nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
A Constrained Kohonen Network and Its Application to Sensor Fault Detection
|
Chan, C.W. |
|
1998 |
31 |
21 |
p. 249-254 6 p. |
artikel |
2 |
Active Control Technology and Restructurable Flight Controller Design
|
Kanai, Kimio |
|
1998 |
31 |
21 |
p. 255- 1 p. |
artikel |
3 |
Adaptive Attitude Control System for Data Relay Test Satellite
|
Yamada, Katsuhiko |
|
1998 |
31 |
21 |
p. 203-209 7 p. |
artikel |
4 |
A Federated Kalman Filter Design Using a Gain Fusion Algorithm
|
Kim, Jinwon |
|
1998 |
31 |
21 |
p. 385-391 7 p. |
artikel |
5 |
A Method of Automatic Air-Combat Simulation and Assessment
|
Imado, Fumiaki |
|
1998 |
31 |
21 |
p. 393-398 6 p. |
artikel |
6 |
μ-Analysis and Synthesis with Rational Multipliers
|
Manceaux, Christelle |
|
1998 |
31 |
21 |
p. 223-229 7 p. |
artikel |
7 |
Analysis of a Station-Keeping Maneuver Strategy for Three Geostationary Satellites Collocation
|
Lee, Byoung-Sun |
|
1998 |
31 |
21 |
p. 295-300 6 p. |
artikel |
8 |
A Robust Adaptive Nonlinear Control Approach to Missile Autopilot Design
|
Kim, Seung-Hwan |
|
1998 |
31 |
21 |
p. 49-52 4 p. |
artikel |
9 |
Attitude Control Operations on Koreasat Satellites
|
Hwangbo, Han |
|
1998 |
31 |
21 |
p. 289-293 5 p. |
artikel |
10 |
Author Index
|
|
|
1998 |
31 |
21 |
p. 455-456 2 p. |
artikel |
11 |
Automatic Tuning for Model Based Predictive Control During Reconfiguration
|
Huzmezan, M. |
|
1998 |
31 |
21 |
p. 237-242 6 p. |
artikel |
12 |
Autonomous Navigation of Rovers for Planetary Exploration
|
Schilling, Klaus |
|
1998 |
31 |
21 |
p. 83-87 5 p. |
artikel |
13 |
A Visible Range Earth Sensor: The Algorithm of Determination of the Earth Image Edge Accessible Accuracy Estimation
|
Soloviov, L.V. |
|
1998 |
31 |
21 |
p. 361-366 6 p. |
artikel |
14 |
Challenges in Control and Autonomy of Communications Satellites
|
Gottzein, E. |
|
1998 |
31 |
21 |
p. 141-160 20 p. |
artikel |
15 |
Coefficient Diagram Method
|
Manabe, S. |
|
1998 |
31 |
21 |
p. 211-222 12 p. |
artikel |
16 |
Control Aspects of Aerospace Plane Docking with Ekranoplane for Water Landing
|
Nebylov, A.V. |
|
1998 |
31 |
21 |
p. 379-384 6 p. |
artikel |
17 |
Control Design for the Rosetta Comet Lander
|
Ankersen, Finn |
|
1998 |
31 |
21 |
p. 173-178 6 p. |
artikel |
18 |
Control of Dynamic Systems in Spatial Networks: Applications, Results, and Challenges
|
Speyer, Jason L. |
|
1998 |
31 |
21 |
p. 101-110 10 p. |
artikel |
19 |
Control of Flexible Arm Robot Using Genetic Algorithm
|
Goto, Yasuhiro |
|
1998 |
31 |
21 |
p. 95-99 5 p. |
artikel |
20 |
Control of Launch Vehicles as Flexible Bodies
|
Mori, Hidehiko |
|
1998 |
31 |
21 |
p. 323-334 12 p. |
artikel |
21 |
Correction of Spacecraft Autonomous Navigation System Using Terrain Image Processing and Analysis
|
Krasilshikov, M.N. |
|
1998 |
31 |
21 |
p. 407-411 5 p. |
artikel |
22 |
Design of Realtime Onboard GNC Systems Using Integrated Design Tools
|
Ankersen, Finn |
|
1998 |
31 |
21 |
p. 353-360 8 p. |
artikel |
23 |
Dynamic Manipulation Characteristics of Robot Arms Mounted on a Flexible Space structure
|
Jiang, Zhao Hui |
|
1998 |
31 |
21 |
p. 89-94 6 p. |
artikel |
24 |
