on the subsequent evening. Angle rate data provided an improvement in state error reduction, but more importantly, allowed for better constraint of initial orbit hypotheses via the admissible region

18 Future Work Assess how many data of what accuracy / precision are required to obtain approximately Gaussian state pdfs Compare the current method with non-gaussian pdf approaches Adaptive Gaussian Mixtures Investigate the utility of information-theoretic approaches to determining what observations should be collected in a pass in order to successfully and unambiguously correlate to subsequent passes

19 Interactive Multiple Model Probabilistic Data Association Filter

20 Interactive Multiple Model Probabilistic Data Association Filter

Initial Orbit Determination Using Stereoscopic Imaging and Gaussian Mixture Models

Initial Orbit Determination Using Stereoscopic Imaging and Gaussian Mixture Models Initial Orbit Determination Using Stereoscopic Imaging and Gaussian Mixture Models Keith A. LeGrand K. DeMars, H.J. Pernicka Department of Mechanical and Aerospace Engineering Missouri University of Science

More information

Technical analysis of commercially hosted optical payloads for enhanced SSA

Technical analysis of commercially hosted optical payloads for enhanced SSA Technical analysis of commercially hosted optical payloads for enhanced SSA Jonathan D. Lowe Analytical Graphics, Inc., Exton, Pennsylvania, 19341. Email:jlowe@agi.com David A. Vallado Center for Space

More information

FBK Optical Data Association in a Multi-Hypothesis Framework with Maneuvers

FBK Optical Data Association in a Multi-Hypothesis Framework with Maneuvers FBK Optical Data Association in a Multi-Hypothesis Framework with Maneuvers W. R. Faber and Islam I. Hussein Applied Defense Solutions John T. Kent and Shambo Bhattacharjee University of Leeds Moriba K.

More information

ABSTRACT 1. INTRODUCTION

ABSTRACT 1. INTRODUCTION Probabilistic Admissible Region for Short-Arc Angles-Only Observations Islam I. Hussein and Christopher W. T. Roscoe Applied Defense Solutions, Columbia, Maryland Paul W. Schumacher, Jr. Air Force Research

More information

LINEARIZED ORBIT COVARIANCE GENERATION AND PROPAGATION ANALYSIS VIA SIMPLE MONTE CARLO SIMULATIONS

LINEARIZED ORBIT COVARIANCE GENERATION AND PROPAGATION ANALYSIS VIA SIMPLE MONTE CARLO SIMULATIONS LINEARIZED ORBIT COVARIANCE GENERATION AND PROPAGATION ANALYSIS VIA SIMPLE MONTE CARLO SIMULATIONS Chris Sabol, Paul Schumacher AFRL Thomas Sukut USAFA Terry Alfriend Texas A&M Keric Hill PDS Brendan Wright

More information

An AEGIS-CPHD Filter to Maintain Custody of GEO Space Objects with Limited Tracking Data

An AEGIS-CPHD Filter to Maintain Custody of GEO Space Objects with Limited Tracking Data An AEGIS-CPH Filter to Maintain Custody of GEO Space Objects with Limited Tracing ata Steven Gehly, Brandon Jones, and Penina Axelrad University of Colorado at Boulder ABSTRACT The Geosynchronous orbit

More information

Short-arc tracklet association for geostationary objects

Short-arc tracklet association for geostationary objects Short-arc tracklet association for geostationary objects J.A. Siminski, O. Montenbruck, H. Fiedler German Space Operations Center, Deutsches Zentrum für Luft- und Raumfahrt, 82234 Weßling, Germany T. Schildknecht

More information

Autonomous Mobile Robot Design

Autonomous Mobile Robot Design Autonomous Mobile Robot Design Topic: Extended Kalman Filter Dr. Kostas Alexis (CSE) These slides relied on the lectures from C. Stachniss, J. Sturm and the book Probabilistic Robotics from Thurn et al.

More information

COMPARISON OF ANGLES ONLY INITIAL ORBIT DETERMINATION ALGORITHMS FOR SPACE DEBRIS CATALOGUING

COMPARISON OF ANGLES ONLY INITIAL ORBIT DETERMINATION ALGORITHMS FOR SPACE DEBRIS CATALOGUING COMPARISON OF ANGLES ONLY INITIAL ORBIT DETERMINATION ALGORITHMS FOR SPACE DEBRIS CATALOGUING Fran Martinez Fadrique, Alberto Águeda Maté, Joan Jorquera Grau, Jaime Fernández Sánchez, Laura Aivar García

More information

A COMPARISON OF JPDA AND BELIEF PROPAGATION FOR DATA ASSOCIATION IN SSA

A COMPARISON OF JPDA AND BELIEF PROPAGATION FOR DATA ASSOCIATION IN SSA A COMPARISON OF JPDA AND BELIEF PROPAGATION FOR DATA ASSOCIATION IN SSA Mar Rutten, Jason Willams, and Neil Gordon, NSID, Defence Science and Technology Organisation, Australia School of EEE, The University

More information

PARALLEL ALGORITHM FOR TRACK INITIATION FOR OPTICAL SPACE SURVEILLANCE

PARALLEL ALGORITHM FOR TRACK INITIATION FOR OPTICAL SPACE SURVEILLANCE PARALLEL ALGORITHM FOR TRACK INITIATION FOR OPTICAL SPACE SURVEILLANCE Paul W. Schumacher, Jr., * Matthew P. Wilkins, and Christopher W. T. Roscoe INTRODUCTION We propose a type of admissible-region analysis

