14th  International Symposium on Space Flight Dynamics

Foz do Iguaçu, Brazil, 8 - 12 February, 1999

The 14th  ISSFD was organized by INPE (Brazilian Institute for Space Research) under the auspices of AEB (Brazilian Space Agency) and ABCM (Brazilian Society of Mechanical Sciences).

 

Program:

First Author Name

Country

Title

   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

 


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