Technical Session
Technical Session Poster
Finalist Student Session
Technical Session
Program on Tuesday, 6 June.2017
[d-1] |
Flight Dynamics Operations 1 |
Chairs: Lutz Massonne (Telespazio VEGA Deutschland GmbH at ESOC Flight Dynamics, Germany) Petr Kuchynka (GMV/ESOC, Germany) |
| 9:00 – 9:20 | ISTS-2017-d-001/ISSFD-2017-001 Feasibility of Metop-A Mission Extension on Drifting Local Time |
Pier Luigi Righetti, Richard Dyer EUMETSAT, Darmstadt, Germany Abstract | Paper |
| 9:20 – 9:40 | ISTS-2017-d-003/ISSFD-2017-003 Flight Dynamics Support to extend Metop Instruments Useful Lifetime |
Antimo Damiano1, Pier Luigi Righetti2, RüDiger Lang2, Francisco Sancho3
1RHEA Group at EUMETSAT, 2EUMETSAT, 3WGS at EUMETSAT Abstract | Paper |
| 9:40 – 10:00 | ISTS-2017-d-004/ISSFD-2017-004 Non-nominal Attitude Manoeuvres during Metop-A Extended Lifetime |
Francisco Sancho1, Jörg Fischer2, Stefania Tarquini3
1WGS Workgroup Solutions at EUMETSAT, Darmstadt, Germany, 2Jade Aerospace at EUMETSAT, Darmstadt, Germany, 3EUMETSAT, Darmstadt, Germany Abstract | Paper |
| 10:00 – 10:20 | ISTS-2017-d-002/ISSFD-2017-002 Metop Long Term Free-dynamics Attitude Analysis, for Improved Re-entry Prediction |
Stefano Pessina1, Pierluigi Righetti1, João Branco2, Victor Manuel Moreno Villa3, Thomas Vincent Peters3
1EUMETSAT, Darmstadt, Germany, 2GMV, Lisbon, Portugal, 3GMV, Madrid, Spain Abstract | Paper |
[d-2] |
Orbit Dynamics (Martian Moon) |
Chairs: Osamu Mori (Japan Aerospace Exploration Agency, Japan) Laurence Lorda (CNES, France) |
| 9:00 – 9:20 | ISTS-2017-d-005/ISSFD-2017-005 Quasi-Satellite Orbits around Deimos and Phobos Motivated by the DePhine Mission Proposal |
Sofya Spiridonova1, Kai Wickhusen2, Ralph Kahle1, Jürgen Oberst2
1German Space Operations Center, DLR, Oberpfaffenhofen, Germany, 2Institute of Planetary Research, DLR, Berlin, Germany Abstract | Paper |
| 9:20 – 9:40 | ISTS-2017-d-006/ISSFD-2017-006 Trajectory Analysis for the Phobos Proximity Phase of the MMX Mission |
Elisabet Canalias1, Laurence Lorda1, Thierry Martin1, Julien Laurent-Varin1,2, Jean Charles Marty1,2, Yuya Mimasu3
1CNES, French Space Agency, Toulouse, France., 2GRGS Spatial Geodesy Research Group, Toulouse, France., 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan. Abstract | Paper |
| 9:40 – 10:00 | ISTS-2017-d-007/ISSFD-2017-007 The Dynamical Environment for The Exploration of Phobos |
Daniel Scheeres, Stefaan VAN Wal, Zubin Olikara, Nicola Baresi
Smead Department of Aerospace Engineering Sciences, The University of Colorado, Boulder, Colorado, USA Abstract | Paper |
| 10:00 – 10:20 | ISTS-2017-d-008/ISSFD-2017-008 Orbital Operations Strategy in the Vicinity of Phobos |
Hitoshi Ikeda1, Shinji Mitani1, Yuya Mimasu2, Go Ono1, Kenichiro Nigo1, Yasuhiro Kawakatsu2
1Research and Development Directorate, JAXA, Tsukuba, Ibaraki, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Kanagawa, Japan Abstract | Paper |
| 10:20 – 10:40 | ISTS-2017-d-009/ISSFD-2017-009 Quasi-Satellite Orbits around Phobos for the Sample Return Mission |
Javier Martín, Simone Centuori
Deimos Space SLU, Spain Abstract | Paper |
[d-3] |
Trajectory Design & Optimization 1 |
Chairs: Satoshi Ueda (JAXA, Japan) Lorenzo Casalino (Politecnico di Torino, Italy) |
| 9:00 – 9:20 | ISTS-2017-d-010/ISSFD-2017-010 A Linear Analysis for the Flight Path Control of the Cassini Grand Finale Orbits |
Mar Vaquero, Yungsun Hahn, Duane Roth, Mau Wong
Jet Propulsion Laboratory / California Institute of Technology, Pasadena, CA Abstract | Paper |
| 9:20 – 9:40 | ISTS-2017-d-011/ISSFD-2017-011 Uncertainty Analysis of Mars Entry Trajectories Using Stochastic Collocation |
Yuechen Huang, Haiyang Li, Yazhong Luo
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, China Abstract | Paper |
| 9:40 – 10:00 | ISTS-2017-d-012/ISSFD-2017-012 Orbit Design for Martian Moons Explorer |
Naoko Ogawa1, Yuichi Tsuda1, Yuto Takei1, Hiroka Inoue1, Shota Takahashi2, Yasuhiro Kawakatsu1
1Japan Aerospace Exploration Agency, Japan, 2Keio University, Japan Abstract | Paper |
| 10:00 – 10:20 | ISTS-2017-d-013/ISSFD-2017-013 Descent Isochrones in Martian Atmosphere |
Miljan Kolcic, Dusan Marceta
Department of Astronomy, Faculty of Mathematics, University of Belgrade, Serbia Abstract | Paper |
| 10:20 – 10:40 | ISTS-2017-d-014/ISSFD-2017-014 General Characteristics of Robust Orbit Insertion and Trajectory Design with MOI Robustness in MMX Mission |
Shota Takahashi1, Naoko Ogawa2, Yasuhiro Kawakatsu2
1Department of Mechanical Engineering, Keio University, Japan, 2Institute of Space and Astronautical Science, JAXA, Japan Abstract | Paper |
[d-5] |
Orbit Dynamics (Small Body) 1 |
Chairs: Hitoshi Ikeda (Japan Aerospace Exploration Agency, Japan) Daniel J. Scheeres (University of Colorado, USA) |
| 11:00 – 11:20 | ISTS-2017-d-017/ISSFD-2017-017 Assessing the Hazard Posed by Ryugu Ejecta Dynamics on Hayabusa2 Spacecraft |
Stefania Soldini, Yuichi Tsuda
Institute of Space and Astronautical Science/JAXA, Sagamihara, Japan Abstract | Paper |
| 11:20 – 11:40 | ISTS-2017-d-018/ISSFD-2017-018 Investigation of 1:1 Resonance in a Rotating 4th Degree and Order Gravitational Field |
Jinglang Feng1, Ron Noomen2, Xiyun Hou1, Pieter Visser2, Jianping Yuan3, Jingshi Tang1, Lin Liu1
1Nanjing University, China, 2Delft University of Technology, the Netherlands, 3Northwestern Polytechnic University, China. Abstract | Paper |
| 11:40 – 12:00 | ISTS-2017-d-019/ISSFD-2017-019 Orbital Stability Regions for Hypothetical Natural Satellites |
Samantha Rieger, Daniel Scheeres
Ann and H.J. Smead Department of Aerospace Engineering Sciences, University of Colorado Boulder, Boulder, Colorado, USA Abstract | Paper |
| 12:00 – 12:20 | ISTS-2017-d-020/ISSFD-2017-020 Stability Analysis of Orbital Motions around Uniformly Rotating Irregular Asteroids |
Xiyun Hou1, Daniel J. Scheeres2, Xiaosheng Xin1, Jinglang Feng1, Jingshi Tang1, Lin Liu1
1School of Astronomy and Space Science, Nanjing University, Nanjing, China, 2Department of Aerospace Engineering Sciences, The University of Colorado at Boulder, Boulder, USA Abstract | Paper |
| 12:20 – 12:40 | ISTS-2017-d-021/ISSFD-2017-021 On the Equilibrium Points of Doubly Synchronous Binary Asteroid Systems |
Xiaosheng Xin1,2, Xiyun Hou2,3, Lin Liu2,3, Guangliang Dong1
1Beijing Institute of Tracking and Telecommunication Technology, Beijing, China, 2School of Astronomy and Space Science, Nanjing University, Nanjing, China, 3Institute of Space Environment and Astrodynamics, Nanjing University, Nanjing, China Abstract | Paper |
[d-6] |
Trajectory Design & Optimization 2 |
Chairs: Naoko Ogawa (Japan Aerospace Exploration Agency, Japan) Mar Vaquero (NASA Jet Propulsion Laboratory, USA) |
| 11:20 – 11:40 | ISTS-2017-d-023/ISSFD-2017-023 Design of High-Energy Escape Trajectories with Lunar Gravity Assist |
Lorenzo Casalino, Lucio Filizola
Politecnico di Torino, Torino, Italy Abstract | Paper |