More information

ORBIT DETERMINATION AND DATA FUSION IN GEO

ORBIT DETERMINATION AND DATA FUSION IN GEO ORBIT DETERMINATION AND DATA FUSION IN GEO Joshua T. Horwood, Aubrey B. Poore Numerica Corporation, 4850 Hahns Pea Drive, Suite 200, Loveland CO, 80538 Kyle T. Alfriend Department of Aerospace Engineering,

More information

Kyle DeMars (1), Moriba Jah (2), Dan Giza (3), Tom Kelecy (4) , ABSTRACT

Kyle DeMars (1), Moriba Jah (2), Dan Giza (3), Tom Kelecy (4) , ABSTRACT ORBIT DETERMINATION PERFORMANCE IMPROVEMENTS FOR HIGH AREA-TO-MASS RATIO SPACE OBJECT TRACKING USING AN ADAPTIVE GAUSSIAN MIXTURES ESTIMATION ALGORITHM Kyle DeMars (1), Moriba Jah (2), Dan Giza (3), Tom

More information

Catalogue Creation for Space Situational Awareness with Optical Sensors

Catalogue Creation for Space Situational Awareness with Optical Sensors Catalogue Creation for Space Situational Awareness with Optical Sensors Tyler A. Hobson and I. Vaughan L. Clarkson School of Information Technology and Electrical Engineering, The University of Queensland

More information

AIR FORCE RESEARCH LABORATORY Directed Energy Directorate 3550 Aberdeen Ave SE

AIR FORCE RESEARCH LABORATORY Directed Energy Directorate 3550 Aberdeen Ave SE AFRL-RD-PS TP-2009-1023 AFRL-RD-PS TP-2009-1023 ORBIT DETERMINATION PERFORMANCE IMPROVEMENTS FOR HIGH AREA-TO-MASS RATIO SPACE OBJECT TRACKING USING AN ADAPTIVE GAUSSIAN MIXTURES EXTIMATION ALGORITHM:

More information

ROBOTICS 01PEEQW. Basilio Bona DAUIN Politecnico di Torino

ROBOTICS 01PEEQW. Basilio Bona DAUIN Politecnico di Torino ROBOTICS 01PEEQW Basilio Bona DAUIN Politecnico di Torino Probabilistic Fundamentals in Robotics Gaussian Filters Course Outline Basic mathematical framework Probabilistic models of mobile robots Mobile

More information

2D Image Processing. Bayes filter implementation: Kalman filter

2D Image Processing. Bayes filter implementation: Kalman filter 2D Image Processing Bayes filter implementation: Kalman filter Prof. Didier Stricker Kaiserlautern University http://ags.cs.uni-kl.de/ DFKI Deutsches Forschungszentrum für Künstliche Intelligenz http://av.dfki.de

More information

GEO Optical Data Association with Concurrent Metric and Photometric Information Phan Dao 1 and Dave Monet 2

GEO Optical Data Association with Concurrent Metric and Photometric Information Phan Dao 1 and Dave Monet 2 GEO Optical Data Association with Concurrent Metric and Photometric Information Phan Dao 1 and Dave Monet 1 Air Force Research Laboratory, Kirtland AFB US Naval Observatory, Flagstaff Station Abstract

More information

RADAR-OPTICAL OBSERVATION MIX

RADAR-OPTICAL OBSERVATION MIX RADAR-OPTICAL OBSERVATION MIX Felix R. Hoots + Deep space satellites, having a period greater than or equal to 225 minutes, can be tracked by either radar or optical sensors. However, in the US Space Surveillance

More information

Bounds on Range and Range Rate for Optical Tracking of Satellites

Bounds on Range and Range Rate for Optical Tracking of Satellites Bounds on Range and Range Rate for Optical Tracking of Satellites Paul W. Schumacher, Jr. Air Force Research Laboratory ABSTRACT We propose a type of admissible-region analysis for track initiation in

More information

Radar-Optical Observation Mix

Radar-Optical Observation Mix Radar-Optical Observation Mix Felix R. Hoots" April 2010! ETG Systems Engineering Division April 19, 10 1 Background" Deep space satellites are those with period greater than or equal to 225 minutes! Synchronous!

More information

GROUND OPTICAL SIGNAL PROCESSING ARCHITECTURE FOR CONTRIBUTING SPACE-BASED SSA SENSOR DATA

GROUND OPTICAL SIGNAL PROCESSING ARCHITECTURE FOR CONTRIBUTING SPACE-BASED SSA SENSOR DATA GROUND OPTICAL SIGNAL PROCESSING ARCHITECTURE FOR CONTRIBUTING SPACE-BASED SSA SENSOR DATA Darin Koblick, Alfred Goldsmith, Michael Klug, and Pete Mangus Millennium Space Systems, Inc. El Segundo, CA.

