Automatic Control in Aerospace 2004

VOLUME 1<br><br>PLENARY PAPERS<br><br>Russian Space Programs: Achievements and Prospects of Automatic Control Applications<br><br>Control and Navigation Aspects of the New ESA Earth Observation Missions<br> <br>Current Status of Japanese Aerospace Programs - Focusing on the High Speed Flight Demonstration<br><br>National Achievements in Control Theory (The Aerospace Perspective)<br> <br>Model-Based Fault Detection and Diagnosis - Status and Applications<br> <br><br>SPACECRAFT ATTITUDE AND ORBIT CONTROL <br><br>On the Precision Attitude Control Problems<br> <br>Control System of the Microsatellite “Micron”<br><br>Visual Feedback Attitude Control Experiment of a Bias Momentum Micro Satellite<br> <br>Graph Models of Orbital Assembly and Dynamics of a Large Space Structure<br> <br>Position Control Design and Validation Applied to ATV During Docking to ISS<br> <br>On-Orbit Operation and Performance of Micro LabSat Attitude Control Subsystem<br> <br>Nonlinear Dynamics of a Spacecraft Respinup by a Weak Internal Control<br> <br>Systematic Approach to Achieve Fine Pointing Requirement of SOLAR-B<br> <br>Onboard Control Complex for Vehicles Implementation Concept by ISS Example<br> <br>A Novel Architecture for Magnetic Attitude Control of Gravity Gradient Satellites<br> <br>Accurate Modes Design of the Darwin Precursor Formation Flying Demonstration Mission<br> <br>Spacecraft Disposal on a Graveyard Orbit: The In-Flight AOCS Performance for Eurostar 2000 and SPOT 1 during End-of-Life Operations<br> <br>Development of Attitude Control System of Micro LabSat<br> <br>Steering the Control Moment Gyroscope Clusters Onboard High-Agile Spacecraft<br> <br>Microvibration Management and Pointing Stability Analysis of SELENE Satellite<br> <br>Three DOF Optimal Thrusters Selection and Modulation for Space Vehicles<br> <br>Lessons Learned from the Object-Oriented Design of the BIRD Attitude Control System Software<br> <br>A Lyapunov-Typed Nonlinear Attitude Controller for Spacecraft<br> <br>Integrated Power and Attitude Control Using VSCMGs for Small Agile Satellite<br> <br>Advance of Chinese Spacecraft Control Technologies<br><br>An Autonomous Celestial Navigation Method for Geosychronous Satellite<br> <br>Orbit Dynamics and Kinematics with Full Quaternions<br> <br>AUTONOMOUS CONTROL, MISSION CONTROL AND <br>OPERATIONS<br><br>Overview of Recent Control Technology for Japanese Scientific Space Missions<br> <br>Overview of the Attitude and Orbit Control Systems (AOCS) Developed for NASDA/JAXA Engineering Test and Applications Satellites<br> <br>Autonomous Navigation Concepts for Interplanetary Missions<br> <br>Mechanics and Motion Control of a Space Vehicle in the Project of Relict Substance Delivery on Earth (The Project “Phobos_Grunt”)<br> <br>Orbit Acquisition of the Disaster Monitoring Constellation – Preliminary Results<br> <br>On-Orbit Experiment of Motion Estimation and Tracking of Tumbling Object in Space<br> <br>Electric Propulsions as Actuators of the Spacecraft Flight Control Systems<br> <br>Single-Pulse Correction of the Re-Entry Point of a Payload Module<br> <br>End-to-End Modeling for Drag-Free Missions with Application to LISA Pathfinder<br> <br>Organization of an Intellectual Technological Searching Cycle to Support Making Decisions During a Space Vehicles (SV) Remote Control<br> <br>Capabilities of Multiagent-Based Cargo Layout System for H-II Transfer Vehicle<br> <br>Development of Navigation Algorithm Architecture for Automatic Landing Based on Landmarks Image Processing<br> <br>Dynamic Models of Comprehensive Scheduling for Ground-Based Facilities Communication with Navigation Spacecrafts<br> <br>Corrections of a Vestibular Function Under Extreme Conditions of the Aerospace Flight<br> <br>Control of the Times of Engine Shutdown by the Launch Safety Criterion<br> <br>Observability Analysis of a Geostationary Satellite Autonomous Navigation System<br> <br>An Information Fusion Method for Satellite Autonomous Celestial Navigation<br> <br>Synergy in Power and Momentum Management for Spacecraft