| 11:40 – 12:00 | ISTS-2017-d-024/ISSFD-2017-024 Matching of Patched-Hyperbolasfor Gravity-Assist Trajectory Design |
Yuki Kayama1, Chit Hong Yam2, Kenta Oshima3, Shuntaro Suda4, Yasuhiro Kawakatsu5
1TheUniversity of Tokyo, Japan, 2ispace, Japan, 3Waseda University, Japan, 4Hokkaido University, Japan, 5JAXA, Japan Abstract | Paper |
| 12:00 – 12:20 | ISTS-2017-d-179/ISSFD-2017-179 Patented Orbits Transfers and Manoeuvres Review |
Christophe R Koppel
KopooS Consulting Ind., Paris, France Abstract | Paper |
[d-7] |
Flight Dynamics Operations 2 |
Chairs: Takanori Iwata (JAXA, Japan) Stefano Pessina (EUMETSAT, Germany) |
| 14:00 – 14:20 | ISTS-2017-d-026/ISSFD-2017-026 Lessons Learned from Initial Sentinel-3A Maneuver Operations |
Daniel Aguilar Taboada1, Pier Luigi Righetti2, Rami Houdroge3
1CLC Space at EUMETSAT, Germany, 2EUMETSAT, Germany, 3Serco at EUMETSAT, Germany Abstract | Paper |
| 14:20 – 14:40 | ISTS-2017-d-027/ISSFD-2017-027 Sentinel-3A Flight Dynamics LEOP Operational Experience |
Mikel Catania1, Claudia Dietze2, Jochen Klein3
1LSE at European Space Operations Center, ESA, Darmstadt, Germany, 2CS at European Space Operations Center, ESA, Darmstadt, Germany, 3CGI at European Space Operations Center, ESA, Darmstadt, Germany Abstract | Paper |
| 14:40 – 15:00 | ISTS-2017-d-028/ISSFD-2017-028 Sentinel-1A: Flight Dynamics Analysis of the August 2016 Collision Event |
Petr Kuchynka1,a, Miguel Angel Martin Serrano1,b, Mikel Catania1,c, Xavier Marc1,d, Dirk Kuijper1,e, Vitali Braun2,a, Holger Krag2,b
1Flight Dynamics Division, European Space Operations Center, ESA (GMV INSYEN a), SCISYS b), LSE c), ESA d), CGI e)), Darmstadt, Germany, 2Space Debris Office, European Space Operations Center, ESA (ESA a), IMS b)), Darmstadt, Germany Abstract | Paper |
| 15:00 – 15:20 | ISTS-2017-d-029/ISSFD-2017-029 Sentinel-1B Flight Dynamics Operations during LEOP and Acquisition of its Reference Orbit: Achieving the Sentinel-1 Constellation |
André Vasconcelos1, Miguel A. Martín Serrano1, Javier Sánchez2, Xavier Marc3, Dirk Kuijper4
1Scisys GmbH at ESA/ESOC, Darmstadt, Germany, 2GMV at ESA/ESOC, Darmstadt, Germany, 3European Satellite Operations Centre (ESOC), ESA, Darmstadt, Germany, 4CGI at ESA/ESOC, Darmstadt, Germany Abstract | Paper |
[d-8] |
Orbit Dynamics (Small Body) 2 |
Chairs: Yasuhiro Kawakatsu (JAXA, Japan) Elisabet Canalias (CNES, France) |
| 14:00 – 14:20 | ISTS-2017-d-030/ISSFD-2017-030 Orbit-Attitude Coupled Dynamics of Solar Sail Spacecraft around Small Bodies |
Shota Kikuchi1, Yuichi Tsuda2, Jun’Ichiro Kawaguchi2
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
| 14:20 – 14:40 | ISTS-2017-d-031/ISSFD-2017-031 Reliability Analysis of Ballistic Landing in Binary Asteroid 65803 (1996GT) Didymos under Uncertainty and GNC Error Considerations |
Onur Celik1, Ozgur Karatekin2, Birgit Ritter2, Joan Pau Sánchez3
1Department of Space and Astronautical Science, The Graduate University for Advanced Studies (SOKENDAI), Sagamihara, Japan, 2Reference Systems and Planetology, the Royal Observatory of Belgium (ROB), Brussels, Belgium, 3Space Research Centre, School of Aerospace, Transport & Manufacturing, Cranfield University, Cranfield, United Kingdom Abstract | Paper |
| 14:40 – 15:00 | ISTS-2017-d-032/ISSFD-2017-032 Mascot: Analyses of the Descent and Bouncing Trajectories to Support the Landing Site Selection |
Laurence Lorda1, Elisabet Canalias1, Thierry Martin1, Romain Garmier2, Jens Biele3
1CNES, Toulouse, France, 2CS Système d’Informations, Toulouse, France, 3DLR, Cologne, Germany Abstract | Paper |
| 15:00 – 15:20 | ISTS-2017-d-033/ISSFD-2017-033 Small-Body Lander Simulations Using the GPU |
Stefaan Van Wal1, Robert Reid2, Daniel Scheeres1
1Colorado Center for Astrodynamics Research, University of Colorado Boulder, Boulder, Colorado, USA, 2Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, USA Abstract | Paper |
| 15:20 – 15:40 | ISTS-2017-d-034/ISSFD-2017-034 Family of Quasi-Stable Orbit around Asteroids in Strongly Perturbed Environment |
Yusuke Oki1, Yuichi Tsuda2, Jun’Ichiro Kawaguchi2
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
[d-9] |
Flight Dynamics Operations 3 |
Chairs: Takaya Inamori (Nagoya University, Japan) Pierluigi Righetti (EUMETSAT, Germany) |
| 16:00 – 16:20 | ISTS-2017-d-035/ISSFD-2017-035 Recent Developments and Future Directions in CCSDS Flight Dynamics Standards |
David S. Berry
California Institute of Technology, Jet Propulsion Laboratory, Pasadena, California, USA Abstract | Paper |
| 16:20 – 16:40 | ISTS-2017-d-036/ISSFD-2017-036 In-flight Characterisation and Calibration of Galileo FOC Reaction Control System |
Riccardo DI Corato1, Pere Ramos-Bosch2, Xavier Pena3
1SCISYS Deutschland GmbH @ESA/ESOC, Darmstadt, Germany, 2ESA/ESOC, Darmstadt, Germany, 3CNES, Toulouse, France Abstract | Paper |
| 16:40 – 17:00 | ISTS-2017-d-037/ISSFD-2017-037 Manoeuvre Optimization in the Galileo L7 Orbit Acquisition |
André Vasconcelos1, Pere Ramos Bosch2, Dave Hocken1, Javier Sánchez3, Gerald Ziegler1
1Scisys GmbH at ESA/ESOC, Darmstadt, Germany, 2European Satellite Operations Centre (ESOC), ESA, Darmstadt, Germany, 3GMV at ESA/ESOC, Darmstadt, Germany Abstract | Paper |
| 17:00 – 17:20 | ISTS-2017-d-038/ISSFD-2017-038 MICROSCOPE Mission: On-orbit Assessment of the Drag-Free and Attitude Control System |
Pascal Prieur1,2, Thomas Lienart1,3, Manuel Rodrigues4, Pierre Touboul5, Troelz Denver6, John L. Jørgensen6, Anastassia M. Bang6, Gilles Metris7
1Centre National d’Etudes Spatiales, 18 av Edouard Belin F31400 Toulouse, France, 2Department of Flight Dynamics, 3Department of Propulsion, 4ONERA, Département ‘Physique, Instrumentation, Environnement, Espace’, Chatillon, France, 5ONERA, Microscope space mission Prime Investigator, Palaiseau, France, 6Technical University of Denmark, Lyngby, Denmark, 7Université de la Cote d’Azur, Observatoire de la Côte d’Azur, CNRS, Géoazur, Valbonne, France Abstract | Paper |
| 17:20 – 17:40 | ISTS-2017-d-039/ISSFD-2017-039 A Comparison of Fuel Gauging Methods Utilising the Experience of S/C De-orbiting Operations |
Lutz Massonne
Telespazio VEGA Deutschland GmbH at ESA/ESOC, Darmstadt, Germany Abstract | Paper |
[d-10] |
Guidance, Navigation and Control (Small Body) |
Chairs: Jay McMahon (University of Colorado Boulder, USA) Sofya Spiridonova (German Space Operations Center, Germany) |
| 16:00 – 16:20 | ISTS-2017-d-041/ISSFD-2017-041 Autonomous Navigation of a Formation of Spacecraft in the Proximity of a Binary Asteroid |
Francesco Torre, Massimiliano Vasile, Romain Serra, Stuart Grey
Department of Mechanical and Aerospace Engineering, University of Strathclyde, Glasgow, United Kingdom Abstract | Paper |
| 16:20 – 16:40 | ISTS-2017-d-042/ISSFD-2017-042 Improved Shape Determination for Autonomous State Estimation |
Benjamin Bercovici, Jay Mcmahon
Department of Aerospace Engineering Sciences, University of Colorado at Boulder Abstract | Paper |