More information

Incorporating Uncertainty in Admissible Regions for Uncorrelated Detections

Incorporating Uncertainty in Admissible Regions for Uncorrelated Detections Incorporating Uncertainty in Admissible Regions for Uncorrelated Detections Johnny L. Worthy III, Marcus J. Holzinger Georgia Institute of Technology, Atlanta, GA, 3332 Admissible region methods for initial

More information

Copyright 2016 Advanced Maui Optical and Space Surveillance Technologies Conference (AMOS)

Copyright 2016 Advanced Maui Optical and Space Surveillance Technologies Conference (AMOS) Application of satellite laser ranging techniques for space situational awareness efforts M. Shappirio, NASA Goddard Space Flight Center J.F. McGarry, NASA Goddard Space Flight Center J. Bufton, Global

More information

Probabilistic Fundamentals in Robotics. DAUIN Politecnico di Torino July 2010

Probabilistic Fundamentals in Robotics. DAUIN Politecnico di Torino July 2010 Probabilistic Fundamentals in Robotics Gaussian Filters Basilio Bona DAUIN Politecnico di Torino July 2010 Course Outline Basic mathematical framework Probabilistic models of mobile robots Mobile robot

More information

Initial Relative Orbit Determination Using Stereoscopic Imaging and Gaussian Mixture Models

Initial Relative Orbit Determination Using Stereoscopic Imaging and Gaussian Mixture Models SSC3-VIII-6 Initial Relative Orbit Determination Using Stereoscopic Imaging and Gaussian Mixture Models Keith LeGrand Missouri University of Science and Technology 4 W. 3th St., Rolla, MO; (573) 34-78

More information

2D Image Processing. Bayes filter implementation: Kalman filter

2D Image Processing. Bayes filter implementation: Kalman filter 2D Image Processing Bayes filter implementation: Kalman filter Prof. Didier Stricker Dr. Gabriele Bleser Kaiserlautern University http://ags.cs.uni-kl.de/ DFKI Deutsches Forschungszentrum für Künstliche

More information

Certain Thoughts on Uncertainty Analysis for Dynamical Systems

Certain Thoughts on Uncertainty Analysis for Dynamical Systems Certain Thoughts on Uncertainty Analysis for Dynamical Systems!"#$$%&'(#)*+&!"#$%"&$%'()$%(*+&$,$-$+.(",/(0,&122341,&(5$#$67(8'.&1-.(!"#$%%&'()*+,-.+/01'&2+,304 5,#')67,-642849,:!'-(:'&4;4

More information

Parallel Algorithm for Track Initiation for Optical Space Surveillance

Parallel Algorithm for Track Initiation for Optical Space Surveillance Parallel Algorithm for Track Initiation for Optical Space Surveillance 3 rd US-China Technical Interchange on Space Surveillance Beijing Institute of Technology Beijing, China 12 16 May 2013 Dr. Paul W.

More information

Dynamic Tasking of Networked Sensors Using Covariance Information

Dynamic Tasking of Networked Sensors Using Covariance Information Dynamic Tasking of Networked Sensors Using Covariance Information Keric Hill, Paul Sydney, Randy Cortez, Kris Hamada, and Daron Nishimoto Pacific Defense Solutions, LLC, 1300 N. Holopono St., Suite 116,

More information

Understanding the Differences between LS Algorithms and Sequential Filters

Understanding the Differences between LS Algorithms and Sequential Filters Understanding the Differences between LS Algorithms and Sequential Filters In order to perform meaningful comparisons between outputs from a least squares (LS) orbit determination algorithm and orbit determination

More information

APPLICATION OF OPTICAL TRACKING AND ORBIT ESTIMATION TO SATELLITE ORBIT TOMOGRAPHY

APPLICATION OF OPTICAL TRACKING AND ORBIT ESTIMATION TO SATELLITE ORBIT TOMOGRAPHY AAS 13-824 APPLICATION OF OPTICAL TRACKING AND ORBIT ESTIMATION TO SATELLITE ORBIT TOMOGRAPHY Michael A. Shoemaker, Brendt Wohlberg, Richard Linares, and Josef Koller. INTRODUCTION Satellite orbit tomography

More information

Angular Velocity Determination Directly from Star Tracker Measurements

Angular Velocity Determination Directly from Star Tracker Measurements Angular Velocity Determination Directly from Star Tracker Measurements John L. Crassidis Introduction Star trackers are increasingly used on modern day spacecraft. With the rapid advancement of imaging

More information

Kalman filtering and friends: Inference in time series models. Herke van Hoof slides mostly by Michael Rubinstein

Kalman filtering and friends: Inference in time series models. Herke van Hoof slides mostly by Michael Rubinstein Kalman filtering and friends: Inference in time series models Herke van Hoof slides mostly by Michael Rubinstein Problem overview Goal Estimate most probable state at time k using measurement up to time

More information

Kalman Filter Computer Vision (Kris Kitani) Carnegie Mellon University

Kalman Filter Computer Vision (Kris Kitani) Carnegie Mellon University Kalman Filter 16-385 Computer Vision (Kris Kitani) Carnegie Mellon University Examples up to now have been discrete (binary) random variables Kalman filtering can be seen as a special case of a temporal

More information

OPTIMAL ESTIMATION of DYNAMIC SYSTEMS

OPTIMAL ESTIMATION of DYNAMIC SYSTEMS CHAPMAN & HALL/CRC APPLIED MATHEMATICS -. AND NONLINEAR SCIENCE SERIES OPTIMAL ESTIMATION of DYNAMIC SYSTEMS John L Crassidis and John L. Junkins CHAPMAN & HALL/CRC A CRC Press Company Boca Raton London

More information

When Does the Uncertainty Become Non-Gaussian. Kyle T. Alfriend 1 Texas A&M University Inkwan Park 2 Texas A&M University

