3 rd US-China Space Surveillance Technical Interchange
|
|
|
- Horatio Scott
- 5 years ago
- Views:
Transcription
1 3 rd US-China Space Surveillance Technical Interchange Beijing Institute of Technology Beijing, China May 2013 YE Shuhua China Co- P. Kenneth Seidelmann U.S. Co- ZHANG Jingrui China Technical Kyle T. Alfriend U.S. Technical 1
2 SUNDAY 12 MAY American participants can have a choice to visit Summer Palace or Forbidden City. 2
3 MONDAY 13 MAY Opening Remarks 8:40 Prof. YE Shuhua, China Co- Prof. Kenneth Seidelmann, U.S. Co- Session 1 Probability of Collision Liu Zhonggui S1.1 9:00 Miss Distance - Generalized Variance Non-Central Chi Distribution K. Chan S1.2 9:30 Explicit Expression of Collision Probability In Terms of RSW and NTW Components Of Relative Position BAI X-Z., L. CHEN and TANG G-J. S1.3 10:00 Uncertainty in Probability of Collision Calculation D. Garber 10:30 Coffee Break S1.4 11:00 Bayesian Group Tracking Method For Space Debris HUANG J., HU W. D. and ZHANG L.F. Session 2 Orbit Uncertainty and Propagation Ken Chan S2.1 11:30 A Method to Improve the Precision of Space Debris Orbital Elements LIU Zhonggui S2.2 12:00 Analytical Non-Linear Uncertainty Propagation: Theory And Implementation K. Fujimoto, D.J. Scheeres and K.T. Alfriend 12:30 Lunch S2.3 14:00 Improving low-earth orbit prediction precision with TLEs Liu wei,wang Ronglan,Yan Ruidong,Gong Jiancun 3
4 S2.4 14:30 Orbit Uncertainty Propagation of a Tumbling High Area-to-Mass- Ratio Space Object CHENG Y. Session 3 Tracking Space Debris 1 HU Weidong S3.1 15:00 Multi-source Space Situational Information Fusion and Cooperation WANG Peng. 15:30 Coffee Break S3.2 16:00 An Automated Telescope for Orbital Debris LU X.M. S3.3 16:30 GEO Cross-tag Resolution using Color Signatures T. Payne Banquet 18:00 17:00 Technical Discussion of Monday s Presentations Darren Garber and HU Weidong 4
5 TUESDAY 14 MAY Session 4 Space Situational Awareness Support D. Walsh S4.1 9:00 Parallel Algorithm For Track Initiation For Optical Space Surveillance P. W. Schumacher, M. P. Wilkins and C.W.T. Roscoe S4.2 9:30 Maneuver Detection of Space Object For Space Surveillance HUANG J., HU W. D. and ZHANG L.F. 10:00 Coffee Break S4.3 10:30 Autonomy Architecture for a Raven-Class Telescope with Space Situational Awareness Applications R. D. Coder and M. J. Holzinger Session 5 Space Debris Tracking 2 Gong Zizheng S5.1 11:00 A Survey of Radars Capable of Providing Small Debris Measurements for Orbit Prediction D. Walsh S5.2 11:30 Study on Optical Cross section of Space Debris WANG J.F., LU X.M. and MAO Y. S5.3 12:00 Long Term Behavior of the Thermosphere Determined from Satellite Drag Measurements S. Knowles 12:30 Lunch S5.4 14:00 Application of scmos in space debris measurement Ge L 5
6 Session 6 Space Debris Issues Marcus Holzinger S6.1 14:30 Law Coordinating of Restricting Space Debris CHEN Lingyun 15:00 Coffee Break S6.2 15:30 Space Debris as an Epidemic D. Finkleman (presentation by K.T. Alfriend) S6.3 16:00 CASC Efforts on Dealing with Space Debristoward Space Long Term Sustainability GONG Zizheng. S6.4 16:30 Space Debris Mitigation Status of China's Launch Vehicles SONG Qiang. 17:00 Technical Discussion of Tuesday s Presentations Tamara Payne and LIU Zhonggui 6
