Automatic control in space 1982 : proceedings of the ninth IFAC/ESA symposium, Noordwijkerhout, the Netherlands, 5-9 July 1982

Content: 
Other Titles in the IFAC Proceedings Series, Page ii
Front Matter, Page iii
Copyright, Page iv
IFAC SYMPOSIUM ON AUTOMATIC CONTROL IN SPACE, Page v
PREFACE, Page vi, P Th L M van Woerkom
A MICROPROCESSOR-BASED POSITION CONTROL SYSTEM FOR A TELESCOPE SECONDARY MIRROR, Pages 1-13, K.R. Lorell, R.R. Clappier, W.F. Barrows, G.K. Lee
SPACE TELESCOPE POINTING CONTROL, Pages 15-24, H. Dougherty, C. Rodoni, K. Tompetrini, A. Nakashima
THE ATTITUDE AND ORBIT CONTROL SYSTEM FOR GIOTTO, ESA'S HALLEY ENCOUNTER MISSION, Pages 25-37, G.M. Coupé, P.J. Witteveen
SPACE PLATFORM ATTITUDE CONTROL SYSTEM, Pages 39-45, J. Levinthal, L. Morata, L. Powell
THE L-SAT ATTITUDE AND ORBIT CONTROL SUBSYSTEM, Pages 47-56, J.W. Pengelly, E. Fyfe, A.J. Rogers
SAMPLED CONTROL STABILITY OF THE ESA INSTRUMENT POINTING SYSTEM, Pages 57-65, G. Thieme, P. Rogers, D. Sciacovelli
VALIDATION TECHNIQUES FOR SPOT ATTITUDE CONTROL SYSTEM DEVELOPMENT, Pages 67-73, P.E. Bourg
DIGITAL CONTROL LOOPS FOR TELECOM 1 AOCS, Pages 75-82, P. Peyrot, R. Havas
THE ATTITUDE AND ORBIT CONTROL SUBSYSTEM OF THE TV-SAT/TDF1 SPACECRAFT, Pages 83-102, H. Bittner, A. Brauch, E. Brüderle, Ch. Roche, A. Scheit, J. Starke, M. Surauer
COORDINATE-PARAMETRIC CONTROL SYSTEM FOR SPACECRAFT: FUNCTIONING ALGORITHMS, Pages 103-109, V.Yu. Rutkovsky, S.D. Zemlyakov
INVESTIGATION OF THE STABILITY OF SATELLITE LARGE ANGLE ATTITUDE MANOEUVRES USING NONLINEAR OPTIMIZATION METHODS, Pages 111-124, M.A.H. Dempster, G.M. Coupé
LUMPED PARAMETER DYNAMIC MODELS FOR LARGE SPACE STRUCTURES WITH FLEXIBLE AND RIGID PARTS, Pages 125-131, G. Bertoni, M.E. Penati
ATTITUDE DETERMINATION, CONTROL AND NAVIGATION OF A SPINNING SATELLITE, Pages 133-138, J.J. Rodden
SYNTHESIS OF TERMINAL CONTROL SEQUENCE ALGORITHMS WITH THE USE OF MOVING-POINT GUIDANCE, Pages 139-148, E.I. Mitroshin, V.A. Glinsky, E.V. Khrunov
ONE NEW METHOD OF DYNAMIC FLIGHT CONTROL, Pages 149-155, M.K. Vukobratović, D.M. Stokić, R.D. Stojić
TRAJECTORY CORRECTIONS FOR FLIGHT TO SHORT-PERIOD COMETS IN THE SOLAR SYSTEM IN 1981–1991, Pages 157-164, A.K. Platonov, R.K. Kazakova
AN ADAPTIVE ATTITUDE CONTROL SYSTEM FOR LARGE-ANGLE SLEW MANOEUVRES, Pages 165-172, P.P.J. van den Bosch, W. Jongkind, A.C.W. van Swieten