Using Double Gimbaled Solar Arrays<br><br>The Autonomous Constellation Formation-Keeping Control Exploiting Orbital Maneuver Efficiency<br><br>ENVISAT Payload Operations Planning - The End-To-End View And Experience<br> <br>Formation of Special Balance Mode for a Return Space Vehicle in Dynamics of Atmospheric Descent<br><br>Autonomous Orbit Control Strategy for Accurate Large Delta-V Manoeuvres in Planck Spinning S/C<br> <br>SPACE ROBOTICS AND MANIPULATORS<br><br>Quantitative Feedback Theory Applied to Orbital Rendezvous<br> <br>New Direction on Robotic Hands Design for Space Applications<br> <br>ROKVISS – Space Robotics Dynamics and Control Performance Experiments at the ISS<br> <br>Autonomous Robot Navigation Using Traversability Indices<br> <br>Experimental Demonstration of Coordinated Control for Multi-Vehicle Teams<br> <br>Cognitive Tools for Humanoid Robots in Space<br><br>Trajectory Control of Autonomous Vehicles in Viscous Media<br> <br>Dynamical Analysis for Task Configuration of Redundant Flexible Space Manipulator on Space Platform<br> <br>Robot/Balloon Facility for Autonomous Robotic Grasping of Objects in Space<br> <br><br>GUIDANCE AND CONTROL THEORY AND ANALYSIS<br><br>Filtering, Prediction and Smoothing with Point-Mass Approach<br> <br>Decentralized Iterative Learning Control Schemes for Large Scale Systems Including Delayed State <br>Perturbations in the Interconnections<br><br>Comparison of H-inf and Coefficient Diagram Method in Aerospace<br> <br>Synthesis of Optimal and Suboptimal Adaptive Control Systems Under Bounded Disturbances<br> <br>Logic and Numerical Methods of Spacecraft Attitude Control and Reconfiguration<br> <br>On the Refinement of Discretization for Optimal Control Problems<br> <br>Computer Aided Modelling and Analytical Synthesis of Control Algorithms for a Spacecraft with Discretely Changing Structure<br> <br>Energy Speed-Gradient Control of Satellite Oscillations<br> <br>Longitudinal Anisotropy-Based Flight Control in a Wind Shear<br> <br>h- Robust Algorithms of Flight Control on Variable Asymmetrical Limitations<br> <br>Influence of Time Delay on Engagement Process Under Proportional Navigation Law<br> <br>Sample Size Adaptation for Particle Filters<br> <br>A Discrete-Time Adaptive Control Scheme Based on Interval Persistency<br> <br>An Improved Recursive Interacting Multi-Model Algorithm Based on Genetic Algorithm<br> <br>Unified Approach for Open-Loop Optimal Control with Applications to Aerospace Systems<br> <br>Explicit Guidance for an Oblate Gravitational Field<br> <br><br>FLIGHT CONTROL FOR AIRCRAFT AND HELICOPTERS<br><br>AWIATOR’s Study of a Wing Load Control: Design and Flight-Test Results<br> <br>Aircraft-on-Ground Lateral Control for Low Speed Maneuvers<br> <br>Hybrid Model for Receding Horizon Guidance of Agile Autonomous Rotorcraft<br> <br>Controller Design in Presence of Non-Smooth Nonlinearity: A Flight Control Example<br> <br>An Agent Based Framework for Control of Merging Air-Traffic<br> <br>Aircraft Guidance Law Analysis<br> <br>Automatically Controlled Ekranoplanes: Experience and Problems<br> <br>Some Problems of Design of Computer-Based Training Systems for Civil Aviation Pilots, Methods of their Solving<br> <br>Invariant and Periodic Filters for Helicopter Vibration Attenuation<br> <br>An Overview of Compressor Instabilities: Basic Concepts and Control<br> <br>Control Design for F-16 Longitudinal Motion<br> <br>A System Identification Approach to Assessing Airline Pilot Skills<br> <br>Problem of Optimal Control of the Local System of Aircrafts (LSA) Resources on the Basis of the Game Forecast<br> <br>Regulated Air Traffic Flow Simulation Tool<br> <br>Nonlinear Dynamics of a Gyroplane Rotor<br> <br>Air-Breathing Hypersonic Flight Control Dynamics of Coupled Flap-Lag Motion by the Helicopter Rotor Blades <br><br><br>VOLUME 2<br><br>MISSILE GUIDANCE, NAVIGATION AND CONTROL<br><br>On the Optimal Estimator of Randomly Maneuvering Targets for Terminal Guidance<br> <br>Multi-Objective Frequency Loop-Shaping of a Lateral Missile Autopilot<br> <br>3D Nonlinear H2/H¥ Adaptive Guidance Law for Homing Missiles<br> <br>High-Precision Navigation and Guidance Systems of Aerial Vehicles is the Use of Computer Vision Technologies<br> <br>Shunting Method for Control of Homing Missiles with Uncertain Parameters<br> <br>Variable Speed Missile Guidance Law Against a Maneuvering Target<br> <br>Differential Geometric Guidance Based on the Involute of the Target’s Trajectory: 3-D Aspect<br><br>Extensive Comparison Between Quantitative Pursuit Evasion Game Guidance Law and PNS<br> <br>Terminal Missile Guidance Using a Semi-Markov Target Model<br> <br>The Multiple Hypothesis Extension of the Information Set-Based Tracking Algorithm for Multi-Target Environment<br> <br>Integrated Guidance and Control of Missiles with è-D Method<br> <br>Zero Miss Interception Guidance: Cheap Control Approach<br> <br>Advanced Fuzzy Side Force Control for Missile Against Hypersonic Target<br> <br>Avionic of Fifth-Generation for Seekers of Smart Weapon<br> <br>Optimal Guidance Law for Impact Angle Control<br><br>3-D Biased PNG for Evasive Maneuver of Anti-Ship Missiles Against CIWS<br> <br>Autopilot Design for Agile Missile Using Time-Varying Control Technique<br> <br>Feedback Control of MEMS Gyroscope to Achieve the Tactical-Grade Specifications <br><br><br>ROBUST CONTROL FOR AEROSPACE APPLICATIONS<br><br>QFT/H¥ Control of a Small Solar Thermal Transfer Vehicle (SOTV) with Inflatable Appendages<br> <br>Robust Digital Control of Drag-Free Satellites<br><br>Robust Nonlinear Control of a Spacecraft during Landing Maneuvers on a Planet<br> <br>The m-Synthesis Applied to a Launcher Control<br><br>The Generalized (µ, MU )-Iteration Illustrated by Flexible Aircraft Robust Control<br> <br>An Alternative to Circumvent HJI Computation Difficulty in Nonlinear Robustness Analysis<br> <br>Robustness Analysis of a Nonlinear Missile Autopilot via Integral Quadratic Constraints<br><br>Aeroservoelastic Analysis of Missile Control Surfaces via Robust Control Methods<br> <br>Robust Computer Image Analysis for Flight Vehicles Navigation and Guidance<br> <br>Robust GPS C/A Code Tracking Based on H¥ Control<br><br>High-Precision Attitude Control of Remote Sensing Satellite<br> <br><br>VOLUME 3<br><br>SENSORS, ON-BOARD EQUIPMENT AND SIGNAL PROCESSING<br><br>3-Axes Attitude Estimation Experiments Using CCD Earth Sensor<br> <br>DEIS UAV: GNC Design and Avionics Implementation Issues<br> <br>A Rendezvous and Docking Sensor Using a Videometer SpaceWire Satellite Onboard Data-Handling Networks<br> <br>Integrated Sensor/Actuator FDI Based on RKF Insensitive to Sensor Failures<br> <br>Experimental Evaluation of the Micro-Tech.-Sensor for Attitude and Orbit Determination<br> <br>Stationkeeping and Slewing Control of a Multi-Tethered Aerostat<br> <br>The Conception of Electric Propulsion Systems Vector Control<br> <br>Modelling Real-Time Behaviour of Soft Computations within Integrated Avionics Systems<br> <br>The Data Flow and Distributed Calculations Intelligence Information Technology for Decision Support Embeded System in Real Time<br> <br>Integrated Modular Spacecraft Avionics.Architecture and SpaceWire-Based Implementation<br> <br>Nutation Stability Study of Flywheel Rotor Supported by AMB<br> <br>Nonlinear Filtering, Interpolation and Extrapolation in Stochastic Systems Under Continuous and Discrete Observations with Memory<br><br>Automatic Real-Time Star Detection Technique<br><br>The Problems of Characteristic Stabilization for Micromechanical Gyroscopes<br> <br>MCFLIGHT™ – Systems-on-Chip for Aerospace Applications<br> <br>Micro Sun Sensor for Spacecraft Attitude Control<br><br>Feedback Controller Design for the Basic Science Mode of the LISA Pathfinder Mission<br> <br>Measuring Microaccelerations Aboard Spacecrafts<br> <br>FAULT-TOLERANT CONTROL SYSTEMS FOR AEROSPACE APPLICATIONS<br><br>Development and Evaluation of Fault-Tolerant Flight Control for RLV by Mutual Compensation with <br>Available Aerosurfaces<br> <br>Sensor Fault Diagnosis of Singularly Perturbed Systems Applied to F-8 Flight Dynamic<br> <br>Fault Detection and Diagnosis of a