7 WEDNESDAY 15 MAY Session 7 Mathematical Applications Jiang xiaojun S7.1 9:00 Robust Formation Design for High-Eccentricity Satellite Missions Using a Stochastic Optimization Approach C. W. T. Roscoe, S. R. Vadali, and K. T. Alfriend S7.2 9:30 Introduction of a new ISO project: Standard Calculation of Orbit Elements at Satellite-Launch Vehicle Separation LIU Jiarun. 10:00 Coffee Break S7.3 10:30 Mean Solar Time, UT1, UTC, and Leap Seconds P.K. Seidelmann and J. H. Seago 11:00 Closing Comments & Discussion YE Shihua, ZHANG Jingrui, Ken Seidelmann and Terry Alfriend 12:00 Lunch 14:00 Quadrilateralized Spherical Cube (QLSC)(about two-hour) Ken Chan 16:00 The National Meteorological Bureau American participants 18:30 LaoShe Tea-House American participants 7
8 THURSDAY 16 MAY 9:00 Spacecraft Collision Probability (1) Ken Chan 12:30 Lunch 13:30 Spacecraft Collision Probability (2) Ken Chan 16:00 Technical Discussion(one-hour) American participants who don t attend the Chan s lecture can have a choice to visit Great Wall and Ming Tombs or WangFuJing 8
8 th US/Russian Space Surveillance Workshop
8 th US/Russian Space Surveillance Workshop Wailea Marriott Resort Wailea, Maui, HI 18-23 April 2010 P. Kenneth Seidelmann General Chair Kyle T. Alfriend US Technical Chair Stanislav Veniaminov Russian
Improving LEO prediction precision with TLEs
Improving LEO prediction precision with TLEs LIU Wei,WANG Ronglan,YAN Ruidong,GONG Jiancun (1. Center for Space Science and Applied Research, CAS,Beijing 119, China) Abstract: TLE is the only publicly
ORBITAL SOLUTIONS TO LEO-TO-LEO ANGLES-ONLY VERY- SHORT-ARC TRACKS
ORBITAL SOLUTIONS TO LEO-TO-LEO ANGLES-ONLY VERY- SHORT-ARC TRACKS Jizhang Sang (1), Xiangxu Lei (2), Pin Zhang (3), Teng Pan (4), Huaifeng Li (5) (1) School of Geodesy and Geomatics, Wuhan University,
Orbital Anomaly Detection and Application of Space Object
Orbital Anomaly Detection and Application of Space Object Lei CHEN *, Xianzong BAI, Taotao ZHANG College of Aerospace and Materials Engineering, National University of Defense Technology, Changsha 473,China
The Inter-Agency Space Debris Coordination Committee (IADC)
The Inter-Agency Space Debris Coordination Committee (IADC) An overview of the IADC annual activities Holger Krag, ESA IADC Chair www.iadc-online.org 54 th Session of the Scientific and Technical Subcommittee
USA Space Debris Environment, Operations, and Modeling Updates
USA Space Debris Environment, Operations, and Modeling Updates Presentation to the 51 st Session of the Scientific and Technical Subcommittee Committee on the Peaceful Uses of Outer Space United Nations
Study of Physical Characteristics of High Apogee Space Debris
Study of Physical Characteristics of High Apogee Space Debris Yongna Mao, Jianfeng Wang, Xiaomeng Lu, Liang Ge, Xiaojun Jiang (National Astronomical Observatories, Beijing, 100012, China) Abstract Date
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
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.