| 16:40 – 17:00 | ISTS-2017-d-043/ISSFD-2017-043 The High-fidelity Asteroid Deflection Evaluation Software (HADES):Assessing the Impact of Environmental and System Uncertainties on Autonomous Proximity Operations |
Massimo Vetrisano, Juan L. Cano, Simone Centuori
Deimos Space S.L.U., Madrid, Spain Abstract | Paper |
| 17:20 – 17:20 | ISTS-2017-d-044/ISSFD-2017-044 Range Measurement based Localization between Mothership and Lander Considering Asteroid Shape Using Particle Filter |
Hirokazu Ishida1, Yuichi Tsuda2
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
Program on Wednesday, 7 June.2017
[d-11] |
Attitude Dynamics |
Chairs: Yu Nakajima (Japan Aerospace Exploration Agency, Japan) Hirohisa Kojima (Tokyo Metropolitan University, Japan) |
| 9:00 – 9:20 | ISTS-2017-d-046/ISSFD-2017-046 Dynamical Modeling for Flat-Spin Recovery Applications |
Frank Janssens1, Jozef Van Der Ha2
1Consultant, Noordwijk, the Netherlands, 2Satellite Mission Design & Operations, Deming, WA, USA Abstract | Paper |
| 9:20 – 9:40 | ISTS-2017-d-047/ISSFD-2017-047 Utilisation of the “Dzhanibekov’s Effect” for the Possible Future Space Missions |
Pavel M. Trivailo1, Hirohisa Kojima2
1School of Engineering, RMIT University, Melbourne, Australia, 2Department of Aerospace Engineering, Tokyo Metropolitan University, Hino, Japan Abstract | Paper |
| 9:40 – 10:00 | ISTS-2017-d-048/ISSFD-2017-048 Dynamics of a Space Multi-pointing Stewart System Using the New Form of Kane’s Method |
Quan Hu, Fei Liu, Yao Zhang
School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China Abstract | Paper |
| 10:00 – 10:20 | ISTS-2017-d-049/ISSFD-2017-049 Optimal Fault-Tolerant Configurations of Thrusters |
Yasuhiro Yoshimura, Hirohisa Kojima
Aerospace Engineering, Tokyo Metropolitan University, Hino, Japan Abstract | Paper |
[d-12] |
Guidance, Navigation and Control (Landing) 1 |
Chairs: Satoshi Ikari (The University of Tokyo, Japan) Alexey Yu Kutomanov (TSNIImash, Russia) |
| 9:00 – 9:20 | ISTS-2017-d-050/ISSFD-2017-050 OMOTENASHI Trajectory Analysis and Design: Landing Phase |
Javier Hernando-Ayuso1, Stefano Campagnola2, Toshinori Ikenaga3, Tomohiro Yamaguchi3, Yusuke Ozawa1, Bruno V. Sarli4, Shota Takahashi5, Chit Hong Yam6
1The University of Tokyo, Japan, 2JPL, USA, 3JAXA, Japan, 4Catholic University of America, USA, 5Keio University, Japan, 6ispace technologies, Japan Abstract | Paper |
| 9:20 – 9:40 | ISTS-2017-d-052/ISSFD-2017-052 Fight Control of Flying Test Bed for Future Planetary Landing |
Takehiro Higuchi1, Toshiki Tamura1, Seiya Ueno1, Kazuhisa Fujita2, Takashi Ozawa2, Hiroki Takayanagi2
1Yokohama National University, Yokohama, Japan, 2Chofu Aerospace Center, JAXA, Tokyo, Japan Abstract | Paper |
| 9:40 – 10:00 | ISTS-2017-d-053/ISSFD-2017-053 A Study on Guidance Technique for Precise Lunar Landing |
Satoshi Ueda, Takahiro Ito, Shin-ichiro Sakai
Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
[d-13] |
Orbit Dynamics & Control 1 |
Chairs: Stefania Soldini (JAXA, Japan) Hodei Urrutxua (University of Southampton, UK) |
| 9:00 – 9:20 | ISTS-2017-d-055/ISSFD-2017-055 Harnessing the Sun’s Gravity for LEO to GEO Transfers |
Stijn De Smet1, Jeffrey S. Parker2, Daniel J. Scheeres1
1University of Colorado at Boulder, Boulder, CO, USA, 2Advanced Space, Boulder, CO, USA Abstract | Paper |
| 9:20 – 9:40 | ISTS-2017-d-056/ISSFD-2017-056 Systematic Study of the Dynamics about and between the Libration Points of the Sun-Earth-Moon System |
Bastien Le Bihan1, Josep J. Masdemont2, Gerard Gómez3, Stéphanie Lizy-Destrez1
1ISAE-Supaéro, Toulouse, France, 2IEEC & Departament de Matemàtiques, Universitat Politècnica de Catalunya, Barcelona, Spain, 3IEEC & Departament de Matemàtiques i Informàtica, Universitat de Barcelona, Barcelona, Spain Abstract | Paper |
| 9:40 – 10:00 | ISTS-2017-d-057/ISSFD-2017-057 Assessment of the Gaussian Covariance Approximation Over an Earth-Asteroid Encounter Period |
Daniel Mattern
Omitron, Inc., Beltsville, MD | NASA Goddard Space Flight Center, Flight Dynamics Facility, Greenbelt, MD Abstract | Paper |
| 10:00 – 10:20 | ISTS-2017-d-058/ISSFD-2017-058 Improved Reference Orbits for the Repeat-Ground-Track Missions EnMAP and Tandem-L |
Ralph Kahle, Sofya Spiridonova, Michael Kirschner
German Space Operations Center (DLR/GSOC), Wessling, Germany Abstract | Paper |
| 10:20 – 10:40 | ISTS-2017-d-059/ISSFD-2017-059 Nonlinear Uncertainty Propagation of Orbital Mechanics Subject to Stochastic Error in Atmospheric Mass Density Models |
Changyong He1,2, Yang Yang1,2, Brett Carter2, Han Cai1,2, Suqin Wu2, Kefei Zhang2
1Space Environment Research Centre (SERC) Limited, Australia, 2Satellite Positioning for Atmosphere, Climate and Environment (SPACE) Research Centre, School of Sciences, RMIT University, Australia Abstract | Paper |
[d-14] |
Attitude / Orbit Dynamics & Control |
Chairs: Yasuhiro Yoshimura (Tokyo Metropolitan University, Japan) Jozef C. van der Ha (Mission Design & Operations, USA) |
| 11:00 – 11:20 | ISTS-2017-d-060/ISSFD-2017-060 An Efficient Algorithm to Compute the SRP Force and Torque on Spacecraft |
Juan Manuel García1,2
1European Space Operations Center, ESA, Darmstadt, Germany, 2Flight Dynamics and Operations, GMV-Insyen AG, Darmstadt, Germany Abstract | Paper |
| 11:20 – 11:40 | ISTS-2017-d-061/ISSFD-2017-061 Optimal Design of Advanced Reflectivity Control Device for Solar Sails Considering Polarization Properties of Liquid Crystal |
Hirokazu Ishida1, Toshihiro Chujo1, Osamu Mori2, Junichiro Kawaguchi2
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
| 11:40 – 12:00 | ISTS-2017-d-062/ISSFD-2017-062 Optical Property Estimation by Precomputed Tensor Method for High-fidelity SRP Model |
Satoshi Ikari1, Kakeru Tokunaga1, Takahiro Ito2, Takaya Inamori3, Ryu Funase1, Shinichi Nakasuka1
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3Department of Micro-Nano System Engineering , Nagoya University, Nagoya, Japan Abstract | Paper |
| 12:00 – 12:20 | ISTS-2017-d-063/ISSFD-2017-063 Dynamics and Control of Modular and Extended Space Structures in Cislunar Environment |
Andrea Colagrossi, Michèle Lavagna
Aerospace Science and Technology Department, Politecnico di Milano, Milan, Italy Abstract | Paper |
| 12:20 – 12:40 | ISTS-2017-d-064/ISSFD-2017-064 Estimation of Shape and Optical Parameters of Spinning Solar Sail Equipped with Reflectivity Control Devices |
Akihiro Ishikawa, Kenshiro Oguri, Satoshi Ikari, Ryu Funase, Shinichi Nakasuka
Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan Abstract | Paper |
[d-15] |
Guidance, Navigation and Control (Landing) 2 |
Chairs: Takehiro Higuchi (Yokohama National University, Japan) |
| 11:00 – 11:20 | ISTS-2017-d-065/ISSFD-2017-065 Position and Displacement Estimation Using Crater-Based Line Segments for Pinpoint Lunar Landing |
Kazuki Kariya1, Takayuki Ishida2, Shujiro Sawai2,1, Seisuke Fukuda2,1
