| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Accelerated Gradient Projection Technique with Application to Rocket Trajectory Optimization
|
Speyer, J.L.
|
|
1970
|
3 |
1 |
p. 458-464
7 p.
|
artikel
|
| 2 |
Adaptive Variable-Parameter Control of Vehicles
|
Petrov, B.N.
|
|
1970
|
3 |
1 |
p. 452-457
6 p.
|
artikel
|
| 3 |
A Guidance System for the Ascent of a Martian Probe
|
Heffron Jr., W. Gordon
|
|
1970
|
3 |
1 |
p. 154-162
9 p.
|
artikel
|
| 4 |
A Gyroless Control System for Sub-Arc Second Solar Pointing of a Sounding Rocket Payload
|
Hansen, Q.M.
|
|
1970
|
3 |
1 |
p. 313-325
13 p.
|
artikel
|
| 5 |
A Multipurpose Global Satellite Navigation System
|
Puri, N.N.
|
|
1970
|
3 |
1 |
p. 769-778
10 p.
|
artikel
|
| 6 |
An Active Magnetic Attitude Control System for a Spinning Sun Oriented Satellite
|
Birkhold, E.
|
|
1970
|
3 |
1 |
p. 326-338
13 p.
|
artikel
|
| 7 |
An Application of Kalman-Bucy Theory for a Gyro-Stabilized Platform
|
Bertoni, Gianni
|
|
1970
|
3 |
1 |
p. 599-605
7 p.
|
artikel
|
| 8 |
A New Standard for Information Processing Systems for Manned Space Flight
|
Hopkins Jr., Albert L.
|
|
1970
|
3 |
1 |
p. 223-229
7 p.
|
artikel
|
| 9 |
AOOSY Automatic Orbital Operations System for Satellites and Space Probes
|
Wagner, Wolf-Udo
|
|
1970
|
3 |
1 |
p. 260-264
5 p.
|
artikel
|
| 10 |
Application of the Theory of Optimal Control of Stochastic Processes to the Attitude Control of a Launcher
|
Cornu, J.P.
|
|
1970
|
3 |
1 |
p. 438-451
14 p.
|
artikel
|
| 11 |
Applications of the Gauss-Newton Algorithm to Optimization and Identification
|
Boudarel, R.
|
|
1970
|
3 |
1 |
p. 664-673
10 p.
|
artikel
|
| 12 |
A Spin and Attitude Control System for the ISIS-I and ISIS-B Satellites
|
Kowalik, H.
|
|
1970
|
3 |
1 |
p. 629-638
10 p.
|
artikel
|
| 13 |
Attitude Acquisition and Station Keeping of a Synchronous Satellite
|
Leorat, F.
|
|
1970
|
3 |
1 |
p. 550-571
22 p.
|
artikel
|
| 14 |
Attitude Control System of Molniya I Communication Satellite
|
Raushenbakh, B.V.
|
|
1970
|
3 |
1 |
p. 611-620
10 p.
|
artikel
|
| 15 |
Attitude-Translation Coupling in Drag-Free Satellites
|
Fleming, Alan W.
|
|
1970
|
3 |
1 |
p. 411-418
8 p.
|
artikel
|
| 16 |
Author Index
|
|
|
1970
|
3 |
1 |
p. 808-
1 p.
|
artikel
|
| 17 |
Calculation of Aerodynamic Force and Moment Coefficients for Satellites
|
Lunderstädt, R.
|
|
1970
|
3 |
1 |
p. 206-222
17 p.
|
artikel
|
| 18 |
Computational Method of Crosstalk Effects in Multichannel Systems for Aerospace Communications
|
Puigjaner, Luis C.
|
|
1970
|
3 |
1 |
p. 797-807
11 p.
|
artikel
|
| 19 |
Control of the Optical Surface of a Thin Deformable Primary Mirror with Application to an Orbiting Astronomical Observatory
|
Creedon, Jeremiah F.
|
|
1970
|
3 |
1 |
p. 339-358
20 p.
|
artikel
|
| 20 |
Controls for the Stabilization of a Satellite by Means of Magnetic Torquers
|
Liegeois, A.
|
|
1970
|
3 |
1 |
p. 515-523
9 p.
|
artikel
|
| 21 |
Description and Performance of the Saturn Launch Vehicle's Navigation, Guidance, and Control System
|
Haeussermann, Walter
|
|
1970
|
3 |
1 |
p. 275-312
38 p.
|
artikel
|
| 22 |
Dynamics Control for Operational Spacecraft
|
Lindorfer, W.
|
|
1970
|
3 |
1 |
p. 245-259
15 p.
|
artikel
|
| 23 |
Effectiveness of Different Optimum Filtering Techniques for the Particular Example of Radio Guidance of the Third Stage of Europa 1 Carrier Vehicle
|
Bittner, Helmut
|
|
1970
|
3 |
1 |
p. 674-694
21 p.
