ESA GNC Conference Papers Repository
60 search results:
PRACTICAL ANALYTIC SOLUTION OF RELATIVE MOTION BETWEEN FORMATION FLYING SATELLITES WITH DIFFERENT BALLISTIC COEFFICIENTS IN THE NEAR-CIRCULAR REFERENCE ORBIT
T. Yamamoto
MICROCOPE: MYRIADE AOCS ADAPTATION FOR A DRAG-FREE MISSION
Ch. Pittet, P. Prieur, A. Torres, A. Peus & C. Fallet
GNC DESIGN FOR THE DARWIN SPACEBORNE INTERFEROMETER
C. Beugnon, E. Buvat, M. Kersten & S. Boulade
RENDEZVOUS AND FORMATION FLYING EXPERIMENTS WITHIN THE PRISMA IN-ORBIT TESTBED
S. Berge, B. Jakobsson, P. Bodin, A. Edfors & S. Persson
AOCS DESIGN FOR A 160-M, 450-KG SOLAR SAIL SPACECRAFT OF THE SOLAR POLAR IMAGER MISSION
B. Wie & D. Murphy
A SCALABLE SYSTEM FOR FORMATION FLYING GUIDANCE AND CONTROL
J.B. Mueller & S.J. Thomas
CONTROL TASKS AND FUNCTIONAL ARCHITECTURE OF THE LISA PATHFINDER DRAG-FREE SYSTEM
W. Fichter, A. Schleicher, N. Brandt, S. Vitale & D. Bortoluzzi
MARS EXPRESS AND ROSETTA AUTONOMOUS STR: IN FLIGHT EXPERIENCE
A. Landi, F. Boldrini & D. Procopio
MARS EXPRESS AOCS IN-FLIGHT BEHAVIOUR
O. Bonnamy, C. Bonneau, E. Ecale & M. Denis
MICRO CMGS FOR AGILE SMALL SATELLITES: DESIGN AND IN-ORBIT TESTS
V. Lappas, P. Oosthuizen, P. Madle, L. Cowie, G. Yuksel & D. Fertin
ENVISAT ATTITUDE AND ORBIT CONTROL IN-ORBIT PERFORMANCE: AN OPERATIONAL VIEW
P.Bargellini, M.A. Garcia Matatoros, L.Ventimiglia, & D.Suen
IN-FLIGHT GEOSTATIONNARY AOCS BASED ON STAR TRACKER
L. Gaudic, E. Brouillard, J.M. Pasquet & H. Renault
SMART-1 LUNAR MISSION: OPERATIONAL EXPERIENCE WITH ITS AUTOMATIC ATTITUDE AND ORBIT CONTROL SUBSYSTEM AND ITS RELATION WITH ELECTRIC PROPULSION SYSTEM
M. Alonso, J. De Bruin, D. Milligan, D. Gestal, O. Camino, L. Stagnaro & P. Bodin
MARS ENTRY AND AEROCAPTURE ROBUST CONTROL USING STATIC OUTPUT FEEDBACK AND LPV TECHNIQUES
A. Kron, J. de Lafontaine & C. LePeuvédic
SIX-DOF FORMATION FLYING MODELING AND CONTROL WITH AN APPLICATION TO SPACE INTERFEROMETRY
S. Gaulocher, C. Pittet & J.-P. Chrétien
OPTIMAL DISCRETE-TIME DESIGN OF MAGNETIC ATTITUDE CONTROL LAWS
T. Pulecchi, M. Lovera & A. Varga
ROBUST CONTROL OF UNCERTAIN FLEXIBLE SPACECRAFT USING DISTURBANCE OBSERVER BASED CONTROL STRATEGIES
W.-H. Chen
CLOSED LOOP RELATIVE MOTION CONTROL FOR A SEGMENTED ALONG-TRACK RADAR ANTENNA IN LOW EARTH ORBIT
J.-P. Chrétien
(?-MU)-ITERATION TECHNIQUE APPLIED TO THE CONTROL OF SATELLITES WITH LARGE FLEXIBLE APPENDAGES