1Department of Space and Astronautical Science, SOKENDAI, Sagamihara, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
| 11:20 – 11:40 | ISTS-2017-d-066/ISSFD-2017-066 A Study of Terrain Feature Matching for Lunar Landing Navigation |
Yasuhiro Katayama1, Shigehito Shimizu2, Misuzu Haruki2, Shuhei Shigeto2, Isao Kawano2, Kazuhisa Fujita1
1Research and Development Directorate, JAXA, Chofu, Tokyo, Japan, 2Research and Development Directorate, JAXA, Tsukuba, Ibaraki, Japan Abstract | Paper |
| 11:40 – 12:00 | ISTS-2017-d-067/ISSFD-2017-067 The Robust Spacecraft Locaiton Estimation Algorithm toward the Misdetection Crater and the Undetected Crater in SLIM |
Haruyuki Ishii1, Keiki Takadama1, Akinori Murata1, Fumito Uwano1, Takato Tatsumi1, Yuta Umenai1, Kazuma Matsumoto1, Hiroyuki Kamata2, Takayuki Ishida3, Seisuke Fukuda4, Shujiro Sakai4, Shinichiro Sawai4
1Department of Information, The University of Electro-Communication, Tokyo, Japan, 2Department of Electrical engineering, Meiji University, Tokyo, Japan, 3Institute of Space and Astronautical Science, JAXA & ISAS, Sagamihara, Japan, 4Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
| 12:20 – 12:40 | ISTS-2017-d-069/ISSFD-2017-069 Evaluation of Landing Stability of Two-step Landing Method for Small Lunar-planetary Lander |
Shunpei Morikawa1, Hikaru Eguchi2, Yusuke Maru2,3, Taro Kawano3, Masahiro Nohmi1, Shujro Sawai2,3
1Department of Engineering, Shizuoka University, Shizuoka, Japan, 2Department of Space and Astronautical Science, The Graduate University for Advanced Studies(SOKENDAI), Sagamihara, Japan, 3Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
[d-16] |
Orbit Dynamics & Control 2 |
Chairs: Toshinori Ikenaga (Japan Aerospace Exploration Agency, Japan) Yue Wang (Beihang University, China) |
| 11:00 – 11:20 | ISTS-2017-d-071/ISSFD-2017-071 Orbit Uncertainty Propagation around Non-Spherical Bodies Using the Dromo Formulation |
Javier Hernando-Ayuso1, Claudio Bombardelli2
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Space Dynamics Groups, Technical University of Madrid, Spain Abstract | Paper |
| 11:20 – 11:40 | ISTS-2017-d-073/ISSFD-2017-073 Moon Mission Lifetime Analysis of a 2U CubeSat Equipped with Pulsed Plasma Thrusters; The Aoba-VELOX IV Mission Case |
Jose Rodrigo Cordova Alarcon1, Necmi Cihan Örger1, Sangkyun Kim1, Tran Quang Vinh2, Lim Wee Seng2, Bui Tran Duy Vu2, Mengu Cho1
1Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology, Japan, 2Nanyang Technology Institute, Singapore Abstract | Paper |
| 11:40 – 12:00 | ISTS-2017-d-074/ISSFD-2017-074 A Look at the Capture Mechanisms of the “Temporarily Captured Asteroids” of the Earth |
Hodei Urrutxua1, Claudio Bombardelli2
1Astronautics Group, University of Southampton, United Kingdom, 2Space Dynamics Group, Technical University of Madrid, Spain Abstract | Paper |
[d-17] |
Attitude Determination |
Chairs: Takanori Iwata (JAXA, Japan) Juan Manuel Garcia (GMV GmbH, ESOC, Germany) |
| 16:00 – 16:20 | ISTS-2017-d-075/ISSFD-2017-075 Study on an Advanced Attitude Determination Algorithm for the ERG Spacecraft |
Halil Ersin Söken, Shin-Ichiro Sakai, Kazushi Asamura, Yosuke Nakamura, Takeshi Takashima
Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
| 16:20 – 16:40 | ISTS-2017-d-076/ISSFD-2017-076 Labelling Technique for the Fast Star Identification |
Sangkyun Kim, Mengu Cho
Kyushu Institute of Technology, Japan Abstract | Paper |
| 16:40 – 17:00 | ISTS-2017-d-077/ISSFD-2017-077 Non-Traditional Robust UKF against Attitude Sensors Faults |
Demet Cilden Guler1, Halil Ersin Soken2, Chingiz Hajiyev1
1Department of Aeronautics and Astronautics, Istanbul Technical University, Istanbul, Turkey, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
| 17:00 – 17:20 | ISTS-2017-d-078/ISSFD-2017-078 Spinning Spacecraft Attitude Filtering with Spin Parameters: Performance Evaluation with Real Data |
Halil Ersin Söken1, Jozef C. Van Der Ha2, Shin-Ichiro Sakai2
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Satellite Mission Design and Operations, Deming, WA, USA Abstract | Paper |
| 17:20 – 17:40 | ISTS-2017-d-079/ISSFD-2017-079 Regularized Particle Filter with Roughening for Gyros Bias and Attitude Estimation using Simulated Measurements |
William Silva1, Roberta Garcia2, Hélio Kuga1, Maria Zanardi3
1Technological Institute of Aeronautics, ITA, São José dos Campos, Brazil, 2São Paulo University, USP, Lorena, Brazil, 3Federal University of ABC, UFABC, Santo André, Brazil Abstract | Paper |
[d-18] |
Guidance, Navigation and Control (Ascent/Descent/Deorbit) |
Chairs: Shinji Hokamoto (Kyushu University, Japan) Massimiliano L Vasile (University of Strathclyde, UK) |
| 16:00 – 16:20 | ISTS-2017-d-080/ISSFD-2017-080 Method of Safe Descent in Case of Off-nominal Onboard Situation on Russian Perspective manned Spacecraft “Federation” |
Alexey Yu. Kutomanov, Maxim M. Matushin, Vladimir N. Pochukaev
TSNIImash, Mission Control Centre Abstract | Paper |
| 16:20 – 16:40 | ISTS-2017-d-081/ISSFD-2017-081 Flight Control Stability of Multi-Hierarchy Dynamic Inversion for Winged Rocket |
Hiroshi Yamasaki, Koichi Yonemoto, Takahiro Fujikawa, Kent Shirakata, Hayato Tobiyama
Department of Mechanical and Control Engineering, Kyushu Institute of Technology, Fukuoka, Japan Abstract | Paper |
| 16:40 – 17:00 | ISTS-2017-d-082/ISSFD-2017-082 Deorbit Maneuver Strategy for the Three Themis Probes |
S. Frey1, V. Angelopoulos2, M. Bester1
1Space Sciences Laboratory, University of California, 7 Gauss Way, Berkeley, CA, 2ESS/IGPP, University of California, Los Angeles, 405 Hilgard Avenue, Los Angeles, CA Abstract | Paper |
| 17:20 – 17:40 | ISTS-2017-d-084/ISSFD-2017-084 The Study on Performance of MEMS IMU for Launch Vehicle under High Vibration Environment |
Eri Shimane1, Shuichi Matsumoto1, Takafumi Moriguchi2, Yuzo Iwai2, Ryohei Uchino2
1Japan Aerospace Exploration Agency, Tsukuba, Japan, 2Sumitomo Precision Products Co., Ltd., Amagasaki, Japan Abstract | Paper |
[d-19] |
Orbit Dynamics & Control 3 |
Chairs: Takanao Saiki (Japan Aerospace Exploration Agency, Japan) Pavel M. Trivailo (RMIT University, Australia) |
| 16:00 – 16:20 | ISTS-2017-d-085/ISSFD-2017-085 Study on Low-Thrust Stationkeeping on Geostationary Orbit |
Toshinori Ikenaga1, Masayoshi Utashima1, Yu Nakajima1, Toru Yamamoto1, Tadahiko Sano2, Noriyasu Inaba1
1Research and Development Directorate, JAXA, Ibaraki, Japan, 2Space Technology Directorate I, JAXA, Ibaraki, Japan Abstract | Paper |
| 16:20 – 16:40 | ISTS-2017-d-086/ISSFD-2017-086 Predictive Autonomous Orbit Control Method for Low Earth Orbit Satellites |
Jérôme Thomassin1, Maxime Ecochard2, Guillaume Azema2
1Department of Flight Dynamics, CNES, Toulouse, France, 2Spaceflight Dynamics Department, Thales Services, Toulouse, France Abstract | Paper |
| 16:40 – 17:00 | ISTS-2017-d-087/ISSFD-2017-087 De-orbiting Timing for Spacecraft in Geostationary Transfer Orbits Exploiting Luni-solar Perturbations |