|
artikel
|
| 24 |
Effectiveness of Space Information Systems Evaluation Problems
|
Matveevsky, S.F.
|
|
1970
|
3 |
1 |
p. 265-274
10 p.
|
artikel
|
| 25 |
Entry Trajectory Reconstruction Using Flight Data
|
Morth, Raymond
|
|
1970
|
3 |
1 |
p. 712-718
7 p.
|
artikel
|
| 26 |
Error Analysis of Navigation Satellite Systems
|
Conrad, D.A.
|
|
1970
|
3 |
1 |
p. 779-796
18 p.
|
artikel
|
| 27 |
Estimation of the Local Attitude of Orbiting -Spacecraft
|
Bryson Jr., A.E.
|
|
1970
|
3 |
1 |
p. 481-507
27 p.
|
artikel
|
| 28 |
Filtering and its Applications
|
Bucy, R.S.
|
|
1970
|
3 |
1 |
p. 606-610
5 p.
|
artikel
|
| 29 |
Flight Testing of a Highly Sensitive Accelerometer (Operation Athalie)
|
Bouttes, Jacques
|
|
1970
|
3 |
1 |
p. 375-381
7 p.
|
artikel
|
| 30 |
Gravity-Gradient Stabilization Studies with the Dodge Satellite
|
Fischell, R.E.
|
|
1970
|
3 |
1 |
p. 639-654
16 p.
|
artikel
|
| 31 |
High Accuracy Attitude Control for Pointing to the Sun
|
Honda, Tsunenori
|
|
1970
|
3 |
1 |
p. 532-537
6 p.
|
artikel
|
| 32 |
High Precision Attitude Determination by Sensing the Earth and Lunar Horizon in the Infrared
|
Astheimer, Robert W.
|
|
1970
|
3 |
1 |
p. 359-366
8 p.
|
artikel
|
| 33 |
Man-Machine Design for the Apollo Navigation, Guidance, and Control System -- Revisited
|
Nevins, J.L.
|
|
1970
|
3 |
1 |
p. 1-27
27 p.
|
artikel
|
| 34 |
Mariner Mars 1969 Navigation, Guidance, and Control
|
Scull, John R.
|
|
1970
|
3 |
1 |
p. 163-174
12 p.
|
artikel
|
| 35 |
Method of Modulating Functions in Re-Entry Control Problem
|
Okhotaimski, D.E.
|
|
1970
|
3 |
1 |
p. 750-768
19 p.
|
artikel
|
| 36 |
On Distribution of Functions Among Man-Operator and Elements of Automatics in Closed Control Systems
|
Pavlov, V.
|
|
1970
|
3 |
1 |
p. 65-71
7 p.
|
artikel
|
| 37 |
On Man-Machine Coupling Concerning the Control of a Machine Whose Dynamics Do Not Present Damping Factors
|
Raoult, Monsieur
|
|
1970
|
3 |
1 |
p. 35-41
7 p.
|
artikel
|
| 38 |
On the Optimal Putting of an Artificial Earth Satellite in the Gravity-Stable Position
|
Beletskii, V.V.
|
|
1970
|
3 |
1 |
p. 419-432
14 p.
|
artikel
|
| 39 |
On the Stability and Stabilization of Stationary Motions of Satellites
|
Rumjanchev, V.V.
|
|
1970
|
3 |
1 |
p. 591-598
8 p.
|
artikel
|
| 40 |
Operations and Functions of the Apollo Guidance Computer During Rendezvous
|
Saponaro, Joseph A.
|
|
1970
|
3 |
1 |
p. 116-135
20 p.
|
artikel
|
| 41 |
Optimal Control at Entering the Atmosphere
|
Lebedev, A.A.
|
|
1970
|
3 |
1 |
p. 741-749
9 p.
|
artikel
|
| 42 |
Optimization Technique for Launching a Spacecraft
|
De Montcheuil, J. Moreau
|
|
1970
|
3 |
1 |
p. 433-437
5 p.
|
artikel
|
| 43 |
Optimum Properties of a Single-Parameter Orbital Correction of a Spacecraft
|
Platonov, A.K.
|
|
1970
|
3 |
1 |
p. 465-480
16 p.
|
artikel
|
| 44 |
Orbital Parameter Estimation Using Manual Space Navigation Sensors and Computer
|
Levine, Stephen A.
|
|
1970
|
3 |
1 |
p. 695-705
11 p.
|
artikel
|
| 45 |
Orbital Stations and Studies of the Earth from Space
|
Petrov, B.N.
|
|
1970
|
3 |
1 |
p. 183-205
23 p.
|
artikel
|
| 46 |
Orbit and Attitude Control Systems for Synchronous Satellites
|
Pujes, J.-P.
|
|
1970
|
3 |
1 |
p. 508-514
7 p.