The Inter-Agency Space Debris Coordination Committee (IADC)
The Inter-Agency Space Debris Coordination Committee (IADC) An overview of the IADC annual activities Prof. Richard Crowther, UKSA, United Kingdom IADC Chair Dr. Holger Krag, ESA/ESOC, incoming IADC Chair
Statistical methods to address the compliance of GTO with the French Space Operations Act
Statistical methods to address the compliance of GTO with the French Space Operations Act 64 th IAC, 23-27 September 2013, BEIJING, China H.Fraysse and al. Context Space Debris Mitigation is one objective
Asia-Pacific ground-base Optical Satellite Observation System APOSOS
Asia-Pacific ground-base Optical Satellite Observation System APOSOS Center for Research and Application of Space Debris National Astronomical Observatories, CAS GUO Xiaozhong Oct 2011 Outline Space debris
Space Debris Activities in India
Indian Presentation to the 47 th Session of Scientific and Technical Subcommittee of United Nations Committee on the Peaceful Uses of Outer Space Agenda 8 Space Debris Activities in India 1 Space Debris
The Inter-Agency Space Debris Coordination Committee (IADC)
The Inter-Agency Space Debris Coordination Committee (IADC) An overview of IADC s annual activities Mitsuru Ohnishi, JAXA, Japan IADC Chair www.iadc-online.org 55 th Session of the Scientific and Technical
Orbit Determination of Satellite Formations. Terry Alfriend 9 th US Russian Space Surveillance Workshop
Orbit Determination of Satellite Formations Terry Alfriend 9 th US Russian Space Surveillance Workshop Outline What is a Satellite Formation Types of Formations Proposed Approach for Orbit Determination
Space Debris Mitigation Activities at ESA
Space Debris Mitigation Activities at ESA Heiner Klinkrad ESA Space Debris Office H. Klinkrad, ESA, Feb 2011, page 1 Space Debris Environment in 2010 4,765 launches and 251 on-orbit break-ups led to 16,200
INTEROPERABILITY AND STANDARDS ACROSS THE ENTIRE SPACE ENTERPRISE. GSAW 2007 Manhattan Beach, CA March 2007
INTEROPERABILITY AND STANDARDS ACROSS THE ENTIRE SPACE ENTERPRISE. GSAW 2007 Manhattan Beach, CA 26-29 March 2007 DAVID FINKLEMAN, CENTER FOR SPACE STANDARDS AND INNOVATION ANALYTICAL GRAPHICS INC. Pg
TWO APPLICATIONS OF IMPROVEMENTS FOR AMVS OF NSMC/CMA
TWO APPLICATIONS OF IMPROVEMENTS FOR AMVS OF NSMC/CMA RE-NAVIGATION BASED ON FULL EARTH DISC IMAGE & CALCULATION OF RADIATION TRANSFER USING NWP DATA Zhang Xiaohu, Xu Jianmin National Satellite Meteorological
ACTIVITY OF RUSSIAN FEDERATION ON SPACE DEBRIS PROBLEM
ACTIVITY OF RUSSIAN FEDERATION ON SPACE DEBRIS PROBLEM 51-th session of the UN Committee on the Peaceful Uses of Outer Space (COPUOS) 1 Federal Space Agency of Russia continues consecutive activity in
V Control Distance with Dynamics Parameter Uncertainty
V Control Distance with Dynamics Parameter Uncertainty Marcus J. Holzinger Increasing quantities of active spacecraft and debris in the space environment pose substantial risk to the continued safety of
OUTBREAK INVESTIGATION AND SPATIAL ANALYSIS OF SURVEILLANCE DATA: CLUSTER DATA ANALYSIS. Preliminary Programme / Draft_2. Serbia, Mai 2013
OUTBREAK INVESTIGATION AND SPATIAL ANALYSIS OF SURVEILLANCE DATA: CLUSTER DATA ANALYSIS Preliminary Programme / Draft_2 Serbia, 20-24 Mai 2013 1. Course presentation Outbreak investigation is one of the
Collision Risk Assessment for Spacecraft with CASS
Collision Risk Assessment for Spacecraft with CASS Ma Chaowei 2011, 17-18 Oct 2011 Beijing Institute of Tracking and Telecommunications Technology Ma Chaowei 2 Contents Introduction Basic Information of
Conjunction Risk Assessment and Avoidance Maneuver Planning Tools
Conjunction Risk Assessment and Avoidance Maneuver Planning Tools Saika Aida DLR German Space Operations Center (GSOC), Oberpfaffenhofen, 834 Weßling, Germany +49 8153 8-158, saika.aida@dlr.de ASTRACT
SPACE SITUATIONAL AWARENESS AND SPACE DEBRIS ACTIVITIES IN INDIA
SPACE SITUATIONAL AWARENESS AND SPACE DEBRIS ACTIVITIES IN INDIA P Soma, Adjunct Faculty, NIAS Agenda The Growth of Space Objects since 1957 Space Situational Awareness India s Space Assets and SSA Space
Analytical Non-Linear Uncertainty Propagation: Theory And Implementation
Analytical Non-Linear Uncertainty Propagation: Theory And Implementation Kohei Fujimoto 1), Daniel J. Scheeres 2), and K. Terry Alfriend 1) May 13, 2013 1) Texas A&M University 2) The University of Colorado
Program at a Glance. (Part II) (Part I) (Part I) (Part II) (Part II) (Part II) (Part III) (Part IV) (Part II) 12:15-14:00 Light Lunch