Yue Wang1, Pini Gurfil2
1School of Astronautics, Beihang University, Beijing, China, 2Faculty of Aerospace Engineering, Technion–Israel Institute of Technology, Haifa, Israel Abstract | Paper |
| 17:00 – 17:20 | ISTS-2017-d-088/ISSFD-2017-088 Analysis of the Eccentricity Vector in Low Earth Orbits as Planar Rigid Body Motion |
Javier Sanchez, Petr Kuchynka
GMV at ESA/ESOC, Darmstadt, Germany Abstract | Paper |
Program on Thursday , 8 June.2017
[d-20] |
Formation Flying & Satellite Constellations 1 |
Chairs: Masayuki Ikeuchi (JAXA, Japan) Jean-Sébastien Ardaens (DLR, Germany) |
| 9:20 – 9:40 | ISTS-2017-d-091/ISSFD-2017-091 SAOCOM-CS: Flight Dynamics Operational Approach to a Highly Demanding Formation |
Itziar Barat1, Miguel Martin Serrano2, Bram de Vogeleer3, Berthyl Duesmann4, Cecilia Mezzera5
1Deimos-Space@ESA, ESTEC, Noordwijk, Netherlands, 2Scisys@ESA, ESOC, Darmstadt, Germany, 3Ims space consultancy@ESA, ESOC, Darmstadt, Germany, 4ESA, ESTEC, Noordwijk, Netherlands, 5ESA, ESTEC, Noordwijk, Netherlands, currently GMV, Trescantos, Spain Abstract | Paper |
| 9:40 – 10:00 | ISTS-2017-d-092/ISSFD-2017-092 Operational Flight Dynamics System for PROBA-3 Formation Flying Mission |
Pablo García, Catherine Praile, Jesús Robles
GMV, Madrid, Spain Abstract | Paper |
| 10:00 – 10:20 | ISTS-2017-d-093/ISSFD-2017-093 Performance of Contactless Micro Vibration Isolator Using Flux Pinning Effect |
Takuma Shibata1, Shin-Ichiro Sakai2
1Department of Aerospace and Astronautics Science, SOKENDAI, Kanagawa, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
[d-21] |
Orbit Determination 1 |
Chairs: Tsutomu Ichikawa (Japan Aerospace Exploration Agency, Japan) Tomas Jorge Martin-Mur (California Institute of Technology, USA) |
| 9:00 – 9:20 | ISTS-2017-d-094/ISSFD-2017-094 Monte for Orbit Determination |
Jonathon Smith, Theodore Drain, Shyam Bhaskaran, Tomas Martin-Mur
California Institute of Technology / Jet Propulsion Laboratory, Pasadena, California Abstract | Paper |
| 9:20 – 9:40 | ISTS-2017-d-095/ISSFD-2017-095 Multi-arc Orbit Determination to Determine Rosetta Trajectory and 67P Physical Parameters |
Bernard Godard1, Frank Budnik2, Gabriele Bellei3, Pablo Muñoz4, Trevor Morley1
1Telespazio VEGA Deutschland GmbH, located at ESOC, Germany, 2ESA/ESOC, Germany, 3Deimos Space, located at ESOC, Germany, 4GMV, located at ESOC, Germany Abstract | Paper |
| 9:40 – 10:00 | ISTS-2017-d-096/ISSFD-2017-096 Shadow Navigation Support at JPL for the Rosetta Landing on Comet 67P/ Churyumov-Gerasimenko |
Stephen Broschart1, Shyam Bhaskaran1, Julie Bellerose1, Ann Dietrich2, Dongsuk Han1, Robert Haw1, Nickolaos Mastrodemos1, William Owen, Jr.1, Brian Rush1, David Surovik3
1Jet Propulsion Laboratory, California Institute of Technology, California, USA, 2University of Colorado – Boulder, Colorado, USA, 3Rutgers University, New Jersey, USA Abstract | Paper |
| 10:00 – 10:20 | ISTS-2017-d-097/ISSFD-2017-097 A Quasi-Kinematic Orbit Determination Method for Deep Space Probes |
Hiroshi Takeuchi1, Tomohiro Yamaguchi1, Makoto Yoshikawa1, Tsutomu Ichikawa1, Naoko Ogawa1, Kazutaka Nishiyama1, Takanao Saiki1, Yuichi Tsuda1, Sho Taniguchi2, Nobuaki Fujii2, Tomoko Yagami2
1Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2Technical computing solutions unit, science solutions div, Fujitsu Limited, Tokyo, Japan Abstract | Paper |
| 10:20 – 10:40 | ISTS-2017-d-098/ISSFD-2017-098 Orbit Determination for Long-term Prediction of Solar Power Sail Demonstrator IKAROS |
Sho Taniguchi1, Takafumi Ohnishi1, Osamu Mori2, Hideki Kato2, Hiroshi Takeuchi2, Atsushi Tomiki2, Yuya Mimasu2, Naoko Ogawa2, Jun Matsumoto2, Taichi Ito2, Tsutomu Ichikawa2, Makoto Yoshikawa2, Shota Kikuchi3, Yosuke Kawabata3
1Technical computing solutions unit, science solutions div, Fujitsu Limited, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 3Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan Paper |
[d-22] |
Trajectory Design & Optimization 3 |
Chairs: Takayuki Yamamoto (JAXA, Japan) Hongru Chen (Chinese Academy of Sciences, China) |
| 9:20 – 9:40 | ISTS-2017-d-100/ISSFD-2017-100 Optimised GTO-GEO Transfer Using Low-Thrust Propulsion |
Marilena DI Carlo1, Massimiliano Vasile1, Stephen Kemble2
1Department of Mechanical and Aerospace Engineering, University of Strathclyde, Glasgow, United Kingdom, 2Airbus Defence and Space, Stevenage, United Kingdom Abstract | Paper |
| 9:40 – 10:00 | ISTS-2017-d-101/ISSFD-2017-101 Minimum Time Orbit Raising of Geostationary Spacecraft by Optimizing Feedback Gain of Steering-law |
Kenji Kitamura1, Katsuhiko Yamada2, Takeya Shima1
1Advanced Technology R&D Center, Mitsubishi Electric Corporation, Amagasaki, Japan, 2Graduate School of Engineering, Osaka University, Osaka, Japan Abstract | Paper |
| 10:00 – 10:20 | ISTS-2017-d-102/ISSFD-2017-102 Operational Concept for Orbit Raising with Low Thrust |
Ferdi DE Bruijn, Francesca Letizia, Juan C. Bastante
OHB System AG, Bremen, Germany Abstract | Paper |
| 10:20 – 10:40 | ISTS-2017-d-103/ISSFD-2017-103 Indirect Optimization of End-of-Life Disposal for Galileo Constellation Using Low Thrust Propulsion |
Juan Luis Gonzalo1, Francesco Topputo2, Roberto Armellin3
1School of Aerospace Engineering – ETSIAE, Technical University of Madrid – UPM, Madrid, Spain, 2Dipartimento di Scienze e Tecnologie Aerospaziali, Politecnico di Milano, Milan, Italy, 3Surrey Space Center, University of Surrey, Guildford, UK Abstract | Paper |
[d-23] |
Formation Flying & Satellite Constellations 2 |
Chairs: Tatsuaki Hashimoto (Japan Aerospace Exploration Agency, Japan) Berthyl Duesmann (European Space Agency, Netherlands) |
| 11:00 – 11:20 | ISTS-2017-d-104/ISSFD-2017-104 Optimal Configurations for Nanosatellite Formation Flying in Binary Asteroid Environment |
Andrea Capannolo, Michèle Lavagna, Fabio Ferrari, Paolo Lunghi
Department of Aerospace Sciences and Technologies, Politecnico di Milano, Milan, Italy Abstract | Paper |
| 11:20 – 11:40 | ISTS-2017-d-105/ISSFD-2017-105 Relative Spiral Trajectories for Low-Thrust Formation Flying |
Matthew Willis1, Simone D’Amico2
1Department of Mechanical Engineering, Stanford University, USA, 2Department of Aeronautics and Astronautics, Stanford University, USA Abstract | Paper |
| 11:20 – 11:40 | ISTS-2017-d-106/ISSFD-2017-106 Optimal Trajectory Design of Formation Flying based on Attractive Sets |
Motoki Yamane, Mai Bando, Shinji Hokamoto
Department of Aeronautics and Astronautics, Kyushu University, Fukuoka, Japan Abstract | Paper |
[d-24] |
Orbit Determination 2 |
Chairs: Hiroshi Takeuchi (JAXA, Japan) Shyam Bhaskaran (JPL, USA) |
| 11:00 – 11:20 | ISTS-2017-d-107/ISSFD-2017-107 Radar Observations of Spacecraft in Lunar Orbit |
Marina Brozović1, Ryan S. Park1, Joseph G. Mcmichael1, Jon D. Giorgini1, Martin A. Slade1, David S. Berry1, Joseph S. Jao1, Frank D. Ghigo2, Patrick A. Taylor3, Edgard Rivera-Valentín3
