ESA GNC Conference Papers Repository

ASTRO-SPAS AMCS Design and Flight Experience

Brüderle, E.; Boinghoff, A; Gradmann, N.; Kaffer, L.; Wullstein, P.

In-Flight Experimentation for the SPOT-1 Safe Mode

Lebreton, D. ; Benoit, A ; Horblin, M. ; Aubel, E.

Gyroless Attitude Estimation for Hipparcos

Val Serra, S. ; Carron, C. ; Heger, D. '; McDonald, A.

In-Flight Experience with the Eureca Attitude Measurement Assembly

Martinet, Y.; Pinaud, J.M.; Szczepaniak, R.; Duhamel, T.

In-Flight Performance and Lessons Learned for the Eurostar AOCS

Auxepaules, S.; Dekneudt, J.; Gaullier, F.; Cheoux-Damas, P.; Duhamel, T.

Attitude Determination and Control System Operation of Intelsat 701 Spacecraft

Raman, K. V. ; Chang, C. ; Hsing, J. ; Anderson, J. ; Tilley, S. ; Kazimi, F. ; Adsit, R.

Intelsat VI(F-3) Reboost Mission Rendezvous Planning and Implementation

Virdee, L. ; Davis, S. ; Meyer, C.

Consider-Filter Revisited for Recursive Attitude Determination

Bar-Itzhack, I.; Nathan, J.

In-flight Performance of the Attitude Measurement and Control of the TSS-1 Satellite

Musetti, B.; Cibrario, B.

The Analysis of Spacecraft Pointing Errors-An Updated ESA Error Handbook

Dungate, D.

Attitude Determination of Spacecraft Ulysses with Precision Doppler Tracking

less, L.; Arduini, C. (University of Rome La Sapienza, ITALY)

"3-Slits" Star Mapper Data Processing for the Determination of Spin Axis Misalignment Determination

Mortari, D.; Arduini, C.

Attitude Determination and Control for Spacecraft Using Differential GPS

Glenn Lightsey, E.; Cohen, C.; Parkinson, B.

An Experiment of Wide-Band Pointing Control of a Flexible Structure Using Non-colocated Actuators and Sensors

Preumont, A; Loix, N.

Microdynamics Tests at Matra Marconi Space

Laurens, Ph.; Guillaud, V.

Design and Utilization of INTELSAT Attitude Determination and Control System Simulators

Anderson, J.; Main, E.

SAX AOCS Subsystem Simulation and Tests. Results Evaluation and Plan for Future Developments

Battistoni, G.; Cassi, C.; Ravazzotti, M.

An Experimental Framework for Attitude Control

Pignatelli, A; Monaco, S.

A New Generation Test and Verification Equipment for Attitude and Control Systems

Sonnenschein, F. ; Nicolai, R. ; Versteeg, M. ; Beerthuizen, P. ; Kollen, J. ; Van Rossem, P. ; Storni, B.

Pointing and Tracking Space Mechanism for Laser Communication

Bruneau, B.; De Boisanger, M.; Doittau, P. O.

Mastering Microvibrations for High Pointing Accuracy Systems

Guillaud, V.; Champetier, C.; Capitaine, A; Jourdon, N.; Lefevre, Y-M.

The Design and Verification of the Pointing Acquisition and Tracking System SILEX

Benoit, A; Griseri, G.

A Star Sensor Based AOCS for ENVISAT

Riant, P.; Val Serra, S.; Fragnol, D.; Desire, P.

Advanced AOCS Concepts for Drag-Free Applications

Vaillon, L.; Duhamel, T.; Champetier, C.

The Impedance Approach to the Control of Flexible Bodies

Cope, P.

Pointing Algorithm: A Strategy for Orbit Injection with Uncontrolled Last Stage

De Castro Leite Filho, W.

Explicit Guidance Law: a Unique Algorithm for Multiple Types of Missions

Demessant-Garnero, A

Mathematical Modelling and Test of the Gimbal Control Loop of an Upper State Engine

Klotz, H.; De Rose, F.; Weber, V.

Inertial Guidance System for H-II Launch Vehicle

Kobayashi, W.; Suzuki, Y; Nakamura, T.; Kawamura, Y.

Design of an Attitude Control System for Fine Pointing of an Axisymmetric Spinning Reentry Vehicle

Landiech, Ph.

An Optimal Control Strategy for the Italian Unmanned Re-entry Capsule (Carina)

Martella, P.; Musetti, B.

Adaptive Guidance Law for a Re-Entry Vehicle

Caillaud, J.; Meloux, E.

