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First Author Name
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Country
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Title
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Mon, Feb. 08 - Constellations 1 (Jean-Pierre Carrou)
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R. Bertrand
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France
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Constellation Design Optimization with a DOP based Criterion
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P. Rozanès
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France
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Definition of a Reference Orbit for the Constellation Skybridge
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Theresa W. Beech
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Spain
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A Study of Three Satellite Constellation Design Algorithms
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Christine Fernandez
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France
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First Acquisition Analysis for the Skybridge Constellation Satellites
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Mon, Feb. 08 - Orbit Control 1 (Rolf Münch)
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Christophe Koppel
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France
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Advantages of a Continuous Thrust Str. From a Geosynchronous Transfer Orbit, Using High Specific Impulse Thrusters
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Valcir Orlando
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Brazil
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Analysis of an Autonomous Orbit Control Concept Using GPS
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R. Bertrand
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France
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Use of Some Volumic Methods in Resolution of Two Point Boundary Value Problems
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Mats Rosengren
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ESA
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The Orbit Control of ERS-1 and ERS-2 for a Very Accurate Tandem Configuration
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Isabelle Grousset
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France
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Study of a Splitting Method for Rendezvous Manoeuvres
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Mon, Feb. 08 - Attitude Dynamics & Determination (Valcir Orlando)
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Roberto V. F. Lopes
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Brazil
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Attitude Determination from GPS Interferometry Applied to Spin Stabilized Satellites at an Arbitrary Spin Rate
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Michiaki Horii
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Japan
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Efficient Iterative Algorithms for Minimizing Attitude Functions and Their Application to Three-Axis Attitude Determination
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Ruth Azor
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Israel/USA
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Angular-Rate Estimation Using Quaternion Measurements
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M. Challa
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USA
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Recent Developments in Earth Oblateness Modeling forAttitude Determination
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Tatsuaki Hashimoto
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Japan
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Magnetic Unloading Scheme for Improving Pointing Performance of Astronomy Mission Satellites
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Ijar M. Fonseca
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Brazil
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After-Separation Attitude Dynamics of the Brazilian Scientific Satellite SACI-2
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Tue, Feb. 09 - Orbit Dynamics (Siegmar Pallaschke)
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Ana Paula Marins Chiaradia
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Brazil
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Investigation of Simplified Dynamical Force Models for Orbit Determination Using Single Frequency GPS Measurements
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Mina Ogawa
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Japan
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Real-time Estimation of COMETS trajectory
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Kyle T. Alfriend
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USA
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Characterizing Orbit Uncertainty Due to Atmospheric Drag Uncertainty
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M.Maruya
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Japan
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Estimation of Motion and Shape of Asteroid Based on Image Sequences
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Antonio Elipe
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Spain
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Periodic Orbits Around Natural Elongated Bodies
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Tue, Feb. 09 - Autonomous Navigation (Oliver Montenbruck)
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Thierry Tournier
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France
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Orbit and Time on-Board Computation: from the Current SPOT4 Solution To GNSS2
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Son H. Truong
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USA
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A Self-tuning Kalman Filter for Autonomous Spacecraft Navigation
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Toshihiko Misu
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Japan
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Autonomy in Guidance Using Image-Based Terrain Recognition and Optical Navigation
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Tue, Feb. 09 - Mission Design & Analysis (Jerome Teles)
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B.P. Robertson
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USA
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On-Orbit Performance Of The TRMM Mission Mode
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M. Mayrhofer
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Germany
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Optimal Mission Aborts of a Winged Orbital Stage
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D. F. Zimbelman
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USA
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The Attitude and Orbit Control System Design for the TRIANA Mission
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Tue, Feb. 09 - Interplanetary Flight (Kuninori Uesugi)
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Hiroshi Yamakawa
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Japan
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ISAS Mercury Orbiter Mission Trajectory Design Strategy
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F. Weischede
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Germany
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Lunar Prospector Orbit Determination and Gravity Field Modeling based on Weilheim 3-Way Doppler Measurements
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Jun ichiro Kawaguchi
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Japan
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On the Lunar and Heliocentric Gravity Assist Experienced in Planet-B( NOZOMI )
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J. Bernard
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France
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Mission Analysis For Rosetta: Descending Phase
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Mina Ogawa
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Japan
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Selene Translunar Trajectory And Lunar Orbit Injection
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A. A. Sukhanov
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Russia
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Trajectory Design for Experimental Mission to Sun-Earth L1, and L2 Points Using SEP
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Wed, Feb. 10 - Systems Analysis & Operations (L. C. Gadelha de Souza)
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Rolf E. Münch
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ESA
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A different Year 2000 Challenge: ESOC s Peak Load in Development and Operations
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Marcelo L. O. Souza
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Brazil
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Study of Tridimensional Impulsive Maneuvers with Thrust Errors
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Siegmar Pallaschke
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ESA
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High-Precision Tracking Calibration with the ESA Tenerife Telescope
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Hélio Koiti Kuga
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Brazil
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Flight Dynamics Operations During LEOP for the INPE s Second Environmental Data Collecting Satellite SCD2
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Wed, Feb. 10 - Orbit Determination (Efraim L. Akim)
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Roberto V. F. Lopes
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Brazil
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Coarse Orbit Determination as a Dividend from Attitude Sensors for Spin-Stabilized Satellites
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Maki Maeda
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Japan
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NASDA's Precise Orbit Determination System
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B. Christophe
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France
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Multi-model filtering for orbit determination during manoeuvre
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Thu, Feb. 11 - Systems & Operations (Edward Christensen)
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Kazuaki Nonaka
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Japan
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Orbital operation of Communications and Broadcasting Engineering Test Satellite (COMETS)
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James R. O'Donnell, Jr.