The 5th International Conference on Scientific Computing and Partial Differential (SCPDE14) On the Occasion of Eitan Tadmor's 60th Birthday Program at a Glance Day 1 8 Dec (Mon) Day 2 9 Dec (Tue) Day 3
SECOND ANNOUNCEMENT International Technical Laser Workshop 2012 (ITLW-12)
SECOND ANNOUNCEMENT International Technical Laser Workshop 2012 (ITLW-12) Version 31/Oct/12 Satellite, Lunar and Planetary Laser Ranging: characterizing the space segment Frascati National Laboratories
Orbital Debris Observation via Laser Illuminated Optical Measurement Techniques
Orbital Debris Observation via Laser Illuminated Optical Measurement Techniques Makoto TAGAWA Kyushu University Toshiya HANADA Kyushu University Kozue HASHIMOTO, Yukihito KITAZAWA, Aritsune KAWABE IHI
Contribution of ISON and KIAM space debris. space
Contribution of ISON and KIAM space debris data center into improvement of awareness on space objects and events in the near-earth space Vladimir Agapov Keldysh Institute of Applied Mathematics RAS 2015
Orbital Data Applications for Space Objects
Orbital Data Applications for Space Objects Lei Chen Xian-Zong Bai Yan-Gang Liang Ke-Bo Li Orbital Data Applications for Space Objects Conjunction Assessment and Situation Analysis 123 Lei Chen National
How to Improve Small Satellite Missions in Two Easy Steps:
How to Improve Small Satellite Missions in Two Easy Steps: Adopting Space Debris Mitigation Guidelines and Improving Space Surveillance Network Tracking Support G. Taft DeVere Jason C. Randolph Headquarters
Attitude Control Method of Spin-Stabilized Satellite Base on Equiangular Precession
International Conference on Artificial Intelligence and Engineering Applications (AIEA 2016) Attitude Control Method of Spin-Stabilized Satellite Base on Equiangular Precession Yonggang Li a, Jiping Ren
Previous Lecture. The Von Zeipel Method. Application 1: The Brouwer model. Application 2: The Cid-Lahulla model. Simplified Brouwer transformation.
2 / 36 Previous Lecture The Von Zeipel Method. Application 1: The Brouwer model. Application 2: The Cid-Lahulla model. Simplified Brouwer transformation. Review of Analytic Models 3 / 36 4 / 36 Review:
Swiss Contributions to a Better Understanding of the Space Debris Environment
Swiss Contributions to a Better Understanding of the Space Debris Environment T. Schildknecht Astronomical Institute, University of Bern (), Switzerland 47 th Session of UNCOPUOS Scientific and Technical
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,
ACCURACY ASSESSMENT OF GEOSTATIONARY-EARTH-ORBIT WITH SIMPLIFIED PERTURBATIONS MODELS
ARTIFICIAL SATELLITES, Vol. 51, No. 2 2016 DOI: 10.1515/arsa-2016-0005 ACCURACY ASSESSMENT OF GEOSTATIONARY-EARTH-ORBIT WITH SIMPLIFIED PERTURBATIONS MODELS Lihua Ma, Xiaojun Xu, Feng Pang National Astronomical
3 rd WHU Summer Theory Institute
3 rd WHU Summer Theory Institute Frontiers in Quantum Control and Computational Physics July 3 7, 2017 School of Physics and Technology Wuhan University Initiated in 2015, the 3 rd WHU Summer Theory Institute
IMPROVED DESIGN OF ON-ORBIT SEPARATION SCHEMES FOR FORMATION INITIALIZATION BASED ON J 2 PERTURBATION
IAA-AAS-DyCoSS- IMPROVED DESIGN OF ON-ORBIT SEPARATION SCHEMES FOR FORMATION INITIALIZATION BASED ON J PERTURBATION Jiang Chao, * Wang Zhaokui, and Zhang Yulin INTRODUCTION Using one Multi-satellite Deployment
The Characteristics and Consequences of the Break-up of the Fengyun-1C Spacecraft
The Characteristics and Consequences of the Break-up of the Fengyun-1C Spacecraft N. Johnson, E. Stansbery, J.-C. Liou, M. Horstman, C. Stokely, D. Whitlock NASA Orbital Debris Program Office NASA Johnson
A method for calculating probability of collision between space objects
RAA 2014 Vol. 14 No. 5, 601 609 doi: 10.1088/1674 4527/14/5/009 http://www.raa-journal.org http://www.iop.org/journals/raa Research in Astronomy and Astrophysics A method for calculating probability of
Past and Future Climate of Thermospheric Density: Solar and Anthropogenic Influences
Past and Future Climate of Thermospheric Density: Solar and Anthropogenic Influences Thermosphere energy balance Thermosphere climate from satellite drag Attribution of 2008 solar minimum behavior Scenarios
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
Modeling of Ground Based Space Surveillance System Based on MAS Method. Xue Chen 1,a, Li Zhi 2
Applied Mechanics and Materials Online: 2014-03-24 ISSN: 1662-7482, Vols. 543-547, pp 2755-2758 doi:10.4028/www.scientific.net/amm.543-547.2755 2014 Trans Tech Publications, Switzerland Modeling of Ground
How Can Small Satellites be used to Support Orbital Debris Removal Goals Instead of Increasing the Problem?
