26th International Symposium on Space Flight Dynamics ISSFD  June 3-9, 2017, Matsuyama, Japan

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)
16:00 – 16:20

ISTS-2017-d-035/ISSFD-2017-035

Pierluigi Righetti (EUMETSAT, Germany)

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

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