nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
Adaptive Control of Flexible Space Structures
|
Govin, B. |
|
1983 |
16 |
11 |
p. 361-371 11 p. |
artikel |
2 |
A Delayed Pulse Roll/Yaw Controller for a Momentum Biased Spacecraft
|
Goel, P.S. |
|
1983 |
16 |
11 |
p. 243-248 6 p. |
artikel |
3 |
A Ground Loop Attitude Control System for ANIK B
|
Kowalik, H. |
|
1983 |
16 |
11 |
p. 509-518 10 p. |
artikel |
4 |
A High Accuracy Sun Sensor
|
Bokhove, H. |
|
1983 |
16 |
11 |
p. 265-272 8 p. |
artikel |
5 |
A Microprocessor-Based Position Control System for a Telescope Secondary Mirror
|
Lorell, K.R. |
|
1983 |
16 |
11 |
p. 1-13 13 p. |
artikel |
6 |
An Adaptive Attitude Control System for Large-Angle Slew Manoeuvres
|
van den Bosch, P.P.J. |
|
1983 |
16 |
11 |
p. 165-172 8 p. |
artikel |
7 |
An Advanced Star Tracker Design using the Charge Injection Device
|
Kollodge, J.C. |
|
1983 |
16 |
11 |
p. 297-309 13 p. |
artikel |
8 |
A New Method of Satellite Attitude Control using a Bias-Momentum
|
Chen, Zu-Gui |
|
1983 |
16 |
11 |
p. 237-242 6 p. |
artikel |
9 |
Apple Attitude Acquisition with One Solar Panel Undeployed
|
Goel, P.S. |
|
1983 |
16 |
11 |
p. 541-547 7 p. |
artikel |
10 |
Application of Model Following Control and Estimation Techniques to Attitude Control of Manoeuvring Spacecraft
|
Zwartbol, T. |
|
1983 |
16 |
11 |
p. 173-184 12 p. |
artikel |
11 |
Attitude Control System with Quantization Elements
|
Yeh, Ching-Ming |
|
1983 |
16 |
11 |
p. 227-235 9 p. |
artikel |
12 |
Attitude Determination, Control and Navigation of a Spinning Satellite
|
Rodden, J.J. |
|
1983 |
16 |
11 |
p. 133-138 6 p. |
artikel |
13 |
Attitude Measurement and Estimation of Solar Observation Satellites
|
Yu, S.H. |
|
1983 |
16 |
11 |
p. 185-189 5 p. |
artikel |
14 |
Author Index
|
|
|
1983 |
16 |
11 |
p. 591-592 2 p. |
artikel |
15 |
Automatic Controls on Board Planetary Probes
|
Beretta, A. |
|
1983 |
16 |
11 |
p. 583-589 7 p. |
artikel |
16 |
Combined Orbit and Attitude Control of Geostationary Satellites using Electric Propulsion
|
Krulle, G. |
|
1983 |
16 |
11 |
p. 469-475 7 p. |
artikel |
17 |
Coordinate-Parametric Control System for Spacecraft: Functioning Algorithms
|
Rutkovsky, V.Yu. |
|
1983 |
16 |
11 |
p. 103-109 7 p. |
artikel |
18 |
Damping-Augmentation Mechanism for Flexible Spacecraft
|
Inoue, M. |
|
1983 |
16 |
11 |
p. 347-352 6 p. |
artikel |
19 |
Design of Reaction Jet Attitude Control Systems for Flexible Spacecraft
|
Bittner, H. |
|
1983 |
16 |
11 |
p. 372-373 2 p. |
artikel |
20 |
Digital Control Loops for Telecom 1 AOCS
|
Peyrot, P. |
|
1983 |
16 |
11 |
p. 75-82 8 p. |
artikel |
21 |
Dynamics of Space Cable Systems
|
Beletskii, V.V. |
|
1983 |
16 |
11 |
p. 409-416 8 p. |
artikel |
22 |
Failure Detection and Correction in Low Orbit Satellite Attitude Control System
|
Marie, J.L. |
|
1983 |
16 |
11 |