How Can Small Satellites be used to Support Orbital Debris Removal Goals Instead of Increasing the Problem? August 19, 2010 Jose Guerrero, Jon Manash, Kevin McKee, Matt Russell, Steve Stone and Doyle Towles
STUDY THE SPACE DEBRIS IMPACT IN THE EARLY STAGES OF THE NANO-SATELLITE DESIGN
ARTIFICIAL SATELLITES, Vol. 51, No. 4 2016 DOI: 10.1515/arsa-2016-0014 STUDY THE SPACE DEBRIS IMPACT IN THE EARLY STAGES OF THE NANO-SATELLITE DESIGN Mohammed Chessab Mahdi Al-Furat Al-Awsat Technical
USA Space Debris Environment, Operations, and Policy Updates
USA Space Debris Environment, Operations, and Policy Updates Presentation to the 48 th Session of the Scientific and Technical Subcommittee Committee on the Peaceful Uses of Outer Space United Nations
New Observation Results from A Rotating-drift-scan CCD System
New Observation Results from A Rotating-drift-scan CCD System TANG Zheng-Hong, MAO Yin-Dun, LI Yan, YU Yong Shanghai Astronomical Observatory, Chinese Academy of Sciences Abstract: A Rotating-drift-scan
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
Prof. Richard Crowther Chief Engineer, UK Space Agency. Reflections on Orbital Debris Mitigation Measures
Prof. Richard Crowther Chief Engineer, UK Space Agency Reflections on Orbital Debris Mitigation Measures near-earth satellite population reflects use of space >17000 tracked objects concentrated in distinct
FOSS4G 2010 presented by OSGeo Proposal
FOSS4G 2010 presented by OSGeo Proposal About OSGeo China The China Chapter of OSGeo is formed by Chinese Active Users of Open Source Geospatial Software, hosted by National Remote Sensing Center of China
45th Meeting of the DPS Block Schedule
Saturday, 5 October 2013 9:00am Workshop: ExoPAG 8, 9:00am-5:00pm, Director's Row H Sunday, 6 October 2013 8:00am Workshop: Using Astronomy and Planetary Science in K-12, 8:00am-5:00pm, Governor's Square
Modeling of the Orbital Debris Environment Risks in the Past, Present, and Future
Modeling of the Orbital Debris Environment Risks in the Past, Present, and Future Mark Matney, Ph.D. Orbital Debris Program Office NASA Johnson Space Center 2 National Aeronautics and Space Administration
Overview of JAXA Activities on Sustainable Space Development and Space Situational Awareness
Overview of JAXA Activities on Sustainable Space Development and Space Situational Awareness 26 February 2015 Shizuo YAMAMOTO Vice President, JAXA CONTENTS 1. Japan s Space Activities Structure 2. JAXA
GEO protected region: ISON capabilities to provide informational support for tasks of spacecraft flight safety and space debris removal
Russian Academy of Sciences Keldysh Institute of Applied Mathematics GEO protected region: ISON capabilities to provide informational support for tasks of spacecraft flight safety and space debris removal
on space debris objects obtained by the
KIAM space debris data center for processing and analysis of information on space debris objects obtained by the ISON network Vladimir Agapov, Igor Molotov Keldysh Institute of Applied Mathematics RAS
Orbital Support for China's Chang'E-2 Lunar Exploration Satellite
Orbital Support for China's Chang'E-2 Lunar Exploration Satellite WANG Hong 1 and FAN Min 2 Beijing Institute of Tracking and Telecommunication Technology, Beijing, China, 100094 DONG Guangliang 3 Beijing
The Evaluation Methods of Collision. Between Space Debris and Spacecraft
The Evaluation Methods of Collision Between Space Debris and Spacecraft Wang Xinfeng, Li Yanjun, Northwestern Polytechnical University, Xi an, 710072 Wu Gongyou Xi an Jiaotong University, Xi an 710048
Kyle T. Alfriend Astrodynamics Symposium May Monterey, California
Conference Program Kyle T. Alfriend Astrodynamics Symposium 17-19 May 2010 Monterey, California 1 Schedule of Events Monday, 17 May 6pm - 8pm Welcome Reception Tuesday, 18 May 7 am - 8 am Breakfast 8:30