1Jet Propulsion Laboratory/California Institute of Technology, Pasadena, California, USA, 2Green Bank Observatory, Green Bank, West Virginia, USA, 3Arecibo Observatory/Universities Space Research Association, Arecibo, Puerto Rico, USA Abstract | Paper |
| 11:20 – 11:40 | ISTS-2017-d-108/ISSFD-2017-108 Orbit Determination Adaptations for the Cassini Grand Finale |
Zahi Tarzi, Julie Bellerose, Duane Roth, Rodica Ionasescu, Dylan Boone, Kevin Criddle
California Institute of Technology, Jet Propulsion Laboratory, Pasadena, USA Abstract | Paper |
| 11:40 – 12:00 | ISTS-2017-d-109/ISSFD-2017-109 Resolution of Orbit Determination Prediction Instabilities at Titan During Cassini’s Solstice Mission |
Dylan Boone, Julie Bellerose, Duane Roth
Cassini Navigation Team, Jet Propulsion Laboratory, California Institute of Technology Abstract | Paper |
| 12:00 – 12:20 | ISTS-2017-d-110/ISSFD-2017-110 50,000 Laps Around Mars: Navigating the Mars Reconnaissance Orbiter Through the Extended Missions (January 2009 – March 2017) |
Premkumar Menon, Sean Wagner, Stuart Demcak, David Jefferson, Eric Graat, Kyong Lee, William Schulze
Jet Propulsion Laboratory, California Institute of Technology, USA Abstract | Paper |
[d-25] |
Trajectory Design & Optimization 4 |
Chairs: Massimo Casasco (European Space Agency, Netherlands) Volker Maiwald (German Aerospace Center, Germany) |
| 11:00 – 11:20 | ISTS-2017-d-112/ISSFD-2017-112 Approximate Two-Point Boundary Value Problem Solutions to Low Thrust Trajectory by Superposition |
Ming Tony Shing1, Chit Hong Yam2, Albert Wai Kit Lau1
1Department of Physics, Hong Kong University of Science and Technology, Hong Kong, 2ispace inc., Tokyo Japan Abstract | Paper |
| 11:20 – 11:40 | ISTS-2017-d-113/ISSFD-2017-113 Low-Thrust Trajectory Optimization with No Initial Guess |
Nathan L. Parrish, Daniel J. Scheeres
Colorado Center for Astrodynamics Research, University of Colorado, Boulder, USA Abstract | Paper |
| 11:40 – 12:00 | ISTS-2017-d-114/ISSFD-2017-114 A Minimum-Fuel Fixed-Time Low-Thrust Rendezvous Solved with the Switching Systems Theory |
Clément Gazzino1, Denis Arzelier1, Luca Cerri2, Damiana Losa3, Christophe Louembet1, Christelle Pittet2
1LAAS-CNRS, Université de Toulouse, France, 2CNES, Centre Spatial de Toulouse, France, 3Thales Alenia Space, France Abstract | Paper |
| 12:00 – 12:20 | ISTS-2017-d-115/ISSFD-2017-115 Open Source Implementation of A Fast and Precise N-body Low-Thrust Propagator |
Weichen Xiao1, Chit Hong Yam2, Wen Han Chiu1
1Department of Physics, The Hong Kong University of Science and Technology, Hong Kong, 2ispace inc., Tokyo, Japan Abstract | Paper |
| 12:20 – 12:40 | ISTS-2017-d-116/ISSFD-2017-116 Unified Formulation for Element-Based Indirect Trajectory Optimization |
Juan Luis Gonzalo1, Claudio Bombardelli1, Francesco Topputo2
1School of Aerospace Engineering – ETSIAE, Technical University of Madrid – UPM, Madrid, Spain, 2Dipartimento di Scienze e Tecnologie Aerospaziali, Politecnico di Milano, Milan, Italy Abstract | Paper |
[d-26] |
Formation Flying & Satellite Constellations 3 |
Chairs: Kenji Kitamura (Mitsubishi Electric Corporation, Japan) Andres Ayala (GMW for European Space Agency, Netherlands) |
| 14:00 – 14:20 | ISTS-2017-d-117/ISSFD-2017-117 Rendezvous Control of Spacecrafts via Constrained Optimal Control Using Generating Functions |
Dijian Chen1, Kenji Fujimoto2
1Department of Mechanical Science and Engineering, Nagoya University, Nagoya, Japan, 2Department of Aeronautics and Astronautics, Kyoto University, Kyoto, Japan Abstract | Paper |
| 14:20 – 14:40 | ISTS-2017-d-118/ISSFD-2017-118 Attitude and Orbit Coupled Tumbling Space Debris Tracking Control |
Shuquan Wang1, Lingchao Zhu1,2
1Technology and Engineering Center for Space Utilization, China Academy of Sciences, Beijing, China, 2University of Chinese Academy of Sciences, Beijing, China Abstract | Paper |
| 14:40 – 15:00 | ISTS-2017-d-119/ISSFD-2017-119 Angles-Only Relative Orbit Determination during the AVANTI Experiment |
Jean-Sébastien Ardaens, Gabriella Gaias
German Space Operations Center (DLR/GSOC), Wessling, Germany Abstract | Paper |
| 15:00 – 15:20 | ISTS-2017-d-120/ISSFD-2017-120 Effect of Observation by Angle Only Navigation to Plan Non-Cooperative Approach for ADR |
Masayuki Ikeuchi
Safety and Mission Assurance Department, JAXA, Sagamihara, Japan Abstract | Paper |
[d-27] |
Orbit Determination 3 |
Chairs: Makoto Yoshikawa (Japan Aerospace Exploration Agency, Japan) Frank Budnik (ESA, Germany) |
| 14:00 – 14:20 | ISTS-2017-d-122/ISSFD-2017-122 On-Board Orbit Determination for a Deep Space CubeSat |
Boris Segret1, Daniel Hestroffer2, Gary Quinsac3, Marco Agnan4, Jordan Vannitsen4,5
1Laboratory of Excellence for Exploration of Space Environments (LabEx ESEP), Paris Observatory, Paris, France, 2Institut de Mecanique Celeste et de Calcul des Ephemerides (IMCCE), Paris Observatory, Paris, France, 3Paris Sciences Lettres (PSL) Research University, Paris Observatory, Paris, France, 4ODYSSEUS Space Co. Ltd., Tainan, Taiwan, 5Department of Aeronautics and Aerospace (DAA), National Cheng Kung University (NCKU), Tainan, Taiwan Abstract | Paper |
| 14:20 – 14:40 | ISTS-2017-d-123/ISSFD-2017-123 A Study of the Navigation for Spacecraft by Using the Modified Estimator |
Tsutomu Ichikawa
Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
| 15:00 – 15:20 | ISTS-2017-d-015/ISSFD-2017-015 Rosetta Navigation during the End of Mission Phase |
Pablo Muñoz1, Vicente Companys2, Frank Budnik2, Bernard Godard3, Dario Pellegrinetti1, Gabriele Bellei4, Rainer Bauske5, Waldemar Martens2
1GMV at ESOC, Darmstadt, Germany, 2ESA/ESOC, Darmstadt, Germany, 3Telespazio Vega at ESOC, Darmstadt, Germany, 4Deimos Space at ESOC, Darmstadt, Germany, 5Terma at ESOC, Darmstadt, Germany Abstract | Paper |
[d-28] |
Trajectory Design & Optimization 5 |
Chairs: Jun Matsumoto (Japan Aerospace Exploration Agency, Japan) Yanping Guo (Johns Hopkins University Applied Physics Laboratory, USA) |
| 14:00 – 14:20 | ISTS-2017-d-126/ISSFD-2017-126 A Smoothed Eclipse Model for Solar Electric Propulsion Trajectory Optimization |
Jonathan D. Aziz1, Daniel J. Scheeres1, Jeffrey S. Parker1, Jacob A. Englander2
1University of Colorado Boulder, USA, 2NASA Goddard Space Flight Center, USA Abstract | Paper |
| 14:20 – 14:40 | ISTS-2017-d-127/ISSFD-2017-127 Robust Differential Dynamic Programming for Low-Thrust Trajectory Design:Approach with Robust Model Predictive Control Technique |
Naoya Ozaki1, Stefano Campagnola2, Ryu Funase1
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Jet Propulsion Laboratory, NASA, Pasadena, California Abstract | Paper |
| 14:40 – 15:00 | ISTS-2017-d-128/ISSFD-2017-128 Initial Results of a New Method for Optimizing Low-Thrust Gravity-Assist Missions |
Volker Maiwald
