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