p. 575-582 8 p. |
artikel |
23 |
Ground Support Software for the EXOSAT Onboard Computer
|
Bares, P. |
|
1983 |
16 |
11 |
p. 557-561 5 p. |
artikel |
24 |
Guidance and Control at the Near-Planet LEG of the “VENERA” Mission
|
Demiokhin, A.S. |
|
1983 |
16 |
11 |
p. 533-540 8 p. |
artikel |
25 |
Impact of Spacecraft Design on Remote Control of Satellite operations
|
Barrett, M. |
|
1983 |
16 |
11 |
p. 563-567 5 p. |
artikel |
26 |
In-Space Assembly and Maintenance of Unmanned Spacecraft
|
Lacombe, J.L. |
|
1983 |
16 |
11 |
p. 477-488 12 p. |
artikel |
27 |
Investigation of the Stability of Satellite Large Angle Attitude Manoeuvres using Nonlinear Optimization Methods
|
Dempster, M.A.H. |
|
1983 |
16 |
11 |
p. 111-124 14 p. |
artikel |
28 |
ION Attitude Control Circuit Operational Experience
|
Legostayev, V.P. |
|
1983 |
16 |
11 |
p. 311-325 15 p. |
artikel |
29 |
ION Sensor Signal Fluctuations During Spacecraft Jet Engine Operation
|
Legostayev, V.P. |
|
1983 |
16 |
11 |
p. 327-340 14 p. |
artikel |
30 |
Lumped Parameter Dynamic Models for Large Space Structures with Flexible and Rigid Parts
|
Bertoni, G. |
|
1983 |
16 |
11 |
p. 125-131 7 p. |
artikel |
31 |
Magnetic Roll/Yaw Attitude Control of a Momentum Biased Near Polar Orbit Satellite
|
Brüderle, E. |
|
1983 |
16 |
11 |
p. 249-256 8 p. |
artikel |
32 |
Modular Design and Dynamic Tests on Active Bearing Momentum Wheels
|
Knorrchen, H. |
|
1983 |
16 |
11 |
p. 459-468 10 p. |
artikel |
33 |
Multipurpose Sun Sensor using CCD Detector
|
Flamenbaum, S. |
|
1983 |
16 |
11 |
p. 273-281 9 p. |
artikel |
34 |
New Control Schemes for a Magnetic Attitude Control System
|
Tsuchiya, K. |
|
1983 |
16 |
11 |
p. 221-225 5 p. |
artikel |
35 |
New Developments in Infra-Red Sensors for Three-Axis Stabilized Satellites
|
Hébert, M. |
|
1983 |
16 |
11 |
p. 283-288 6 p. |
artikel |
36 |
Noise Characterization and Minimization of a Precision Gyroscopic Rate Sensor
|
Dougherty, H. |
|
1983 |
16 |
11 |
p. 443-448 6 p. |
artikel |
37 |
Observable Degree and Accuracy of Various Attitude Determination for Spinning Satellite
|
Xing, Guangqian |
|
1983 |
16 |
11 |
p. 205-213 9 p. |
artikel |
38 |
One New Method of Dynamic Flight Control
|
Vukobratović, M.K. |
|
1983 |
16 |
11 |
p. 149-155 7 p. |
artikel |
39 |
On the Attitude Estimation of Earth Observation Satellites
|
Yu, S.H. |
|
1983 |
16 |
11 |
p. 215-220 6 p. |
artikel |
40 |
On the Shape and Orientation Control of Orbiting Shallow Spherical Shell Structure
|
Bainum, P.M. |
|
1983 |
16 |
11 |
p. 399-408 10 p. |
artikel |
41 |
Performance Characterization of the Dry Tuned-Gimbal Gyro for Application to Precision Spacecraft Attitude Reference Systems
|
Donoghue, P.J. |
|
1983 |
16 |
11 |
p. 433-442 10 p. |
artikel |
42 |
Preface
|
van Woerkom, P.Th.L.M. |
|
1983 |
16 |
11 |
p. vi- 1 p. |
artikel |
43 |
Recent Advances in the Control of Large Flexible Spacecraft