When Does the Uncertainty Become Non-Gaussian. Kyle T. Alfriend 1 Texas A&M University Inkwan Park 2 Texas A&M University When Does the Uncertainty Become Non-Gaussian Kyle T. Alfriend Texas A&M University Inkwan Park 2 Texas A&M University ABSTRACT The orbit state covariance is used in the conjunction assessment/probability

More information

Parallel Track Initiation for Optical Space Surveillance Using Range and Range-Rate Bounds

Parallel Track Initiation for Optical Space Surveillance Using Range and Range-Rate Bounds Parallel Track Initiation for Optical Space Surveillance Using Range and Range-Rate Bounds Paul W. Schumacher, Jr. Air Force Research Laboratory, Kihei, Hawaii Christopher W. T. Roscoe and Matthew P. Wilkins

More information

Space Surveillance with Star Trackers. Part II: Orbit Estimation

Space Surveillance with Star Trackers. Part II: Orbit Estimation AAS -3 Space Surveillance with Star Trackers. Part II: Orbit Estimation Ossama Abdelkhalik, Daniele Mortari, and John L. Junkins Texas A&M University, College Station, Texas 7783-3 Abstract The problem

More information

Modeling and state estimation Examples State estimation Probabilities Bayes filter Particle filter. Modeling. CSC752 Autonomous Robotic Systems

Modeling and state estimation Examples State estimation Probabilities Bayes filter Particle filter. Modeling. CSC752 Autonomous Robotic Systems Modeling CSC752 Autonomous Robotic Systems Ubbo Visser Department of Computer Science University of Miami February 21, 2017 Outline 1 Modeling and state estimation 2 Examples 3 State estimation 4 Probabilities

More information

Robotics 2 Target Tracking. Giorgio Grisetti, Cyrill Stachniss, Kai Arras, Wolfram Burgard

Robotics 2 Target Tracking. Giorgio Grisetti, Cyrill Stachniss, Kai Arras, Wolfram Burgard Robotics 2 Target Tracking Giorgio Grisetti, Cyrill Stachniss, Kai Arras, Wolfram Burgard Linear Dynamical System (LDS) Stochastic process governed by is the state vector is the input vector is the process

More information

COE CST Fifth Annual Technical Meeting. Task 187: Space Situational Awareness. PI: Dan Scheeres Student: In-Kwan Park University of Colorado

COE CST Fifth Annual Technical Meeting. Task 187: Space Situational Awareness. PI: Dan Scheeres Student: In-Kwan Park University of Colorado COE CST Fifth Annual Technical Meeting Task 187: Space Situational Awareness PI: Dan Scheeres Student: In-Kwan Park University of Colorado Washington, DC 1 # Agenda Team Members Task Description Research

More information

Robot Localization and Kalman Filters

Robot Localization and Kalman Filters Robot Localization and Kalman Filters Rudy Negenborn rudy@negenborn.net August 26, 2003 Outline Robot Localization Probabilistic Localization Kalman Filters Kalman Localization Kalman Localization with

More information

Performance of a Dynamic Algorithm For Processing Uncorrelated Tracks

Performance of a Dynamic Algorithm For Processing Uncorrelated Tracks Performance of a Dynamic Algorithm For Processing Uncorrelated Tracs Kyle T. Alfriend Jong-Il Lim Texas A&M University Tracs of space objects, which do not correlate, to a nown space object are called

More information

Autonomous Navigation for Flying Robots

Autonomous Navigation for Flying Robots Computer Vision Group Prof. Daniel Cremers Autonomous Navigation for Flying Robots Lecture 6.2: Kalman Filter Jürgen Sturm Technische Universität München Motivation Bayes filter is a useful tool for state

More information

An Optical Survey for Space Debris on Highly Eccentric MEO Orbits

An Optical Survey for Space Debris on Highly Eccentric MEO Orbits An Optical Survey for Space Debris on Highly Eccentric MEO Orbits T. Schildknecht 1), A. Hinze 1), A. Vananti 1), T. Flohrer ) 1) Astronomical Institute, University of Bern, Sidlerstr. 5, CH-31 Bern, Switzerland

More information

Cataloging with an Upgraded Space Surveillance Fence

Cataloging with an Upgraded Space Surveillance Fence Cataloging with an Upgraded Space Surveillance Fence Felix Hoots, Geoff Pierce, Lester Ford AT&T Hugh Hadley Syracuse Research Integrated solutions from a trusted source Fence Provides Robust, Uncued Surveillance

More information

Sensor Tasking and Control

Sensor Tasking and Control Sensor Tasking and Control Sensing Networking Leonidas Guibas Stanford University Computation CS428 Sensor systems are about sensing, after all... System State Continuous and Discrete Variables The quantities

More information

STATISTICAL ORBIT DETERMINATION

STATISTICAL ORBIT DETERMINATION STATISTICAL ORBIT DETERMINATION Satellite Tracking Example of SNC and DMC ASEN 5070 LECTURE 6 4.08.011 1 We will develop a simple state noise compensation (SNC) algorithm. This algorithm adds process noise

More information

SLAM for Ship Hull Inspection using Exactly Sparse Extended Information Filters

SLAM for Ship Hull Inspection using Exactly Sparse Extended Information Filters SLAM for Ship Hull Inspection using Exactly Sparse Extended Information Filters Matthew Walter 1,2, Franz Hover 1, & John Leonard 1,2 Massachusetts Institute of Technology 1 Department of Mechanical Engineering