Institute of Space Systems, German Aerospace Center (DLR), Department of System Analysis Space Segment, Germany Abstract | Paper |
| 15:00 – 15:20 | ISTS-2017-d-129/ISSFD-2017-129 Design and Validation of Ultra Low Thrust Transfers to the Sun-Earth Saddle Point with Application to LISA Pathfinder Mission Extension |
Francesco Topputo1, Diogene Alessandro Dei Tos1, Mirco Rasotto2, Florian Renk3
1Politecnico di Milano, Department of Aerospace Science and Technology, Milan, Italy, 2Dinamica Srl, Milan, Italy, 3European Space Operation Center (ESOC), Darmstadt, Germany Abstract | Paper |
| 15:20 – 15:40 | ISTS-2017-d-130/ISSFD-2017-130 Solar Power Sail Trajectory Design for Jovian Trojan Exploration |
Takanao Saiki, Jun Matsumoto, Osamu Mori, Jun’Ichiro Kawaguchi
Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
[d-29] |
Formation Flying & Satellite Constellations 4 |
Chairs: Kenji Fujimoto (Kyoto University, Japan) Ralph Kahle (DLR, Germany) |
| 16:00 – 16:20 | ISTS-2017-d-131/ISSFD-2017-131 Robust and Safe N-Spacecraft Swarming in Perturbed Near-Circular Orbits |
Adam W. Koenig, Simone D’Amico
Department of Aeronautics and Astronautics, Stanford University, Stanford, California, USA Abstract | Paper |
| 16:20 – 16:40 | ISTS-2017-d-132/ISSFD-2017-132 Satellite Constellations for Altimetry |
Alain Lamy, Josiane Costeraste
CNES – Centre National d’Etudes Spatiales, Toulouse, France Abstract | Paper |
| 16:40 – 17:00 | ISTS-2017-d-134/ISSFD-2017-134 Galileo Extended Slots Characterisation and Relation with the Nominal Constellation |
Andrés Ayala1, Rubén Castro2, Nityaporn Sirikan3, Daniel Blonski3, Daniel Navarro3
1ESTEC, European Space Agency, GMV, Noordwijk, The Netherlands, 2ESTEC, European Space Agency, WGS, Noordwijk, The Netherlands, 3ESTEC, European Space Agency, ESA, Noordwijk, The Netherlands Abstract | Paper |
[d-30] |
Orbit Determination 4 |
Chairs: Sho Taniguchi (Fijitsu Limited., Japan) Jonathon J Smith (California Institute of Technology / Jet Propulsion Laboratory, USA) |
| 16:00 – 16:20 | ISTS-2017-d-135/ISSFD-2017-135 Deep-Space Navigation Using Optical Communications Systems |
Tomas Martin-Mur, Sarah Elizabeth Mccandless, Reza Karimi
Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, USA Abstract | Paper |
| 16:20 – 16:40 | ISTS-2017-d-136/ISSFD-2017-136 The Effectiveness of Solution Technique on the Autonomous Orbit Determination Accuracy of Lagrangian Navigation Constellation |
Youtao Gao1, Bingyu Jin1, Tanran Zhao1, Bo Xu2
1College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing, China, 2College of Astronomy and Space Science, Nanjing University, Nanjing, China Abstract | Paper |
| 16:40 – 17:00 | ISTS-2017-d-138/ISSFD-2017-138 Simplified Covariance Estimation and Target Observation Management Method for On-Board Optical Navigation of Deep Space Probe |
Yosuke Kawabata1, Takanao Saiki2, Yasuhiro Kawakatsu2
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
| 17:00 – 17:20 | ISTS-2017-d-139/ISSFD-2017-139 Autonomous Orbit Determination of Multiple Spacecraft Using Active Sensing with Satellite-to-Satellite Tracking |
Kota Kakihara, Naoya Ozaki, Ryu Funase
Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan Abstract | Paper |
Program on Thursday , 9 June.2017
[d-31] |
Orbit Determination 5 |
Chairs: Takanori Iwata (JAXA, Japan) Pierluigi Righetti (EUMETSAT, Germany) |
| 14:00 – 14:20 | ISTS-2017-d-140/ISSFD-2017-140 Generalized Image Navigation & Registration Method Based on Kalman Filter |
Ahmed A. Kamel1, Handol Kim2, Dochul Yang2, Chul-Min Park3, Jin Woo4
1Kamel Engineering Services, Los Angeles, California, USA, 2Korea Aerospace Research Institute, Daejeon, ROK, 3Korea Aerospace Industries, ROK, 4Korea Meteorological Administration, Daebang-dong, ROK Abstract | Paper |
| 14:20 – 14:40 | ISTS-2017-d-141/ISSFD-2017-141 Satellite Autonomous Navigation with No Ground Links for Korea Regional Navigation Satellite System |
Hyungjik Oh1, Young-Rok Kim2, Chandeok Park1, Seung-Mo Seo3
1Department of Astronomy, Yonsei University, Seoul 03722, Republic of Korea, 2Korea Aerospace Research Institute, Daejeon, Republic of Korea, 3Agency for Defense Development, Daejeon, Republic of Korea Abstract | Paper |
| 15:00 – 15:20 | ISTS-2017-d-143/ISSFD-2017-143 Filter Tuning Using the Chi-squared Statistic |
Tyler Lilly-Salkowski
Omitron, Inc., USA Abstract | Paper |
| 15:20 – 15:40 | ISTS-2017-d-144/ISSFD-2017-144 Generalised Polynomial Chaos Based Particle Filter for Orbit Determination |
Yang Yang1,2, Yanlong Bu3
1SPACE Research Centre, School of Science, RMIT University, Melbourne, Australia, 2Space Environment Research Centre, Canberra, Australia, 3Beijing Aerospace Control Centre, Beijing, China Abstract | Paper |
[d-32] |
Mission Analysis & Design 1 |
Chairs: Katsuhiko Yamada (Osaka University, Japan) Natan Eismont (Space Research Institute of the Russian Academy of Sciences, Russia) |
| 14:00 – 14:20 | ISTS-2017-d-145/ISSFD-2017-145 Advanced methods of low cost mission design for Jovian moons exploration |
Alexey Grushevskii, Yuri Golubev, Victor Koryanov, Andrey Tuchin, Denis Tuchin
KIAM (Keldysh Institute of Applied Mathematics of RAS), Russian Federation Abstract | Paper |
| 14:20 – 14:40 | ISTS-2017-d-146/ISSFD-2017-146 Solar Probe Plus: Primary and Backup Launch Windows |
Yanping Guo
The Johns Hopkins University Applied Physics Laboratory, Maryland, USA Abstract | Paper |
| 14:40 – 15:00 | ISTS-2017-d-147/ISSFD-2017-147 Solar Orbiter Trajectory Profile and Navigation Challenges |
José Manuel Sánchez Pérez, Frank Budnik
European Space Agency, ESA, ESOC, Darmstadt, Germany Abstract | Paper |
| 15:00 – 15:20 | ISTS-2017-d-148/ISSFD-2017-148 AIDA: Measuring Asteroid Binary System Parameters and DART-Imparted Deflection using the AIM Spacecraft |
Julie Bellerose, Shyamkumar Bhaskaran, Steven Chesley
California Institute of Technology, Jet Propulsion Laboratory, Pasadena, USA Abstract | Paper |
| 15:20 – 15:40 | ISTS-2017-d-149/ISSFD-2017-149 Guidance Navigation and Control Challenges for the ESA Asteroid Impact Mission |
Massimo Casasco1, Jesus GIL Fernandez1, Guillermo Ortega1, Ian Carnelli2
1European Space Technology Centre, Noordwijk, The Netherlands;, 2European Space Agency Headquarters, Paris, France Abstract | Paper |
[d-33] |
Attitude Control 1 |
Chairs: Hirohisa Kojima (Tokyo Metropolitan University, Japan) |
| 14:00 – 14:20 | ISTS-2017-d-150/ISSFD-2017-150 LMI-based Mixed H2/H∞ Control with Regional Constraints for Spacecraft Attitude Tracking |
Takahiro Sasaki1,2,3, Takashi Shimomura1, Sayaka Kanata1
1Department of Aerospace Engineering, Osaka Prefecture University, Osaka, Japan, 2Department of Aerospace Engineering Science, University of Colorado Boulder, Colorado, USA, 3Research Fellow of Japan Society for the Promotion of Science (DC1) Abstract | Paper |
| 14:20 – 14:40 | ISTS-2017-d-151/ISSFD-2017-151 Fast Slew Maneuvers for the High-Torque-Wheels BIROS Satellite |
Paul Acquatella B.