|
artikel
|
| 47 |
Orbit and Attitude Stabilization System for “Symphonie” Communications Satellite
|
Brauch, Armin
|
|
1970
|
3 |
1 |
p. 621-628
8 p.
|
artikel
|
| 48 |
Predictive Entry Guidance for an Apollo-Type Vehicle
|
Stiles, J.A.
|
|
1970
|
3 |
1 |
p. 732-740
9 p.
|
artikel
|
| 49 |
Preface
|
Aseltine, John A.
|
|
1970
|
3 |
1 |
p. v-
1 p.
|
artikel
|
| 50 |
Problems Relative to the Automatic Rendez-Vous of Spin-Stabilized Satellites
|
Vohan, Paul
|
|
1970
|
3 |
1 |
p. 86-95
10 p.
|
artikel
|
| 51 |
Reconstitution of the Attitude of a Probe-Rocket Head Destined to Analyse the Infrared Horizon
|
Lemaitre, Marie-Paule
|
|
1970
|
3 |
1 |
p. 367-374
8 p.
|
artikel
|
| 52 |
Rendevous Control at Minimal Propellant Consumption
|
Marin, O.M.
|
|
1970
|
3 |
1 |
p. 96-100
5 p.
|
artikel
|
| 53 |
Satellite Gravitational Stabilization System with Maximum Damping Rate
|
Sarychev, V.A.
|
|
1970
|
3 |
1 |
p. 655-663
9 p.
|
artikel
|
| 54 |
Simulation and Error Analysis of a Manual Rendezvous System
|
Schneider, Alan M.
|
|
1970
|
3 |
1 |
p. 42-64
23 p.
|
artikel
|
| 55 |
Some On-Board Information Processing Systems for Bandwidth Compression and Error Correcting Coding
|
Cappellini, Vito
|
|
1970
|
3 |
1 |
p. 230-238
9 p.
|
artikel
|
| 56 |
Space and Spacecraft Environment
|
Bourrieau, J.
|
|
1970
|
3 |
1 |
p. 239-244
6 p.
|
artikel
|
| 57 |
Space Rendez-vous Terminal Phase Control
|
Legostaev, V.P.
|
|
1970
|
3 |
1 |
p. 72-85
14 p.
|
artikel
|
| 58 |
Space Vehicle Trajectory Control for Entry into the Atmosphere at Hypersolic Speed
|
Klimin, A.V.
|
|
1970
|
3 |
1 |
p. 719-731
13 p.
|
artikel
|
| 59 |
Stochastic Optimal Control System of Re-Entry at Supercircular Velocity
|
Petrov, B.N.
|
|
1970
|
3 |
1 |
p. 401-410
10 p.
|
artikel
|
| 60 |
Sub-Optimal Satellite Attitude Control Using Ionic Propulsion
|
Durante, C.
|
|
1970
|
3 |
1 |
p. 538-549
12 p.
|
artikel
|
| 61 |
Survey of Lunar Surface Mobility Systems
|
Kaplan, Marshall H.
|
|
1970
|
3 |
1 |
p. 175-182
8 p.
|
artikel
|
| 62 |
Synthesis of a Set of Admissible Controls Provides Asymptotic Stability for a Man-Made Satellite
|
Letov, A.M.
|
|
1970
|
3 |
1 |
p. 524-531
8 p.
|
artikel
|
| 63 |
The Damping of Satellite Oscillations by Changing the Mass Distribution
|
Hiller, Manfred H.
|
|
1970
|
3 |
1 |
p. 572-580
9 p.
|
artikel
|
| 64 |
The Design of the Control System Spacecraft Stabilization with Human Operator
|
Solodovnikov, V.V.
|
|
1970
|
3 |
1 |
p. 28-34
7 p.
|
artikel
|
| 65 |
The Dynamics of a Non Rigid Spinning Satellite Containing Oscillating Liquids
|
Michelini, R.C.
|
|
1970
|
3 |
1 |
p. 581-590
10 p.
|
artikel
|
| 66 |
The Minimum-Time Thrust-Vector Control Law in the Apollo Lunar-Module Autopilot
|
Widnall, William S.
|
|
1970
|
3 |
1 |
p. 136-153
18 p.
|
artikel
|
| 67 |
The Use of Electric Microthrusters for Orbit Correction of Geostationary Satellites
|
Luquet, P.
|
|
1970
|
3 |
1 |
p. 382-400
19 p.
|
artikel
|
| 68 |
Trajectory Control in Rendezvous Problems Using the Regularization Techniques
|
Nour Eldin, H.A.
|
|
1970
|
3 |
1 |
p. 101-115
15 p.
|
artikel
|
| 69 |
Verification of Space Navigation Procedures
|
Knoedler, James L.
|
|
1970
|
3 |
1 |
p. 706-711
6 p.
|
artikel
|
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