More information

KRATOS: KOLLISION RISK ASSESSMENT TOOL IN ORBITAL ELEMENT SPACES

KRATOS: KOLLISION RISK ASSESSMENT TOOL IN ORBITAL ELEMENT SPACES KRATOS: KOLLISION RISK ASSESSMENT TOOL IN ORBITAL ELEMENT SPACES Joshua T. Horwood, Navraj Singh, and Jeffrey M. Aristoff Numerica Corporation, 5042 Technology Parkway, Suite 100, Fort Collins, CO 80528

More information

Benefits of hosted payload architectures for improved GEO SSA

Benefits of hosted payload architectures for improved GEO SSA Benefits of hosted payload architectures for improved GEO SSA David Vallado Center for Space Standards and Innovation, Colorado Spring, Colorado, 80920. Email:dvallado@agi.com Jonathan Lowe Analytical

More information

Adaptive Unscented Kalman Filter with Multiple Fading Factors for Pico Satellite Attitude Estimation

Adaptive Unscented Kalman Filter with Multiple Fading Factors for Pico Satellite Attitude Estimation Adaptive Unscented Kalman Filter with Multiple Fading Factors for Pico Satellite Attitude Estimation Halil Ersin Söken and Chingiz Hajiyev Aeronautics and Astronautics Faculty Istanbul Technical University

More information

Constrained State Estimation Using the Unscented Kalman Filter

Constrained State Estimation Using the Unscented Kalman Filter 16th Mediterranean Conference on Control and Automation Congress Centre, Ajaccio, France June 25-27, 28 Constrained State Estimation Using the Unscented Kalman Filter Rambabu Kandepu, Lars Imsland and

More information

Spacecraft Angular Rate Estimation Algorithms For Star Tracker-Based Attitude Determination

Spacecraft Angular Rate Estimation Algorithms For Star Tracker-Based Attitude Determination AAS 3-191 Spacecraft Angular Rate Estimation Algorithms For Star Tracker-Based Attitude Determination Puneet Singla John L. Crassidis and John L. Junkins Texas A&M University, College Station, TX 77843

More information

Detection of Artificial Satellites in Images Acquired in Track Rate Mode.

Detection of Artificial Satellites in Images Acquired in Track Rate Mode. Detection of Artificial Satellites in Images Acquired in Track Rate Mode. Martin P. Lévesque Defence R&D Canada- Valcartier, 2459 Boul. Pie-XI North, Québec, QC, G3J 1X5 Canada, martin.levesque@drdc-rddc.gc.ca

More information

UNCERTAINTY CHARACTERIZATION FOR ANGLES-ONLY INITIAL ORBIT DETERMINATION

UNCERTAINTY CHARACTERIZATION FOR ANGLES-ONLY INITIAL ORBIT DETERMINATION AAS 13-822 UNCERTAINTY CHARACTERIZATION FOR ANGLES-ONLY INITIAL ORBIT DETERMINATION Christopher R. Binz and Liam M. Healy INTRODUCTION When no information is known about a satellite s orbit, an initial

More information

A STUDY ON THE STATE ESTIMATION OF NONLINEAR ELECTRIC CIRCUITS BY UNSCENTED KALMAN FILTER

A STUDY ON THE STATE ESTIMATION OF NONLINEAR ELECTRIC CIRCUITS BY UNSCENTED KALMAN FILTER A STUDY ON THE STATE ESTIMATION OF NONLINEAR ELECTRIC CIRCUITS BY UNSCENTED KALMAN FILTER Esra SAATCI Aydın AKAN 2 e-mail: esra.saatci@iku.edu.tr e-mail: akan@istanbul.edu.tr Department of Electronic Eng.,

More information

Rao-Blackwellized Particle Filter for Multiple Target Tracking

Rao-Blackwellized Particle Filter for Multiple Target Tracking Rao-Blackwellized Particle Filter for Multiple Target Tracking Simo Särkkä, Aki Vehtari, Jouko Lampinen Helsinki University of Technology, Finland Abstract In this article we propose a new Rao-Blackwellized

More information

OBJECT CORRELATION AND MANEUVER DETECTION USING OPTIMAL CONTROL PERFORMANCE METRICS

OBJECT CORRELATION AND MANEUVER DETECTION USING OPTIMAL CONTROL PERFORMANCE METRICS OBJECT CORRELATION AND MANEUVER DETECTION USING OPTIMAL CONTROL PERFORMANCE METRICS Marcus Holzinger Graduate Research Assistant, Aerospace Engineering Sciences University of Colorado at Boulder Daniel

More information

Sensor-scheduling simulation of disparate sensors for Space Situational Awareness Tyler A. Hobson I. Vaughan L. Clarkson ABSTRACT 1.