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USA
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Development and Testing of Automatically-Generated ACS Flight Software for the MAP Spacecraft
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E.L. Akim
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Russia
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Tracking of the launch-vehicle during the insertion to earth orbit
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M.R.A.C. Tredinnick
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Brazil
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Digital Control of a Satellite with Flexible Appendages
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Thu, Feb. 11 - Poster Session
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Regina Kuranaga dos Santos
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Brazil
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A Linear Solution For The Artificial Satellite's Attitude Optimal Control
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Uwe Feucht
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Germany
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Simulation Based Concept for Low Cost Attitude Operations of Equator-S
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M.Parisse
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Italy
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Momentum Bias Systems with Flexible Appendages Stability Considerations
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P. Di Stasio
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Italy
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An Optimal Search Algorithm for Satellite Acquisition
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Felipe E. de la Rosa Bocanegra
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Japan
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Optimal Motion and Position Control of Nonholonomic Flexible Arm
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Cláudio Correa
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Brazil
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The Use of Genetic Algorithms on a Fuzzy Controller for a Satellite During the Pointing Phase
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M. C. Ricci
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Brazil
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Towards a Bapta Mechanism for Small Satellites
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Alan Batten
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UK
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Star Catalog Facility for Spacecraft Mission Support
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Thu, Feb. 11 - Attitude Control (James R. O'Donnell, Jr)
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Karlheinz Spindler
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Germany
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A Simple Attitude Control Law Satisfying Slew-Rate and Torque Constraints
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Fabio Curti
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Italy
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Study on Active Magnetic Attitude Control for the Italian Spacecraft Bus MITA
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Valdemir Carrara
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Brazil
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A Neural Network Satellite Attitude Controller with Error Based Reference Trajectory
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Thu, Feb. 11 - Constellation 2 (Jean-Pierre Carrou)
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B. Raffier
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France
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A Multimedia Constellation Design Method
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Eberhard Gill
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Germany
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Precise GNSS-2 Satellite Orbit Determination
Based on Inter-Satellite-Links
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S. Geffroy
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France
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Optimal use of Electric Propulsion for Future Leo Constellations Positioning
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S. Tebbani
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France
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Station Acquisition of a Homogeneous Constellation by linear and nonlinear optimization
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Andreï Baranov
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Russia
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Optimal Maneuvers for Station Keeping for a Given Configuration of the Satellite Constellation
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Fri, Feb. 12 - Orbit Control 2 (Rolf Münch)
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Hélio Koiti Kuga
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Brazil
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Orbit maintenance and control of CBERS
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Huang Fuming
|
China
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Orbit Maneuvers of Satellites in Near-Earth Quasi-Circular
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Walkíria Schulz
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Brazil
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Optimal Space Maneuvers in a Keplerian Force Field in Three Dimensions
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Valdemir Carrara
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Brazil
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Flight Dynamics Analysis and operational support for CBERS
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Fri, Feb. 12 - Orbit Dynamics / Reentry (Hélio K. Kuga)
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Ulisses T. V. Guedes
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Brazil
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A Study About Dynamic Re-Entry into Earth Atmosphere Avoiding Lateral Maneuvers
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Yu. G. Sikharulidze
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Russia / Brazil
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Analysis of accuracy at ballistic re-entry in the Earth disturbed atmosphere
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Rolan I.Kiladze
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Georgia / Russia
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On New Investigations Of Geostationary Satellite Motion
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Luiz C. Gadelha de Souza
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Brazil
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Large Space Structure Vibration Control During Attitude Manouvre
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Sergey M.Kudryavtsev
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Russia
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Accurate and Quick Account of the Tidal Effects on a Satellite's Motion by the New Analytical Method
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Grigory Zaslavskiy
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Russia
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Effective algorithm for calculating probability of satisfaction of restrictions on spacecraft movement parameters
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