|
Lyons, M.G. |
|
1983 |
16 |
11 |
p. 341-346 6 p. |
artikel |
44 |
Reconfiguration of On-Board Control Algorithms
|
Ivanov, V.P. |
|
1983 |
16 |
11 |
p. 569-573 5 p. |
artikel |
45 |
Sampled Control Stability of the ESA Instrument Pointing System
|
Thieme, G. |
|
1983 |
16 |
11 |
p. 57-65 9 p. |
artikel |
46 |
Software for the Closed Loop Control of Experiments on the GEOS Spacecraft
|
Johnson, A.S. |
|
1983 |
16 |
11 |
p. 503-507 5 p. |
artikel |
47 |
Space Borne Attitude Measurement Units
|
Amieux, J.C. |
|
1983 |
16 |
11 |
p. 417-421 5 p. |
artikel |
48 |
Space Platform Attitude Control System
|
Levinthal, J. |
|
1983 |
16 |
11 |
p. 39-45 7 p. |
artikel |
49 |
Space Telescope Pointing Control
|
Dougherty, H. |
|
1983 |
16 |
11 |
p. 15-24 10 p. |
artikel |
50 |
Spin Free Analytic Platform Type Guidance and Control System
|
Higashiguchi, M. |
|
1983 |
16 |
11 |
p. 549-556 8 p. |
artikel |
51 |
Star Detection and Tracking using CCDs
|
Borghi, G. |
|
1983 |
16 |
11 |
p. 289-295 7 p. |
artikel |
52 |
State Synthesiser; A Digital Observer for Spacecraft Attitude Control Systems
|
Dodds, S.J. |
|
1983 |
16 |
11 |
p. 191-203 13 p. |
artikel |
53 |
Synopsis of Optical Attitude Sensors Developed by ESA
|
Connolly, A. |
|
1983 |
16 |
11 |
p. 257-264 8 p. |
artikel |
54 |
Synthesis of Terminal Control Sequence Algorithms with the Use of Moving-Point Guidance
|
Mitroshin, E.I. |
|
1983 |
16 |
11 |
p. 139-148 10 p. |
artikel |
55 |
Testing and Investigations of Reaction Wheels
|
Bosgra, J.A. |
|
1983 |
16 |
11 |
p. 449-458 10 p. |
artikel |
56 |
The Attitude and Orbit Control Subsystem of the TV-SAT/TDF1 Spacecraft
|
Bittner, H. |
|
1983 |
16 |
11 |
p. 83-102 20 p. |
artikel |
57 |
The Attitude and Orbit Control System for GIOTTO, ESA's Halley Encounter Mission
|
Coupé, G.M. |
|
1983 |
16 |
11 |
p. 25-37 13 p. |
artikel |
58 |
The Effect of Flexible Satellite Elasticity on Orientation Accuracy
|
Rutkovsky, V.Yu |
|
1983 |
16 |
11 |
p. 353-360 8 p. |
artikel |
59 |
The HEAO Experience – Design Through operations
|
Hoffman, D.P. |
|
1983 |
16 |
11 |
p. 489-501 13 p. |
artikel |
60 |
The L-SAT Attitude and Orbit Control Subsystem
|
Pengelly, J.W. |
|
1983 |
16 |
11 |
p. 47-56 10 p. |
artikel |
61 |
Trajectory Corrections for Flight to Short-Period Comets in the Solar System in 1981-1991
|
Platonov, A.K. |
|
1983 |
16 |
11 |
p. 157-164 8 p. |
artikel |
62 |
Validation of the In-Orbit Checkout of the IRAS Gyroscopes using Computer Simulations
|
van Casteren, J.F.M. |
|
1983 |
16 |
11 |
p. 423-432 10 p. |
artikel |
63 |
Validation Techniques for Spot Attitude Control System Development
|
Bourg, P.E. |
|
1983 |
16 |
11 |
p. 67-73 7 p. |
artikel |
64 |
VENERA 13, 14 Unmanned Interplanetary Spacecraft Attitude Control Subsystem
|
Demiokhin, A.S. |
|
1983 |
16 |
11 |
p. 519-531 13 p. |
artikel |