SPACE DEBRIS CHASER CONSTELLATION
THE VISION SPACE DEBRIS CHASER CONSTELLATION Constellation management Application to SSO debris Inclination between 98 and 99.5 Altitude between 750 km and 850 km Constellation of 38 Cubesats Low-thrust
The use of ASPOS OKP System in the interests of ensuring the safety of space operations and increasing awareness about the situation in high orbits
The use of ASPOS OKP System in the interests of ensuring the safety of space operations and increasing awareness about the situation in high orbits Committee on the Peaceful Uses of Outer Space 61 st session,
The 3rd International Intensive Course on UNESCO Global Geoparks Geoparks Management and Earth Heritage Interpretation
China University of Geosciences, Beijing The 3rd International Intensive Course on UNESCO Global s s Management and Earth Heritage Interpretation 3-8 December, 2017 Venues: Geosciences Convention Center,
Tailoring the Observation Scenarios and Data Processing Techniques for Supporting Conjunction Event Assessments
Tailoring the Observation Scenarios and Data Processing Techniques for Supporting Conjunction Event Assessments T. Flohrer *, B. Bastida Virgili *, H. Krag *, H. Klinkrad *, K. Merz *, T. Schildknecht
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
Beijing Institute of Spacecraft Environment Engineering, Beijing , China *Corresponding author
2017 2 nd International Conference on Test, Measurement and Computational Method (TMCM 2017) ISBN: 978-1-60595-465-3 General Lightweight Integrated Space Environment and Effect Detection Technology Zi-cai
Results and Analyses of Debris Tracking from Mt Stromlo
Results and Analyses of Debris Tracking from Mt Stromlo Jizhang Sang 1, Ian Ritchie, Matt Pearson, and Craig Smith EOS Space Systems Pty Ltd, Australia Abstract In the last 2 years, EOS Space Systems has
Spacecraft Orbit Anomaly Representation Using Thrust-Fourier-Coefficients with Orbit Determination Toolbox
Spacecraft Orbit Anomaly Representation Using Thrust-Fourier-Coefficients with Orbit Determination Toolbox Hyun Chul Ko and Daniel J. Scheeres University of Colorado - Boulder, Boulder, CO, USA ABSTRACT
9 th US/Russian Space Surveillance Workshop
9 th US/Russian Space Surveillance Workshop Real-Time Monitoring and Warning of Near- Earth Space Dangerous Events for Mission Control by MCC TSNIIMASH Federal State Unitary Enterprise Speakers: V. M.
Optical Detection for Space Situational Awareness (ODESSA)
Optical Detection for Space Situational Awareness (ODESSA) Brian Kloppenborg Georgia Tech Research Institute, brian.kloppenborg@gtri.gatech.edu Chris Valenta Georgia Tech Research Institute Layne Churchill
Development of Laser Measurement to Space Debris at Shanghai SLR Station
Abstract Development of Laser Measurement to Space Debris at Shanghai SLR Station Zhang Zhongping, Deng Huarong, Tang Kai, Wu Zhibo, Zhang Haifeng (Shanghai Astronomical Observatory of Chinese Academy
COVARIANCE DETERMINATION, PROPAGATION AND INTERPOLATION TECHNIQUES FOR SPACE SURVEILLANCE. European Space Surveillance Conference 7-9 June 2011
COVARIANCE DETERMINATION, PROPAGATION AND INTERPOLATION TECHNIQUES FOR SPACE SURVEILLANCE European Space Surveillance Conference 7-9 June 2011 Pablo García (1), Diego Escobar (1), Alberto Águeda (1), Francisco
A Fast Method for Embattling Optimization of Ground-Based Radar Surveillance Network
A Fast Method for Embattling Optimization of Ground-Based Radar Surveillance Network JIANG Hai University of Chinese Academy of Sciences National Astronomical Observatories, Chinese Academy of Sciences
Scientific Programme. 1. Opening Day
Scientific Programme International Training Course on Seismology, Seismic Data Analysis, Hazard Assessment and Risk Mitigation Potsdam, Germany, 12 August to 6 September, 2013 1. Opening Day Monday, Aug.