G. Bodineau, C. Beugnon, S. Boulade & C. Bérard-Chiappa
ROBUSTNESS ANALYSIS OF A NONLINEAR DYNAMIC INVERSION CONTROLLER FOR AN AEROSERVOELASTIC FLIGHT VEHICLE
C. Papageorgiou
GSTB-V2/A NORMAL MODE AOCS DESIGN
D.G. Dungate, M.C. Pigg, D. Gittins, S. Hardacre, D. Liddle & X. Lefort
MEDIUM TO LOW CLASS GYROS FOR SPACEBUS 4000 APPLICATION
N. Perriault, B. Célérier & S. Dussy
PLANCK ACMS: AUTONOMOUS AND PRECISE CONTROL FOR SLOWLY SPINNING SATELLITE
J.S. Llorente-Martínez, D. Zorita, A. Agenjo, C. Cazorla, A. O´Dwyer, J.M. Del Cura, M. Oort, J. Peters, A. Bachetta, G. Chlewicki, D.Guichon & I. Rasmussen
ATV GNC SYNTHESIS: OVERALL DESIGN, OPERATIONS AND MAIN PERFORMANCES
G. Personne, A. Lopez-y-diaz & P. Delpy
COROT: AN AOCS POWERED BY MISSION TELESCOPE
D. Brethé, N. Canellada, O. Rigaud & M. Tello
MAGNETIC ATTITUDE CONTROL OF THE GOCE SATELLITE
G. Sechi, G. André, D. Andreis & M. Saponara
ACMS FDIR SYSTEM FOR THE HERSCHEL / PLANCK SATELLITES
J.F.T. Bos, D. Zorita, A. Bacchetta, G. Chlewicki, D. Guichon & I. Rasmussen
DESIGN OF THE INTEGRATED CONTROL SYSTEM (ICS), A RE-CONFIGURABLE MULTI-MISSION AOC & DATA HANDLING SUBSYSTEM
G. Campolo, F. Cesaro, A. Intelisano & M. Pantaleoni
POINTING BUDGET ASSESSMENT FOR SPIN-STABILISED SATELLITES
D.G. Dungate, R.C. Theobald, M. Oort, A. Agenjo & I. Rasmussen
ECSS-E60 CONTROL ENGINEERING STANDARDISATION
J. Flemmig, A. Benoit, J. Mignot & P. Laurens
REAL-TIME TEST BENCH WITH CONTROL MOMENT GYRO IN THE LOOP
E. Montfort, M. Kessab, M. Rennie, D.P. McGuinness, P. Palomo, T. Zwartbol & B.A. Oving
AUTOMATED TRANSFER VEHICLE (ATV) NOMINAL SOFTWARE GNC NUMERICAL VALIDATION OVERVIEW
D. Berthelier, M. Chaize, P. Delpy & S. Strandmoe
IMPLEMENTING A GNSS EMULATOR FOR NAVIGATION SYSTEMS
E. Günayd?n, P. Oguz & T. Sönmez
GNCDE: AN INTEGRATED GNC DEVELOPMENT ENVIRONMENT
P. Colmenarejo, F. Gandía, A. García Casas, A. Tomassini & F. Ankersen
AUTOMATED TRANSFER VEHICLE THRUSTERS SELECTION AND MANAGEMENT FUNCTION
N. Silva, F. Martel & P. Delpy
AUTONOMOUS LOW-THRUST GUIDANCE SCHEME FOR INTERPLANETARY TRAJECTORIES: APPLICATION TO SMART-1
J. Gil-Fernández, E. Milic, M. Graziano, B. Polle, S. Mancuso & J. Fertig
DYNAMIC ARTIFICIAL POTENTIAL FUNCTION GUIDANCE FOR AUTONOMOUS ON-ORBIT SERVICING
A. Tatsch & N. Fitz-Coy
NAVIGATION SYSTEMS USING MONTE CARLO METHOD
M. Soták, M. Sopata & F. Kmec