Dynamic Recurrent Neural Networks for Stable Adaptive Control of Wing Rock Motion
|
Kooi, Steven B.L. |
|
1998 |
31 |
21 |
p. 231-236 6 p. |
artikel |
25 |
Failure Accommodation for Large Transport Aircraft Using Thrust and Stabilizers
|
Ochi, Y. |
|
1998 |
31 |
21 |
p. 135-140 6 p. |
artikel |
26 |
Fault Diagnosis of Space Vehicle Guidance and Control Systems Using Analytical Redundancy
|
Suzuki, Hideto |
|
1998 |
31 |
21 |
p. 129-134 6 p. |
artikel |
27 |
Fault-Tolerant Attitude Control Systems of the Communication and Navigation Spacecraft
|
Somov, Ye.I. |
|
1998 |
31 |
21 |
p. 123-128 6 p. |
artikel |
28 |
Flight Control Technology: An Overview
|
Siouris, George M. |
|
1998 |
31 |
21 |
p. 283-288 6 p. |
artikel |
29 |
Fuzzy Artmap Neural Network and its Application to Fault Diagnosis of Integrated Navigation Systems
|
Zhang, H.Y. |
|
1998 |
31 |
21 |
p. 243-248 6 p. |
artikel |
30 |
H∞ Control of a Flying Vehicle in Ground Effect
|
Tokutake, Hiroshi |
|
1998 |
31 |
21 |
p. 257-263 7 p. |
artikel |
31 |
High Alpha Application of Nonlinear Adaptive Control
|
Cho, S. |
|
1998 |
31 |
21 |
p. 277-282 6 p. |
artikel |
32 |
Hybrid Simulation Software Scheme for Validation of a Launcher Control System
|
Carrijo, D.S. |
|
1998 |
31 |
21 |
p. 419-424 6 p. |
artikel |
33 |
Modeling and Control of a Flexible Spacecraft for Large-Angle Rapid Maneuvers
|
Li, Yong |
|
1998 |
31 |
21 |
p. 341-346 6 p. |
artikel |
34 |
Modified Receding Horizon Guidance Law
|
Kim, Ki Baek |
|
1998 |
31 |
21 |
p. 65-69 5 p. |
artikel |
35 |
Motion Estimation and Capturing of Tumbling Object in Non-Gravitational Field
|
Fujiwara, Takeshi |
|
1998 |
31 |
21 |
p. 77-82 6 p. |
artikel |
36 |
Multi-Disciplinary Optimisation of Distributed Aero-Engine Control System Architectures
|
Thompson, H.A. |
|
1998 |
31 |
21 |
p. 271-276 6 p. |
artikel |
37 |
Near-Minimum Fuel Guidance Law of a Lunar Landing Module
|
Ueno, Seiya |
|
1998 |
31 |
21 |
p. 373-378 6 p. |
artikel |
38 |
Nonexciting Control by Orientation of Flexible Space Vehicles
|
Rutkovsky, V.Y.U. |
|
1998 |
31 |
21 |
p. 335-340 6 p. |
artikel |
39 |
Non-Stationary H∞ Control Law for Launcher with Bending Modes
|
Mauffrey, S. |
|
1998 |
31 |
21 |
p. 433-438 6 p. |
artikel |
40 |
On-Orbit Dynamics and Control of Large Scaled Membrane with Satellites at its Corners
|
Nakasuka, Shinichi |
|
1998 |
31 |
21 |
p. 161-166 6 p. |
artikel |
41 |
On the Attitude Control of Flight Vehicle System Using Self-Tuning Method Based on D-L Networks
|
Kim, Yoon-Sang |
|
1998 |
31 |
21 |
p. 167-171 5 p. |
artikel |
42 |
Optimally Guided and Controlled Launch Vehicle System: Flight Experience of a Polar Mission
|
Dasgupta Dr., Santanu |
|
1998 |
31 |
21 |
p. 425-432 8 p. |
artikel |
43 |
Orbit and Attitude Control Systems of Russian Communication, Geodetic and Navigation Spacecraft
|
Bartenev, V.A. |
|
1998 |
31 |
21 |
p. 15-26 12 p. |
artikel |
44 |
Performance Analysis of Wide Area Differential GPS (Wadgps) in East-Asia
|
Kee, Changdon |
|
1998 |
31 |
21 |
p. 311-316 6 p. |
artikel |
45 |
Precision Control Systems of Motion on Russian Spacecraft for Ecological Remote Sensing
|
Kozlov, D.I. |
|
1998 |
31 |
21 |
p. 27-38 12 p. |
artikel |
46 |
Preface
|
|
|
1998 |
31 |
21 |
p. v-vi nvt p. |