Kyle T. Alfriend Astrodynamics Symposium May Monterey, California
Preliminary Program (draft dated 13 April 2010) Kyle T. Alfriend Astrodynamics Symposium 17-19 May 2010 Monterey, California 1 Schedule of Events Monday, 17 May 6-8pm Welcome Reception Tuesday, 18 May
Bi-Annual Reporting. Tsinghua University Chapter. 1. List of current student chapter members. The officer: The other members:
Bi-Annual Reporting 1. List of current student chapter members The officer: Sigang Yang RM 11-112 Tel: 86-10-62792551 ysg03@mails.tsinghua.edu.cn Tsinghua University Chapter The other members: Gao Zhiguo
Space Debris Mitigation Activities at ESA in 2013
Space Debris Mitigation Activities at ESA in 2013 Heiner Klinkrad ESA Space Debris Office H. Klinkrad (ESA) 51st UNCOPUOS STSC 14-Feb-2014 page 1 ESA Launches in 2013 PROBA-V (2013-021A) launch May 7,
Seismology, Seismic Data Analysis, Hazard Assessment and Risk Mitigation
List of institutions, lecturers and assistants contributing to the International Training Course on "Seismology, Hazard Assessment and Risk Mitigation", August 10 to September 4, 2015 in Potsdam, Germany
Croucher Summer Course on Neutron Scattering
Croucher Summer Course on Neutron Scattering August 7-13, 2016 City University of Hong Kong 83 Tat Chee Ave. Kowloon, Hong Kong Sunday August 7: Registration, 14:00 17:00 17:30 Planning meeting with lecturers
INDEMN. A long-term collision risk prediction tool for constellation design. Romain Lucken, Damien Giolito,
INDEMN A long-term collision risk prediction tool for constellation design Romain Lucken, Damien Giolito, romain.lucken@sharemyspace.global 5th European Workshop on Space Debris Modeling and Remediation
Announcement for all of SEIC Staff and Students
Announcement for all of SEIC Staff and Students Basic Facts On 29 Nov. 2018, Kyutech will host a special presentation about LEDSAT nano satellite mission by Prof. Fabio Santoni of Sapienza Univ. of Rome
OVERVIEW ON 2012 SPACE DEBRIS ACTIVITIES IN FRANCE
OVERVIEW ON 2012 SPACE DEBRIS ACTIVITIES IN FRANCE F.ALBY IAA-Beijing 21 September 2013 IAA-Beijing-21 September 2013 1 End of life operations CONT TENT T Collision risk monitoring Atmospheric reentries
Capabilities of observation facilities of Altay opticlaser center in the problem of space debris surveillance
Open Joint Stock Company Research-and-Production Corporation Precision Systems and Instruments, Moscow, Russia Capabilities of observation facilities of Altay opticlaser center in the problem of space
The department of computer science and the chair of Aerospace
International Summer School 20-31 July 2015 in Würzburg (Germany) for Advanced Students Julius-Maximilians- UNIVERSITÄT WÜRZBURG Information Brochure The department of computer science and the chair of
Calculation of Earth s Dynamic Ellipticity from GOCE Orbit Simulation Data
Available online at www.sciencedirect.com Procedia Environmental Sciences 1 (1 ) 78 713 11 International Conference on Environmental Science and Engineering (ICESE 11) Calculation of Earth s Dynamic Ellipticity
Short-Arc Correlation and Initial Orbit Determination For Space-Based Observations
Short-Arc Correlation and Initial Orbit Determination For Space-Based Observations Kohei Fujimoto and Daniel J. Scheeres The University of Colorado at Boulder CONFERENCE PAPER Situational awareness of
Aerodynamic Lift and Drag Effects on the Orbital Lifetime Low Earth Orbit (LEO) Satellites
Aerodynamic Lift and Drag Effects on the Orbital Lifetime Low Earth Orbit (LEO) Satellites I. Introduction Carlos L. Pulido Department of Aerospace Engineering Sciences University of Colorado Boulder Abstract
PROBABILITY OF COLLISION WITH SPECIAL PERTURBATIONS DYNAMICS USING THE MONTE CARLO METHOD