APPLICATION OF MODEL FOLLOWING CONTROL AND ESTIMATION TECHNIQUES TO ATTITUDE CONTROL OF MANOEUVRING SPACECRAFT, Pages 173-184, T. Zwartbol, R.F. van den Dam, A.P. Terpstra, P.Th.L.M. van Woerkom
ATTITUDE MEASUREMENT AND ESTIMATION OF SOLAR OBSERVATION SATELLITES, Pages 185-189, S.H. Yu
STATE SYNTHESISER; A DIGITAL OBSERVER FOR SPACECRAFT ATTITUDE CONTROL SYSTEMS, Pages 191-203, S.J. Dodds
OBSERVABLE DEGREE AND ACCURACY OF VARIOUS ATTITUDE DETERMINATION FOR SPINNING SATELLITE, Pages 205-213, Xing Guangqian
ON THE ATTITUDE ESTIMATION OF EARTH OBSERVATION SATELLITES, Pages 215-220, S.H. Yu, Q.P. Chu
NEW CONTROL SCHEMES FOR A MAGNETIC ATTITUDE CONTROL SYSTEM, Pages 221-225, K. Tsuchiya, M. Inoue
ATTITUDE CONTROL SYSTEM WITH QUANTIZATION ELEMENTS, Pages 227-235, Yeh Ching-Ming, Qiu Yu-Huang
A NEW METHOD OF SATELLITE ATTITUDE CONTROL USING A BIAS-MOMENTUM, Pages 237-242, Chen Zu-gui
A DELAYED PULSE ROLL/YAW CONTROLLER FOR A MOMENTUM BIASED SPACECRAFT, Pages 243-248, P.S. Goel, P. Kudva
MAGNETIC ROLL/YAW ATTITUDE CONTROL OF A MOMENTUM BIASED NEAR POLAR ORBIT SATELLITE, Pages 249-256, E. Brüderle, A. Reindler
SYNOPSIS OF OPTICAL ATTITUDE SENSORS DEVELOPED BY ESA, Pages 257-264, A. Connolly, M. Fabbricotti, P.N. Kruythoff, A.S. Menardi, P. Underwood
A HIGH ACCURACY SUN SENSOR, Pages 265-272, H. Bokhove
MULTIPURPOSE SUN SENSOR USING CCD DETECTOR, Pages 273-281, S. Flamenbaum, P. Anstett
NEW DEVELOPMENTS IN INFRA-RED SENSORS FOR THREE-AXIS STABILIZED SATELLITES, Pages 283-288, M. Hebert, J. Malot, M. Tissot, J.P. Krebs
STAR DETECTION AND TRACKING USING CCDs, Pages 289-295, G. Borghi, A. Buccheri, D. Cumeni
AN ADVANCED STAR TRACKER DESIGN USING THE CHARGE INJECTION DEVICE, Pages 297-309, J.C. Kollodge, J.A. Sand
ION ATTITUDE CONTROL CIRCUIT OPERATIONAL EXPERIENCE, Pages 311-325, V.P. Legostayev, V.D. Nikolayev
ION SENSOR SIGNAL FLUCTUATIONS DURING SPACECRAFT JET ENGINE OPERATION, Pages 327-340, V.P. Legostayev, V.D. Nikolayev
RECENT ADVANCES IN THE CONTROL OF LARGE FLEXIBLE SPACECRAFT, Pages 341-346, M.G. Lyons
DAMPING-AUGMENTATION MECHANISM FOR FLEXIBLE SPACECRAFT, Pages 347-352, M. Inoue, K. Tsuchiya
THE EFFECT OF FLEXIBLE SATELLITE ELASTICITY ON ORIENTATION ACCURACY, Pages 353-360, V.Yu. Rutkovsky, V.M. Sukhanov
ADAPTIVE CONTROL OF FLEXIBLE SPACE STRUCTURES, Pages 361-371, B. Govin, B. Claudinon
DESIGN OF REACTION JET ATTITUDE CONTROL SYSTEMS FOR FLEXIBLE SPACECRAFT, Pages 373-398, H. Bittner, H.D. Fischer, M. Surauer