AN EXACT STEERING LAW FOR TWIN CONTROL MOMENT GYRO SYSTEMS
S. Asghar, P.L. Palmer & M. Roberts
VALIDATION OF INNOVATIVE STATE ESTIMATION AND CONTROL TECHNIQUES ON PROBA-2
J. de Lafontaine, J. Côté, A. Kron, P. Vuilleumier, S. Santandrea & P. Van den Braembussche
GYRO STELLAR ATTITUDE DETERMINATION
M. Ghezal, B. Polle, C. Rabejac & J. Montel
H infinity ANALYSIS AND SYNTHESIS BY GENETIC ALGORITHMS OF THE ATTITUDE CONTROL SYSTEM OF THE BRAZILIAN SATELLITE LAUNCHER
W.C. Leite Filho, P.C. Pellanda & F.E.L. Medeiros
APPROACH COMPARISON FOR CONTROLLER DESIGN OF A LAUNCHER
A.G. Brito, W.C. Leite Filho & F.O. Ramos
USE OF GNSS FOR NEXT EUROPEAN LAUNCHER GENERATION
Narmada, S. Reynaud, P. Delaux & A. Biard
USEFULNESS OF A FORCE FEEDBACK ON ELECTROMECHANICAL ACTUATOR
C. Renault
REACTION WHEEL ACTUATOR WITH TWO NEWTON-METER TORQUE CAPABILITY FOR INCREASED SPACECRAFT AGILITY
B. Bialke & E. Stromswold
AFFORDABLE DUAL-FREQUENCY GPS IN SPACE
M. Garcia-Fernandez, O. Montenbruck, M. Markgraf & J. Leyssens
A COMPACT CAMERA FOR SPACE NAVIGATION
S. Gigli
HRG TECHNOLOGY: A PROMISING GYROMETER SPACE EQUIPMENT
O. Girard, J.M. Caron & P. Berthier
NEXT GENERATION CMOS ACTIVE PIXEL SENSORS FOR ATTITUDE AND ORBIT CONTROL SYSTEMS
J. Bogaerts, W. Ogiers, T. Cools & W. Diels
DEVELOPMENT OF A MEMS RATE SENSOR
D. Durrant, T. Moy, P. Hutton & S. Dussy
NEW SODERNS APS BASED AUTONOMOUS MULTIPLE HEADS STAR SENSOR (HYDRA): THREE HEADS ARE BETTER THAN ONE
L. Blarre, N. Perrimon, A. Lacroix, L. Majewski & E. Anciant
MICRO DIGITAL SUN SENSOR: "A MATCHBOX MIRACLE"
C.W. de Boom, J.A.P. Leijtens & N. van der Heiden
GIMBALLING MAGNETIC BEARING REACTION WHEEL WITH DIGITAL CONTROLLER
B. Gerlach, M. Ehinger, H. Knut Raue & R. Seiler
ADVANCED STAR SENSORS BASED ON ACTIVE PIXEL SENSOR TECHNOLOGY
U. Schmidt, Ch. Kühl & K. Michel
VISION NAVIGATION FOR EUROPEAN LANDERS AND THE NPAL PROJECT
B.Frapard & S. Mancuso
AUTONOMOUS ATTITUDE DETERMINATION AND CONTROL FOR LOW-COST DEEP SPACE PROBES
V. Lappas, G. Prassinos, J. van der Ha & B. Wie
GNC DESIGN FOR A MARS ASCENT VEHICLE
E. Ferreira, P. Augros & G. Ortega
AUTONOMOUS NAVIGATION FOR INTERPLANETARY MISSIONS PERFORMANCE ACHIEVEMENTS BASED ON REAL AND FLIGHT IMAGES
B. Polle, B. Frapard, J. Gil-Fernández, E. Milic, M. Graziano, J. Rebordão & P. Motrena
AUTONOMOUS PLANETARY LANDING USING A LIDAR SENSOR: THE CLOSED-LOOP SYSTEM
J. de Lafontaine, D. Neveu & K. Lebel