AAS 11-435 PROBABILITY OF COLLISION WITH SPECIAL PERTURBATIONS DYNAMICS USING THE MONTE CARLO METHOD Chris Sabol, Christopher Binz and Alan Segerman, Kevin Roe, and Paul W. Schumacher, Jr. INTRODUCTION
Analytical Non-Linear Uncertainty Propagation: Theory And Implementation
Analytical Non-Linear Uncertainty Propagation: Theory And Implementation Kohei Fujimoto 1 Texas A&M University, College Station, TX, 77843 Daniel J. Scheeres 2 The University of Colorado-Boulder, Boulder,
High Cost-Effectiveness Debris Removal Platform with Self-Assembly Modular Solar Sail Units
High Cost-Effectiveness Debris Removal Platform with Modular Solar Sail Units By Cheng Zhengai 1), Huang Xiaoqi 1), Liu Yufei 1) 2), Zhang Xinghua 1) 1) Qian Xuesen Laboratory of Space Technology, China
USA Space Debris Environment and Operational Updates
USA Space Debris Environment and Operational Updates Presentation to the 46 th Session of the Scientific and Technical Subcommittee Committee on the Peaceful Uses of Outer Space United Nations 9-20 February
Analysis of Energy Reception Characteristics of Solar Aircraft in the Tropics of Cancer and Capricorn
Analysis of Energy Reception Characteristics of Solar Aircraft in the Tropics of Cancer and Capricorn Kangwen Sun 1 1, Jiaqi Dong, Xiaobo Sun 2,*, Ziying Zhang 1, Mou Sun 1 and Jian Zhang 3 1 School of
International Symposium for Soft Matter Science and Technology (SMST 2017)
International Symposium for Soft Matter Science and Technology (SMST 2017) Guangzhou, China April 18-19, 2017 Jointly Organized by South China Advanced Institute for Soft Matter Science and Technology,
IMPROVED CONJUNCTION ANALYSIS VIA COLLABORATIVE SPACE SITUATIONAL AWARENESS
IMPROVED CONJUNCTION ANALYSIS VIA COLLABORATIVE SPACE SITUATIONAL AWARENESS T.S. Kelso (1), D. Vallado (2), J. Chan (3), and B. Buckwalter (4) (1) Center for Space Standards & Innovation, 7150 Campus Drive,
Commercial SSA Catalog Performance
Commercial SSA Catalog Performance Robert Hall Director, ComSpOC Operations Analytical Graphics, Inc. (AGI) Tom Johnson VP of Engineering Analytical Graphics, Inc. (AGI) ABSTRACT We present a summary over
Security in Outer Space: Rising Stakes
Security in Outer Space: Rising Stakes Forging ahead: from SSA to Space Safety 12 th ESPI Autumn Conference, Vienna, 27-28 Septembre Nicolas Bobrinsky ESA, H/ SSA Programme ESA UNCLASSIFIED - For Official
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
Analysis of Debris from the Collision of the Cosmos 2251 and the Iridium 33 Satellites
Science & Global Security, 18:87 118, 2010 Copyright C Taylor & Francis Group, LLC ISSN: 0892-9882 print / 1547-7800 online DOI: 10.1080/08929882.2010.493078 Analysis of Debris from the Collision of the
Distributed Coordination and Control of Formation Flying Spacecraft
Distributed Coordination and Control of Formation Flying Spacecraft Michael Tillerson, Louis Breger, and Jonathan P. How MIT Department of Aeronautics and Astronautics {mike t, lbreger, jhow}@mit.edu Abstract
Improved orbit predictions using two-line elements
Improved orbit predictions using two-line elements Creon Levit NASA Ames Research Center, Moffett Field, MS-3, CA 93, USA William Marshall NASA Ames Research Center and Universities Space Research Association,
CORRELATION BETWEEN URBAN HEAT ISLAND EFFECT AND THE THERMAL INERTIA USING ASTER DATA IN BEIJING, CHINA
CORRELATION BETWEEN URBAN HEAT ISLAND EFFECT AND THE THERMAL INERTIA USING ASTER DATA IN BEIJING, CHINA Yurong CHEN a, *, Mingyi DU a, Rentao DONG b a School of Geomatics and Urban Information, Beijing
Autonomy Architecture for a Raven Class Telescope with Space Situational Awareness Applications
Autonomy Architecture for a Raven Class Telescope with Space Situational Awareness Applications 3nd US Chinese Technical Interchange, Beijing May 15-17, 2013 Ryan D. Coder, Graduate Research Assistant