artikel |
47 |
Real-Time Midcourse Guidance Robust to Missile Launch Conditions
|
Song, Eun-Jung |
|
1998 |
31 |
21 |
p. 111-115 5 p. |
artikel |
48 |
Real-Time Orbit Determination Onboard SFU (Space Flyer Unit) Using GPS Data
|
Ninomiya, K. |
|
1998 |
31 |
21 |
p. 307-310 4 p. |
artikel |
49 |
Reference Management for Control Systems Under Constraints
|
Casavola, Alessandro |
|
1998 |
31 |
21 |
p. 71-76 6 p. |
artikel |
50 |
RGPS - Based Automatic Landing System for Light and Commuter Aircraft
|
Lee, S.J. |
|
1998 |
31 |
21 |
p. 413-418 6 p. |
artikel |
51 |
Robust Flight Control Law Design for Automatic Landing Flight Experiment
|
Ohno, Masahiro |
|
1998 |
31 |
21 |
p. 265-270 6 p. |
artikel |
52 |
Sliding Mode Attitude Control for Magnetic Actuated Satellite
|
Wiśniewski, Rafał |
|
1998 |
31 |
21 |
p. 179-184 6 p. |
artikel |
53 |
Some Control Strategies of High Angle of Attack Missile Autopilot
|
Font, S. |
|
1998 |
31 |
21 |
p. 53-58 6 p. |
artikel |
54 |
Spacecraft Attitude and Orbit Control System Development Trends in Korea
|
Kim, Byung-Kyo |
|
1998 |
31 |
21 |
p. 1-8 8 p. |
artikel |
55 |
Spacecraft Attitude Controller Design for Large Angle Maneuver Using Quatemion and Dual Mode Control
|
Nam, Hun-Sung |
|
1998 |
31 |
21 |
p. 301-305 5 p. |
artikel |
56 |
Spacecraft Attitude Maneuver Planning for the Mission Support
|
Park, Sukjune |
|
1998 |
31 |
21 |
p. 45-48 4 p. |
artikel |
57 |
Spaceplane Trajectory Optimization with Vehicle Size Analysis
|
Tsuchiya, Takeshi |
|
1998 |
31 |
21 |
p. 439-444 6 p. |
artikel |
58 |
Space Systems for Research of the Earth - Basis for Monitoring and Management of Scientific and Applied Information Data
|
Kozlov, D.I. |
|
1998 |
31 |
21 |
p. 445-453 9 p. |
artikel |
59 |
Static Output Feedback Design to Achieve Phase Stabilization of Bending Mode
|
Asthana, C.B. |
|
1998 |
31 |
21 |
p. 347-352 6 p. |
artikel |
60 |
Study of Capture and Berthing Experiment of ETS-VII
|
Miyata, Makoto |
|
1998 |
31 |
21 |
p. 195-202 8 p. |
artikel |
61 |
Study of Relative Position and Attitude Estimation and Control Scheme for the Final Phase of an Autonomous Docking Mission
|
Philip, N.K. |
|
1998 |
31 |
21 |
p. 185-193 9 p. |
artikel |
62 |
Technical Challenges of Spacecraft Control Technologies in Japan - Development of Recent Engineering Test Satellites and a Future Scope
|
Ohkami, Yoshiaki |
|
1998 |
31 |
21 |
p. 9-14 6 p. |
artikel |
63 |
The Application of Gain-Scheduling H∞ Controllers for a Missile Autopilot
|
Hiret, A. |
|
1998 |
31 |
21 |
p. 59-64 6 p. |
artikel |
64 |
The Evolution of Microelectronics and Its Impact on a Vionics
|
Torin, Jan |
|
1998 |
31 |
21 |
p. 367-372 6 p. |
artikel |
65 |
The GPS Integrity Problem
|
Bertoni, Gianni |
|
1998 |
31 |
21 |
p. 317-322 6 p. |
artikel |
66 |
The Pre-Requisite for Success: Verification and Validation of the Envisat Spacecraft Flight Operations Control Centre
|
Rudolph, A. |
|
1998 |
31 |
21 |
p. 399-406 8 p. |
artikel |
67 |
Trajectory Control of a Non-Linear Homing Missile
|
Tsourdos, A. |
|
1998 |
31 |
21 |
p. 117-122 6 p. |
artikel |
68 |
Ultra-Precision Attitude Control of the Low-Orbital Remote Sensing Spacecraft
|
Somov, Ye.I. |
|
1998 |
31 |
21 |
p. 39-44 6 p. |
artikel |