ON THE SHAPE AND ORIENTATION CONTROL OF ORBITING SHALLOW SPHERICAL SHELL STRUCTURE, Pages 399-408, P.M. Bainum, A.S.S.R. Reddy
DYNAMICS OF SPACE CABLE SYSTEMS, Pages 409-416, V.V. Beletskii, E.M. Levin
SPACE BORNE ATTITUDE MEASUREMENT UNITS, Pages 417-421, J.C. Amieux, G. Muller
VALIDATION OF THE IN-ORBIT CHECKOUT OF THE IRAS GYROSCOPES USING COMPUTER SIMULATIONS, Pages 423-432, J.F.M. van Casteren, R.M. van Doom
PERFORMANCE CHARACTERIZATION OF THE DRY TUNED-GIMBAL GYRO FOR APPLICATION TO PRECISION SPACECRAFT ATTITUDE REFERENCE SYSTEMS, Pages 433-442, P.J. Donoghue
NOISE CHARACTERIZATION AND MINIMIZATION OF A PRECISION GYROSCOPIC RATE SENSOR, Pages 443-448, H. Dougherty, A.M. Brady, L.F. Reschke, K. Tompetrini, S.P. Weinstein, J. Blondin, H. Kleine, J. Rosenberg
TESTING AND INVESTIGATIONS OF REACTION WHEELS, Pages 449-458, J.A. Bosgra, J.J.M. Prins
MODULAR DESIGN AND DYNAMIC TESTS ON ACTIVE BEARING MOMENTUM WHEELS, Pages 459-468, H. Knörrchen, Th. Lange
COMBINED ORBIT AND ATTITUDE CONTROL OF GEOSTATIONARY SATELLITES USING ELECTRIC PROPULSION, Pages 469-475, G. Krülle, E. Zeyfang
IN-SPACE ASSEMBLY AND MAINTENANCE OF UNMANNED SPACECRAFT (), Pages 477-488, J.L. Lacombe, G. Berger
THE HEAO EXPERIENCE — DESIGN THROUGH OPERATIONS, Pages 489-501, D.P. Hoffman
SOFTWARE FOR THE CLOSED LOOP CONTROL OF EXPERIMENTS ON THE GEOS SPACECRAFT, Pages 503-507, A.S. Johnson
A GROUND LOOP ATTITUDE CONTROL SYSTEM FOR ANIK B, Pages 509-518, H. Kowalik, B.V. Burlton, R.A. Costanzo, F.C. Kes, S.B. Turner
VENERA 13, 14 UNMANNED INTERPLANETARY SPACECRAFT ATTITUDE CONTROL SUBSYSTEM, Pages 519-531, A.S. Demiokhin, V.N. Kheifetz, K.G. Sukhanov, S.M. Voinakov
GUIDANCE AND CONTROL AT THE NEAR-PLANET LEG OF THE “VENERA” MISSION, Pages 533-540, A.S. Demiokhin, V.N. Kheifetz, K.G. Sukhanov, S.M. Voinakov
APPLE ATTITUDE ACQUISITION WITH ONE SOLAR PANEL UNDEPLOYED, Pages 541-547, P.S. Goel, P. Kudva
SPIN FREE ANALYTIC PLATFORM TYPE GUIDANCE AND CONTROL SYSTEM, Pages 549-556, M. Higashiguchi, H. Ishitani
GROUND SUPPORT SOFTWARE FOR THE EXOSAT ONBOARD COMPUTER, Pages 557-561, P. Bares
IMPACT OF SPACECRAFT DESIGN ON REMOTE CONTROL OF SATELLITE OPERATIONS, Pages 563-567, M. Barrett
RECONFIGURATION OF ON-BOARD CONTROL ALGORITHMS, Pages 569-573, V.P. Ivanov, Yu.P. Portnov-Sokolov
FAILURE DETECTION AND CORRECTION IN LOW ORBIT SATELLITE ATTITUDE CONTROL SYSTEM, Pages 575-582, J.L. Marie
AUTOMATIC CONTROLS ON BOARD PLANETARY PROBES, Pages 583-589, A. Beretta, F. Longoni
AUTHOR INDEX, Pages 591-592