Sensor-scheduling simulation of disparate sensors for Space Situational Awareness Tyler A. Hobson I. Vaughan L. Clarkson ABSTRACT 1. Sensor-scheduling simulation of disparate sensors for Space Situational Awareness Tyler A. Hobson School of Information Technology & Electrical Engineering The University of Queensland I. Vaughan L. Clarkson

More information

Robotics 2 Target Tracking. Kai Arras, Cyrill Stachniss, Maren Bennewitz, Wolfram Burgard

Robotics 2 Target Tracking. Kai Arras, Cyrill Stachniss, Maren Bennewitz, Wolfram Burgard Robotics 2 Target Tracking Kai Arras, Cyrill Stachniss, Maren Bennewitz, Wolfram Burgard Slides by Kai Arras, Gian Diego Tipaldi, v.1.1, Jan 2012 Chapter Contents Target Tracking Overview Applications

More information

Particle Filters; Simultaneous Localization and Mapping (Intelligent Autonomous Robotics) Subramanian Ramamoorthy School of Informatics

Particle Filters; Simultaneous Localization and Mapping (Intelligent Autonomous Robotics) Subramanian Ramamoorthy School of Informatics Particle Filters; Simultaneous Localization and Mapping (Intelligent Autonomous Robotics) Subramanian Ramamoorthy School of Informatics Recap: State Estimation using Kalman Filter Project state and error

More information

New Worlds Observer Final Report Appendix J. Appendix J: Trajectory Design and Orbit Determination Lead Author: Karen Richon

New Worlds Observer Final Report Appendix J. Appendix J: Trajectory Design and Orbit Determination Lead Author: Karen Richon Appendix J: Trajectory Design and Orbit Determination Lead Author: Karen Richon The two NWO spacecraft will orbit about the libration point created by the Sun and Earth/Moon barycenter at the far side

More information

Mini-Course 07 Kalman Particle Filters. Henrique Massard da Fonseca Cesar Cunha Pacheco Wellington Bettencurte Julio Dutra

Mini-Course 07 Kalman Particle Filters. Henrique Massard da Fonseca Cesar Cunha Pacheco Wellington Bettencurte Julio Dutra Mini-Course 07 Kalman Particle Filters Henrique Massard da Fonseca Cesar Cunha Pacheco Wellington Bettencurte Julio Dutra Agenda State Estimation Problems & Kalman Filter Henrique Massard Steady State

More information

J. G. Miller (The MITRE Corporation), W. G. Schick (ITT Industries, Systems Division)

J. G. Miller (The MITRE Corporation), W. G. Schick (ITT Industries, Systems Division) Contributions of the GEODSS System to Catalog Maintenance J. G. Miller (The MITRE Corporation), W. G. Schick (ITT Industries, Systems Division) The Electronic Systems Center completed the Ground-based

More information

AN ANALYTICAL SOLUTION TO QUICK-RESPONSE COLLISION AVOIDANCE MANEUVERS IN LOW EARTH ORBIT

AN ANALYTICAL SOLUTION TO QUICK-RESPONSE COLLISION AVOIDANCE MANEUVERS IN LOW EARTH ORBIT AAS 16-366 AN ANALYTICAL SOLUTION TO QUICK-RESPONSE COLLISION AVOIDANCE MANEUVERS IN LOW EARTH ORBIT Jason A. Reiter * and David B. Spencer INTRODUCTION Collision avoidance maneuvers to prevent orbital

More information

Serendipitous Acquisition of Space Situational Awareness From Astronomical Surveys (SASSAFrAS)

Serendipitous Acquisition of Space Situational Awareness From Astronomical Surveys (SASSAFrAS) Serendipitous Acquisition of Space Situational Awareness From Astronomical Surveys (SASSAFrAS) Mark P. Bolden The Pennsylvania State University David B. Spencer, PhD The Pennsylvania State University ABSTRACT

More information

Robot Localisation. Henrik I. Christensen. January 12, 2007

Robot Localisation. Henrik I. Christensen. January 12, 2007 Robot Henrik I. Robotics and Intelligent Machines @ GT College of Computing Georgia Institute of Technology Atlanta, GA hic@cc.gatech.edu January 12, 2007 The Robot Structure Outline 1 2 3 4 Sum of 5 6

More information

Combined Particle and Smooth Variable Structure Filtering for Nonlinear Estimation Problems

Combined Particle and Smooth Variable Structure Filtering for Nonlinear Estimation Problems 14th International Conference on Information Fusion Chicago, Illinois, USA, July 5-8, 2011 Combined Particle and Smooth Variable Structure Filtering for Nonlinear Estimation Problems S. Andrew Gadsden

More information

Josef Koller, ISR-1. NADIR Meeting Website

Josef Koller, ISR-1. NADIR Meeting Website LA-UR- 11-06444 Approved for public release; distribution is unlimited. Title: IMPACT Project: Integrated Modeling of Perturbations in Atmospheres for Conjunction Tracking - A New Orbital Prediction Model

More information

State Estimation and Motion Tracking for Spatially Diverse VLC Networks

State Estimation and Motion Tracking for Spatially Diverse VLC Networks State Estimation and Motion Tracking for Spatially Diverse VLC Networks GLOBECOM Optical Wireless Communications Workshop December 3, 2012 Anaheim, CA Michael Rahaim mrahaim@bu.edu Gregary Prince gbprince@bu.edu

More information

CORRELATION OF SPACE DEBRIS OBSERVATIONS BY THE VIRTUAL DEBRIS ALGORITHM

CORRELATION OF SPACE DEBRIS OBSERVATIONS BY THE VIRTUAL DEBRIS ALGORITHM CORRELATION OF SPACE DEBRIS OBSERVATIONS BY THE VIRTUAL DEBRIS ALGORITHM G. Tommei 1, A. Milani 1, D. Farnocchia 1, and A. Rossi 2 1 Department of Mathematics, University of Pisa, Largo Pontercorvo 5,