Integrated Simulation of Spinning Satellite Dynamics and Nutation Damping Electronics using PSpice

Sund, A

Fault Tolerance Techniques Applied in ISO-AOCS

Beerthuizen, P.; Oort, M.

TOSCA: Tool for the Designing of Simulation and Control of Spacecraft Attitude

Imbert, N. ; Charmeau, M-C ; Truchi, C.

Model Reduction Methods for the Analysis of Control-Structure Interaction in Flexible Space Structures

Spanjaard, J. ; Cowling, D.A.

Sloshing Modellization by Neural Networks

Strauch, H.

Wide-Angle Automonous Star Sensor for Satellite Use

Cope, P. ; Priestley, M.

Design Aspects of a New Multimission Coarse Star Sensor SED 15

Vilaire, D. ; Krebs, J. ; Sebbag, I ; Navoni, R.

High Accuracy Algorithm for Mosaic Earth Sensor

Brunel, O. ; Colmon, A. ; Pezant, C ; Tissot, M. ; Navoni, R. ; Florent, R.

Development and Pre-Qualification of a Medium Accuracy, Wide Field Pattern Recognition Star Sensor

Verhoeff, P ; De Boom, C ; Meier, H. ; Andre, G.

The Mosaic Earth Sensor: A Novel Sensor Development for Geostationary Spacecraft

Beard, C.; Hayhurst, G

Replanning of Guidance Strategies and GNC Modes in the ARC Demonstration Mission

Cosmen, J. ; Alvarez, L. ; Fehse, W. ; Tobfas, A.

Differential and Relative Navigation Results with a GPS Receiver for Space Applications

Legido, J. ; Lucas, R.; Martinez, M

DGPS Navigation Experiment for HOPE Autolanding

Matsumoto, S ; Suzuki, H.; Mineno, H. ; Tomita, H. ; Sagisaka, M. ; Harigae, M. ; Ishikawa, K. ; Maeda, H. ; Itsukaichi, A

LANDSAT-5 and TOPEX/POSEIDON Orbit Determination from GPS Observations

Hesper, E.; Ambrosius, B.; Wakker,. K.

MOMSNAV: Location of the Russian Space Station MlR with Differential GPS

Fockersperger, S.; Jansche, A.; Lemke, N.; Fraile-Ordonez, J.M.

On a New Class of Tools for Computer Aided Control System Specification and Design

Kienitz, K.

An Analysis of the Thermoelastic Nutational Instability of Spinning Spacecraft

Arduini, C. ; Gay, N.; Parisse, M.

Optimal Internally Induced Rest-to-Rest Reorientation of Planar Multibody Systems

Hussain, N.; Kane, T

Tuning Analytical Synthesis Techniques via Multi-Objective Optimization for a Two-Feedback-Loop Control of Flexible Space Structures

Bals, J ; Goh, C-H. ; Grübel, G.

Spacecraft Navigation and Control According to Probabilistic Criteria

Malyshev, V. V.; Karp, K.; Krasilshikov, M.N.

Nonlinear Adaptive Filtering with Application to Space Plane Flight Path Reconstruction

Chu, Q.; Mulder, J.; Van Den Broek, P.; Verbaas, A.

H Sigma: Design for Satellite Attitude Control

Frapard, B ; Van Troostenberghe, P.

Analysis of an Integrated INS/GPS Navigation System for Re-Entry Vehicles

Lohnert, E. ; Wagner, O.; Eissfeller, B. ; Krischke, M.

Inertial Reference Unit Design for Small Spacecraft

Swanson, C.O.; Barton, E.

REGYS 3 S Low Cost Inertial Measurement Unit for Attitude Control of Satellites

Meresse, J.M.; Combelles, B.; Guay, P.

Spain's Minisat Attitude Determination and Control System (ADCS)

Prieto Llanos, T.; Fernandez De La Mora Varela, G.

Gravity Gradient and Magnetorquing Attitude Control for Low Earth Orbit Satellites

Hodgart, M.S.; Ong, W. T.

The Attitude and Orbit Control and Management Subsystem (AOCMS) for the Cluster Spacecraft.

Jackson, P.J.; Pope, J.

Fault Tolerant Feature of Lunar-A Attitude and Orbit Control System

Hashimoto, T. ; Ninomiya, K. ; Uo, M. ; Terada, H. ; Ogasawara, M. ; Shirakawa, K.

ROSETTA Spacecraft and Surface Probe GNC Systems Design & Architecture

Regnier, P.; Champetier, C. ; De Lafontaine, J.';

Spacecraft Attitude Control Software Development Using Automatic Code Generation Technologies

McEwen, R.; Tubb, F.

Guidance & Control of Meteosat, Second Generation

Cope, P.