DLR, German Aerospace Center, Institute of System Dynamics and Control, Oberpfaffenhofen, Germany Abstract | Paper |
| 14:40 – 15:00 | ISTS-2017-d-152/ISSFD-2017-152 Single Axis Pointing for Underactuated Spacecraft with a Residual Angular Momentum |
Alessandro Zavoli1, Fabrizio Giulietti2, Giulio Avanzini3, Guido de Matteis1
1Department of Mechanical and Aerospace Engineering, ‘Sapienza’ Università di Roma, Rome, Italy, 2Department of Industrial Engineering, Università di Bologna (ForlÌ Campus), ForlÌ, Italy, 3Department of Engineering for Innovation, Università del Salento, Lecce, Italy Abstract | Paper |
| 15:00 – 15:20 | ISTS-2017-d-153/ISSFD-2017-153 Model Error Compensator for Attitude Control of 2-Wheel Spacecraft with On-line FRIT based Tuning |
Hiroaki Endo, Kazuma Sekiguchi, Kenichiro Nonaka
Department of Mechanical Systems Engineering, Tokyo City University,Tokyo, Japan Abstract | Paper |
[d-34] |
Orbit Determination 6 |
Chairs: Frank Budnik (ESA, Germany) Yang Yang (RMIT University, Australia) |
| 16:00 – 16:20 | ISTS-2017-d-155/ISSFD-2017-155 Orbit Determination for the MICROSCOPE Mission Specificities and Performance |
David Pascal, John Moyard, Flavien Mercier, Pierre-Yves Guidotti, Thomas Junique, Romain Mathieu
CNES, Toulouse, France Abstract | Paper |
| 16:20 – 16:40 | ISTS-2017-d-156/ISSFD-2017-156 Optical Tracking Extended Network in Support to Operational Flight Dynamics and Conjunction Analysis for Meteosat |
Milan Klinc1, Stefano Pessina2
1Independent Consultant at EUMETSAT, Flight Operations Division, EUMETSAT, Darmstadt, Germany, 2Flight Operations Division, EUMETSAT, Darmstadt, Germany Abstract | Paper |
[d-35] |
Mission Analysis & Design 2 |
Chairs: Ryu Funase (The University of Tokyo, Japan) Alain Lamy (CNES, France) |
| 16:00 – 16:20 | ISTS-2017-d-158/ISSFD-2017-158 Mission Design Problems for Spectrum-Roentgen-Gamma Project |
Ravil Nazirov1, Natan Eismont1, Vadim Arefiev1, Fedor Korotkov1, Andrei Pogodin2, Andrei Tregubov3, Alexey Ditrikh3
1Space Research Institute of the Russian Academy of Sciences, Russia, 2Lavochkin Association, Russia, 3Russian Space Corporation Energia Abstract | Paper |
| 16:20 – 16:40 | ISTS-2017-d-159/ISSFD-2017-159 EQUULEUS Mission Analysis: Design of the Transfer Phase |
Kenta Oshima1, Stefano Campagnola2, Chit Hong Yam3, Yuki Kayama4, Yasuhiro Kawakatsu5, Naoya Ozaki6, Quentin Verspieren6, Kota Kakihara6, Kenshiro Oguri6, Ryu Funase6
1Department of Applied Mechanics and Aerospace Engineering, Waseda University, Tokyo, Japan, 2Jet Propulsion Laboratory, California Institute of Technology, CA, USA, 3ispace inc., Tokyo, Japan, 4Department of Advanced Energy, The University of Tokyo, Tokyo, Japan, 5Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 6Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan Abstract | Paper |
| 16:40 – 17:00 | ISTS-2017-d-072/ISSFD-2017-072 EQUULEUS Mission Analysis: Design of the Science Orbit Phase |
Kenshiro Oguri1, Kota Kakihara1, Stefano Campagnola2, Naoya Ozaki1, Kenta Oshima3, Tomohiro Yamaguchi4, Ryu Funase1
1Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan, 2Jet Propulsion Laboratory, California Institute of Technology, CA, USA, 3Department of Applied Mechanics and Aerospace Engineering, Waseda University, Tokyo, Japan, 4Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan Abstract | Paper |
| 17:00 – 17:20 | ISTS-2017-d-160/ISSFD-2017-160 Preliminary Mission Design and Analysis of a Lunar Far-side Positioning CubeSat Mission |
Hongru Chen1, Lei Liu2,3, Yazhe Meng1,4, Zhenyu Xu1,4, Long Long1,4, Jiangkai Liu1,4
1Key Labrotary of Space Utilization, Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences, Beijing, China, 2College of Science, National University of Defense Technology, Changsha, China, 3Beijing Aerospace Control Center, Beijing, China, 4University of Chinese Academy of Sciences, Beijing, China Abstract | Paper |
| 17:20 – 17:40 | ISTS-2017-d-161/ISSFD-2017-161 SIRIUS-DV: The New Flight Dynamics Algorithms for the Future CNES Missions |
Iván Llamas1, Yannick Tanguy2, Michel Lacotte2, Jean-Jacques Wasbauer2
1GMV, Madrid, Spain, 2CNES, Toulouse, France Abstract | Paper |
[d-36] |
Attitude Control 2 |
Chairs: Takashi Shimomura (Osaka Prefecture University, Japan) Alessandro Zavoli (Rome – Sapienza, Italy) |
| 16:00 – 16:20 | ISTS-2017-d-162/ISSFD-2017-162 Experimental Study on Line-of-Sight (LOS) Attitude Control Using Control Moment Gyros under Micro-Gravity Environment |
Hirohisa Kojima, Kana Hiraiwa, Yasuhiro Yoshimura, Koki Hidaka
Department of Aerospace Engineering, Tokyo Metropolitan University, Hino, Japan Abstract | Paper |
| 16:20 – 16:40 | ISTS-2017-d-163/ISSFD-2017-163 Attitude Control using Three Control Moment Gyros |
Sho Nonomura1, Andrew Meldrum2, Katsuhiko Yamada1, Yasuhiro Shoji1
1Graduate School of Engineering, Osaka University, Osaka, Japan, 2School of Engineering, Osaka University, Osaka, Japan Abstract | Paper |
| 16:40 – 17:00 | ISTS-2017-d-164/ISSFD-2017-164 Conceptual Study of 6 DOF Precision Control of Payload Using 6 Axis Hybrid Actuator |
Norimasa Yoshida1, Seiichi Shimizu2, Kazuhide Kodeki2
1Department of Aerospace Engineering, Osaka Prefecture University, Sakai, Japan, 2Advanced Technology R&D Center, Mitsubishi Electric Corp, Amagasaki, Japan Abstract | Paper |
| 17:00 – 17:20 | ISTS-2017-d-165/ISSFD-2017-165 Singularity Avoidance/Passage Steering Logic for a Variable-speed Double-gimbal Control Moment Gyro Based on Inverse Kinematics |
Shota Kawajiri1, Saburo Matunaga2
1Department of Mechanical and Aerospace Engineering, Tokyo Institute of Technology, Tokyo, Japan, 2Department of Mechanical Engineering, Tokyo Institute of Technology, Tokyo, Japan Abstract | Paper |
| 17:20 – 17:40 | ISTS-2017-d-166/ISSFD-2017-166 Optimal Attitude Control for Spacecraft Using Two Variable-Speed Control Moment Gyros |
Daiki Higashiyama, Katsuhiko Yamada, Yasuhiro Shoji
Graduate School of Engineering, Osaka University, Osaka, Japan Abstract | Paper |
Technical Session Poster
Program on Wednesday, 7June.2017
ISTS-2017-d-167p/ISSFD-2017-167p Formation Flying in Space-Borne Artificial Magnetic Dipole Field |
Yu Cheng1,2, Gerard GóMez1,2, Josep J. Masdemont3, Jianping Yuan1
1School of Astronautics, Northwestern Polytechnical University, Xi’an, China, 2IEEC & Department de Matemàtiques i Informàtica, Universitat de Barcelona, Barcelona, Spain, 3IEEC & Department de Matemàtiques, Universitat Politècnica de Catalunya, Barcelona, Spain Abstract | Paper |
|
ISTS-2017-d-168p/ISSFD-2017-168p Reducing the Lunisolar Numerical Ephemerides for Onboard Applications |
Jingshi Tang1,2, Haishuo Wang1, Hanyang Liu1, Guanshan Pu1, Lin Liu1,2
1School of Astronomy and Space Science, Nanjing University, China, 2Institute of Space Environment and Astrodynamics, Nanjing University, China Abstract | Paper |
|
ISTS-2017-d-171p/ISSFD-2017-171p The Orbit Maneuvers for Full-Parameter Reentry of Spacecraft |
Gefei Li
Beijing Aerospace Control Centre,Beijing,China, China |
|
ISTS-2017-d-172p/ISSFD-2017-172p Dynamics and Mission Design for Space Debris Mitigation in the Geostationary Orbits |
William Silva1, Maisa Terra1, Claudia Celestino2, Cristiano Melo3
1Technological Institute of Aeronautics, ITA, São José dos Campos, Brazil, 2Federal University of ABC, UFABC, Santo André, Brazil, 3Federal University of Minas Gerais, UFMG, Belo Horizonte, Brazil Abstract | Paper |
|
ISTS-2017-d-173p/ISSFD-2017-173p Altitude and Motion Estimation for Autonomous Vehicles through Wide-Field-Integration of Optic Flow |
Ryusuke Nakata, Naoto Kobayashi, Mai Bando, Shinji Hokamoto
Department of Aeronautics and Astronautics, Kyushu University, Fukuoka, Japan Abstract | Paper |
|
ISTS-2017-d-175p/ISSFD-2017-175p Theoretical Analysis on Zero Propellant Maneuver Existent Conditions |
Mo-Yao Yu, Ya-Zhong Luo1,2, Hai-Yang Li2
1College of Aerospace Science and Engineering, 2National University of Defense Technology, Changsha, China Abstract | Paper |
|
ISTS-2017-d-176p/ISSFD-2017-176p Autonomous Orbit Determination of Satellites around Triangular Libration Points in the Earth-Moon System |
Bin Liu, Xinyun Hou, Jingshi Tang, Lin Liu
School of Astronomy and Space Science, Nanjing University, China |
|
ISTS-2017-d-178p/ISSFD-2017-178p SAOCOM-CS: Definition of Orbital Requirements for Tomographic Phase |
Cecilia Mezzera1, Itziar Barat2, Berthyl Duesmann1, Stefano Tebaldini3, Mario Azcueta3, Bram de Vogeleer4
1European Space Agency, Netherlands, 2Deimos-Space@ESA, 3Politecnico di Milano, 4Ims space consultancy @ESA |
Finalist Student Session
Program on Thursday , 8 June.2017
| 10:20 – 10:40 | 2017-s-05-d Low-Thrust Trajectory Design to Improve Overall Mission Success Probability Incorporating Target Changes in Case of Engine Failures |
Akifumi Wachi
Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan Abstract | Paper |
| 11:00 – 11:20 | 2017-s-06-d An Analytical Solution for Multi-revolution Transfer Trajectory with Periodic Thrust and Non-Singular Elements |
Yusuke Ozawa
Department of Advanced Energy, The University of Tokyo, Kashiwa, Japan Abstract | Paper |
| 11:20 – 11:40 | 2017-s-07-d Attitude and Orbit Control of a Spinning Solar Sail by the Vibrational Input on the Sail Membrane |
Yuki Takao
Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan Abstract | Paper |
| 11:40 – 12:00 | 2017-s-08-d Estimation Algorithm of Relative Position and Attitude during Proximity Rendezvous and Docking Using Multiple Ultra-Wide-Band Devices |
Mikihiro Ikura
Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo, Japan Abstract | Paper |