More information

Toward Online Probabilistic Path Replanning

Toward Online Probabilistic Path Replanning Toward Online Probabilistic Path Replanning R. Philippsen 1 B. Jensen 2 R. Siegwart 3 1 LAAS-CNRS, France 2 Singleton Technology, Switzerland 3 ASL-EPFL, Switzerland Workshop on Autonomous Robot Motion,

More information

Tracking and Identification of Multiple targets

Tracking and Identification of Multiple targets Tracking and Identification of Multiple targets Samir Hachour, François Delmotte, Eric Lefèvre, David Mercier Laboratoire de Génie Informatique et d'automatique de l'artois, EA 3926 LGI2A first name.last

More information

2D Image Processing (Extended) Kalman and particle filter

2D Image Processing (Extended) Kalman and particle filter 2D Image Processing (Extended) Kalman and particle filter Prof. Didier Stricker Dr. Gabriele Bleser Kaiserlautern University http://ags.cs.uni-kl.de/ DFKI Deutsches Forschungszentrum für Künstliche Intelligenz

More information

The J-MAPS Mission: Improvements to Orientation Infrastructure and Support for Space Situational Awareness

The J-MAPS Mission: Improvements to Orientation Infrastructure and Support for Space Situational Awareness AIAA SPACE 2007 Conference & Exposition 18-20 September 2007, Long Beach, California AIAA 2007-9927 The J-MAPS Mission: Improvements to Orientation Infrastructure and Support for Space Situational Awareness

More information

Lecture 2: From Linear Regression to Kalman Filter and Beyond

Lecture 2: From Linear Regression to Kalman Filter and Beyond Lecture 2: From Linear Regression to Kalman Filter and Beyond January 18, 2017 Contents 1 Batch and Recursive Estimation 2 Towards Bayesian Filtering 3 Kalman Filter and Bayesian Filtering and Smoothing

More information

Dynamic Tasking of Networked Sensors Using Covariance Information

Dynamic Tasking of Networked Sensors Using Covariance Information Dynamic Tasking of Networked Sensors Using Covariance Information Keric Hill, Paul Sydney, Randy Cortez, Kris Hamada, and Daron Nishimoto Pacific Defense Solutions, LLC, 1300 N. Holopono St., Suite 116,

More information

SLAM Techniques and Algorithms. Jack Collier. Canada. Recherche et développement pour la défense Canada. Defence Research and Development Canada

SLAM Techniques and Algorithms. Jack Collier. Canada. Recherche et développement pour la défense Canada. Defence Research and Development Canada SLAM Techniques and Algorithms Jack Collier Defence Research and Development Canada Recherche et développement pour la défense Canada Canada Goals What will we learn Gain an appreciation for what SLAM

More information

Keck Adaptive Optics Note #385. Feasibility of LGS AO observations in the vicinity of Jupiter. Stephan Kellner and Marcos van Dam

Keck Adaptive Optics Note #385. Feasibility of LGS AO observations in the vicinity of Jupiter. Stephan Kellner and Marcos van Dam Keck Adaptive Optics Note #385 Feasibility of LGS AO observations in the vicinity of Jupiter Stephan Kellner and Marcos van Dam Version 2: 25 July 2006 1 Introduction It has been proposed by Imke De Pater

More information

Estimation and Prediction Scenarios

Estimation and Prediction Scenarios Recursive BLUE BLUP and the Kalman filter: Estimation and Prediction Scenarios Amir Khodabandeh GNSS Research Centre, Curtin University of Technology, Perth, Australia IUGG 2011, Recursive 28 June BLUE-BLUP

More information

SPIN STATE ESTIMATION OF TUMBLING SMALL BODIES

SPIN STATE ESTIMATION OF TUMBLING SMALL BODIES AAS 15-363 SPIN STATE ESTIMATION OF TUMBLING SMALL BODIES Corwin Olson, Ryan P. Russell, and Shyam Bhaskaran INTRODUCTION It is expected that a non-trivial percentage of small bodies that future missions

More information

Partially Observable Markov Decision Processes (POMDPs)

Partially Observable Markov Decision Processes (POMDPs) Partially Observable Markov Decision Processes (POMDPs) Sachin Patil Guest Lecture: CS287 Advanced Robotics Slides adapted from Pieter Abbeel, Alex Lee Outline Introduction to POMDPs Locally Optimal Solutions

More information

Introduction to Astrodynamics and the Air Force Maui Optical and Supercomputing Site (AMOS)

Introduction to Astrodynamics and the Air Force Maui Optical and Supercomputing Site (AMOS) Introduction to Astrodynamics and the Air Force Maui Optical and Supercomputing Site (AMOS) Dr. Moriba K. Jah Director, Advanced Sciences & Technology Research Institute for Astrodynamics (ASTRIA) Air

More information

Distributed Data Fusion with Kalman Filters. Simon Julier Computer Science Department University College London

Distributed Data Fusion with Kalman Filters. Simon Julier Computer Science Department University College London Distributed Data Fusion with Kalman Filters Simon Julier Computer Science Department University College London S.Julier@cs.ucl.ac.uk Structure of Talk Motivation Kalman Filters Double Counting Optimal

More information

ASSOCIATION OF SATELLITE OBSERVATIONS USING BAYESIAN INFERENCE

ASSOCIATION OF SATELLITE OBSERVATIONS USING BAYESIAN INFERENCE AAS 13-245 ASSOCIATION OF SATELLITE OBSERVATIONS USING BAYESIAN INFERENCE Christopher Binz and Liam Healy When observing satellites in an increasingly cluttered space environment, ambiguity in measurement

