| Spacecraft Attitude and Orbit Control System Development Trends in Korea | p. 1 |
| Technical Challenges of Spacecraft Control Technologies in Japan - Development of Recent Engineering Test Satellites and a Future Scope | p. 9 |
| Orbit and Attitude Control Systems of Russian Communication, Geodetic and Navigation Spacecraft | p. 15 |
| Precision Control Systems of Motion on Russian Spacecraft for Ecological Remote Sensing | p. 27 |
| Ultra-Precision Attitude Control of the Low-Orbital Remote Sensing Spacecraft | p. 39 |
| Spacecraft Attitude Maneuver Planning for the Mission Support | p. 45 |
| A Robust Adaptive Nonlinear Control Approach to Missile Autopilot Design | p. 49 |
| Some Control Strategies of High Angle of Attack Missile Autopilot | p. 53 |
| The Application of Gain-Scheduling H[subscript [Infinity]] Controllers for a Missile Autopilot | p. 59 |
| Modified Receding Horizon Guidance Law | p. 65 |
| Reference Management for Control Systems Under Constraints | p. 71 |
| Motion Estimation and Capturing of Tumbling Object in Non-Gravitational Field | p. 77 |
| Autonomous Navigation of Rovers for Planetary Exploration | p. 83 |
| Dynamic Manipulation Characteristics of Robot Arms Mounted on a Flexible Space Structure | p. 89 |
| Control of Flexible Arm Robot Using Genetic Algorithm | p. 95 |
| Control of Dynamic Systems in Spatial Networks: Applications, Results, and Challenges | p. 101 |
| Real-Time Midcourse Guidance Robust to Missile Launch Conditions | p. 111 |
| Trajectory Control of a Non-Linear Homing Missile | p. 117 |
| Fault-Tolerant Attitude Control Systems of the Communication and Navigation Spacecraft | p. 123 |
| Fault Diagnosis of Space Vehicle Guidance and Control Systems Using Analytical Redundancy | p. 129 |
| Failure Accommodation for Large Transport Aircraft Using Thrust and Stabilizers | p. 135 |
| Challenges in Control and Autonomy of Communications Satellites | p. 141 |
| On-Orbit Dynamics and Control of Large Scaled Membrane with Satellites at Its Corners | p. 161 |
| On the Attitude Control of Flight Vehicle System Using Self-Tuning Method Based on D-L Networks | p. 167 |
| Control Design for the Rosetta Comet Lander | p. 173 |
| Sliding Mode Attitude Control for Magnetic Actuated Satellite | p. 179 |
| Study of Relative Position and Attitude Estimation and Control Scheme for the Final Phase of an Autonomous Docking Mission | p. 185 |
| Study of Capture and Berthing Experiment of ETS-VII | p. 195 |
| Adaptive Attitude Control System for Data Relay Test Satellite | p. 203 |
| Coefficient Diagram Method | p. 211 |
| [mu]-Analysis and Synthesis with Rational Multipliers | p. 223 |
| Dynamic Recurrent Neural Networks for Stable Adaptive Control of Wing Rock Motion | p. 231 |
| Automatic Tuning for Model Based Predictive Control During Reconfiguration | p. 237 |
| Fuzzy ARTMAP Neural Network and Its Application to Fault Diagnosis of Integrated Navigation Systems | p. 243 |
| A Constrained Kohonen Network and Its Application to Sensor Fault Detection | p. 249 |
| Active Control Technology and Restructurable Flight Controller Design | p. 255 |
| H[subscript [Infinity]] control of a Flying Vehicle in Ground Effect | p. 257 |
| Robust Flight Control Law Design for Automatic Landing Flight Experiment | p. 265 |
| Multi-Disciplinary Optimisation of Distributed Aero-Engine Control System Architectures | p. 271 |
| High Alpha Application of Nonlinear Adaptive Control | p. 277 |
| Flight Control Technology: An Overview | p. 283 |
| Attitude Control Operations on Koreasat Satellites | p. 289 |
| Analysis of a Station-Keeping Maneuver Strategy for Three Geostationary Satellites Collocation | p. 295 |
| Spacecraft Attitude Controller Design for Large Angle Maneuver Using Quaternion and Dual Mode Control | p. 301 |
| Real-Time Orbit Determination Onboard SFU (Space Flyer Unit) Using GPS Data | p. 307 |
| Performance Analysis of Wide Area Differential GPS (WADGPS) in East-Asia | p. 311 |
| The GPS Integrity Problem | p. 317 |
| Control of Launch Vehicles as Flexible Bodies | p. 323 |
| Nonexciting Control by Orientation of Flexible Space Vehicles | p. 335 |
| Modeling and Control of a Flexible Spacecraft for Large-Angle Rapid Maneuvers | p. 341 |
| Static Output Feedback Design to Achieve Phase Stabilization of Bending Mode | p. 347 |
| Design of Realtime Onboard GNC Systems Using Integrated Design Tools | p. 353 |
| A Visible Range Earth Sensor: The Algorithm of Determination of the Earth Image Edge Accessible Accuracy Estimation | p. 361 |
| The Evolution of Microelectronics and Its Impact on Avionics | p. 367 |
| Near-Minimum Fuel Guidance Law of a Lunar Landing Module | p. 373 |
| Control Aspects of Aerospace Plane Docking with Ekranoplane for Water Landing | p. 379 |
| A Federated Kalman Filter Design Using a Gain Fusion Algorithm | p. 385 |
| A Method of Automatic Air-Combat Simulation and Assessment | p. 393 |
| The Pre-Requisite for Success: Verification and Validation of the ENVISAT Spacecraft Flight Operations Control Centre | p. 399 |
| Correction of Spacecraft Autonomous Navigation System Using Terrain Image Processing and Analysis | p. 407 |
| RGPS - Based Automatic Landing System for Light and Commuter Aircraft | p. 413 |
| Hybrid Simulation Software Scheme for Validation of a Launcher Control System | p. 419 |
| Optimally Guided and Controlled Launch Vehicle System: Flight Experience of a Polar Mission | p. 425 |
| Non-Stationary H[Infinity] Control Law for Launcher with Bending Modes | p. 433 |
| Spaceplane Trajectory Optimization with Vehicle Size Analysis | p. 439 |
| Space Systems for Research of the Earth - Basis for Monitoring and Management of Scientific and Applied Information Data. Reception and Use of Scientific and Applied Information Data in Automatic Space Complexes and Systems | p. 445 |
| Author Index | p. 455 |
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