More information

A Gaussian Mixture Motion Model and Contact Fusion Applied to the Metron Data Set

A Gaussian Mixture Motion Model and Contact Fusion Applied to the Metron Data Set 1th International Conference on Information Fusion Chicago, Illinois, USA, July 5-8, 211 A Gaussian Mixture Motion Model and Contact Fusion Applied to the Metron Data Set Kathrin Wilkens 1,2 1 Institute

More information

Improving Space Surveillance with Space-Based Visible Sensor

Improving Space Surveillance with Space-Based Visible Sensor Improving Space Surveillance with Space-Based Visible Sensor Jayant Sharma, Andrew Wiseman, and George Zollinger MIT Lincoln Laboratory Abstract The Midcourse Space Experiment satellite was launched in

More information

Benefits of a Geosynchronous Orbit (GEO) Observation Point for Orbit Determination

Benefits of a Geosynchronous Orbit (GEO) Observation Point for Orbit Determination Benefits of a Geosynchronous Orbit (GEO) Observation Point for Orbit Determination Ray Byrne, Michael Griesmeyer, Ron Schmidt, Jeff Shaddix, and Dave Bodette Sandia National Laboratories ABSTRACT Determining

More information

AUTOMOTIVE ENVIRONMENT SENSORS

AUTOMOTIVE ENVIRONMENT SENSORS AUTOMOTIVE ENVIRONMENT SENSORS Lecture 5. Localization BME KÖZLEKEDÉSMÉRNÖKI ÉS JÁRMŰMÉRNÖKI KAR 32708-2/2017/INTFIN SZÁMÚ EMMI ÁLTAL TÁMOGATOTT TANANYAG Related concepts Concepts related to vehicles moving

More information

arxiv:hep-ex/ v1 5 Apr 2000

arxiv:hep-ex/ v1 5 Apr 2000 Track Fit Hypothesis Testing and Kink Selection using Sequential Correlations Robert V. Kowalewski and Paul D. Jackson arxiv:hep-ex/48v 5 Apr 2 Abstract Department of Physics and Astronomy, University

More information

RELATIVE NAVIGATION FOR SATELLITES IN CLOSE PROXIMITY USING ANGLES-ONLY OBSERVATIONS

RELATIVE NAVIGATION FOR SATELLITES IN CLOSE PROXIMITY USING ANGLES-ONLY OBSERVATIONS (Preprint) AAS 12-202 RELATIVE NAVIGATION FOR SATELLITES IN CLOSE PROXIMITY USING ANGLES-ONLY OBSERVATIONS Hemanshu Patel 1, T. Alan Lovell 2, Ryan Russell 3, Andrew Sinclair 4 "Relative navigation using

More information

MEETING ORBIT DETERMINATION REQUIREMENTS FOR A SMALL SATELLITE MISSION

MEETING ORBIT DETERMINATION REQUIREMENTS FOR A SMALL SATELLITE MISSION MEETING ORBIT DETERMINATION REQUIREMENTS FOR A SMALL SATELLITE MISSION Adonis Pimienta-Peñalver, Richard Linares, and John L. Crassidis University at Buffalo, State University of New York, Amherst, NY,

More information

The Space-based Telescopes for Actionable Refinement of Ephemeris (STARE) mission

The 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 information

Parallel Particle Filter in Julia

Parallel Particle Filter in Julia Parallel Particle Filter in Julia Gustavo Goretkin December 12, 2011 1 / 27 First a disclaimer The project in a sentence. workings 2 / 27 First a disclaimer First a disclaimer The project in a sentence.

More information

UAV Navigation: Airborne Inertial SLAM

UAV Navigation: Airborne Inertial SLAM Introduction UAV Navigation: Airborne Inertial SLAM Jonghyuk Kim Faculty of Engineering and Information Technology Australian National University, Australia Salah Sukkarieh ARC Centre of Excellence in

More information

LINEARIZED ORBIT COVARIANCE GENERATION AND PROPAGATION ANALYSIS VIA SIMPLE MONTE CARLO SIMULATIONS

LINEARIZED ORBIT COVARIANCE GENERATION AND PROPAGATION ANALYSIS VIA SIMPLE MONTE CARLO SIMULATIONS LINEARIZED ORBIT COVARIANCE GENERATION AND PROPAGATION ANALYSIS VIA SIMPLE MONTE CARLO SIMULATIONS Chris Sabol *, Thomas Sukut, Keric Hill, Kyle T. Alfriend, Brendan Wright **, You Li **, and Paul Schumacher

More information

6.435, System Identification

6.435, System Identification SET 6 System Identification 6.435 Parametrized model structures One-step predictor Identifiability Munther A. Dahleh 1 Models of LTI Systems A complete model u = input y = output e = noise (with PDF).

More information

Automated RSO Stability Analysis. Thomas M. Johnson Analytical Graphics, Inc., 220 Valley Creek Blvd, Exton, PA 19468, USA

Automated RSO Stability Analysis. Thomas M. Johnson Analytical Graphics, Inc., 220 Valley Creek Blvd, Exton, PA 19468, USA Automated RSO Stability Analysis Thomas M. Johnson Analytical Graphics, Inc., 220 Valley Creek Blvd, Exton, PA 19468, USA ABSTRACT A methodology for assessing the attitude stability of a Resident Space

More information