Linear Hydraulic Servo Axis<br> <br>FDI for Inertial Sensor using Single Antenna GPS Receiver<br> <br>Residual Generator Computation for Fault Detection of a General Aviation Aircraft<br> <br>Extended Parity Space Approach Considering Two-Faults<br> <br>Design and Analysis of Helicopter Fault-Tolerant Flight Control System<br> <br><br>STUDENT AEROSPACE PROJECTS<br><br>System Design and Attitude Control Analyses for the Pico-Satellite UWE-1<br> <br>Russian Multifunctional Education-Research Students’ Satellite “Mozhaetz” on the Orbit<br> <br>University of Tokyo's Student Nano-Satellite Project CubeSat-XI and Its On-Orbit Experiment Results<br> <br>Application of the Robust Approach to the Problem of Airborne Gravimetry<br> <br>Micro-Gravity Isolation using Only Electo-Magnetic Actuators<br> <br>Autonomous Parafoil Control Experiment as “Comeback Competition” for Effective First Step Training Towards Satellite Development<br> <br>Method of Conflict-Optimum Guidance of the Wing of Two Aircrafts on the Basis of the Stable-Effective Compromise<br> <br>Tokyo Tech 1kg Pico-Satellite CUTE-I - Development, Launch & Operations<br> <br>Kansas Universities’ Technology Evaluation Satellite Program<br> <br>The Spatial Reconstruction of Earth Surface by Stereoimages<br> <br>The AAU-Cubesat Student Satellite Project: Architectural Overview and Lessons Learned<br> <br>Active Angular Stabilization of the GAIA Space Telescope Through Laser Interferometry<br> <br><br>LAUNCHER CONTROL<br><br>Launcher Attitude Control: Some Answers to the Robustness Issue<br> <br>Robust Impulse-to-Peak Synthesis: Application to the Control of an Aerospace Launcher<br> <br>Mathematical Models and Software for Flexible Vehicle Simulation<br> <br>Flexible Launch Vehicle Attitude Control Design Using Coevolutionary Algorithm<br> <br>Load Relief Control of H-IIA Launch Vehicle<br><br>Semi- Active Vibration Isolation System for Launch Vehicles<br> <br>Control Aspects of Aerospace Plane Docking and Undocking with Moving Ekranoplane<br> <br>Robust Control of a Space Launcher by Introducing LQG/LTR Ideas in the NCF Robust Stabilisation Problem<br> <br>An Adaptive Tuning Strategy of PID Attitude Control System<br> <br>Modelling and Simulation of Flexibility Induced Disturbances for a Flying Rocket<br> <br>Analytical Method for Computing Controller Gains of a Satellite Launcher<br> <br>A Proof-of-Concept Approach for Horizontal Take-Off/Landing Rocket Plane <br><br><br>GAS TURBINE ENGINE HEALTH MONITORING<br><br>Correlated Fault Modelling for Diagnostics and Monitoring of GTE Control Systems<br> <br>Condition Monitoring of Gas Turbine Engine Transmission<br> <br>Investigation of Genetic Algorithms On-Line Application for Aero Engine Modelling and Condition Monitoring<br> <br>Gas-Turbine Engine Control System of the Unmanned Airplane<br> <br>Linearization and Identification of Aircraft Turbofan Engine Models<br> <br>Development of a Condition Monitoring Module for Aircraft Engines and it’s Experimental Investigation<br><br> <br>COOPERATIVE CONTROL<br><br>A Formal Approach for Decentralised Co-Ordination Among UAVs Using Hybrid Control<br> <br>Asynchronous Switching Decentralized Controllers for Spacecraft Formations<br> <br>Target Arrival Coordination in Boid Based Formation Flight<br> <br>A Command Governor Approach to Formation Flying Control Problems<br> <br>On-Line Evolutionary Algorithm Guidance for Multiple Missiles Against Multiple Targets<br> <br><br>SATELLITE NAVIGATION SYSTEMS GPS/GLONASS APPLICATION<br><br>Commercial Use of GNSS Signals in GEO<br> <br>A Miniaturised GPS Receiver for Space Application<br><br>FDI Algorithms for GPS Signals: A Different Perspective of a Known Problem<br> <br>Flight Data Analysis of ADEOS-II GPS Receivers<br><br>A New Error Compensation Scheme for INS Vertical Channel<br> <br>Preliminary Tests of GPS/HAPS Positioning System Using a Pseudolite on Helicopter<br> <br>LAAS Ground Facility and Navigation Virtual Laboratory Integration Aspects: A Mixed Real/Simulated Environment to Test DGNSS Avionics<br><br>Flight Evaluation of GPS Aided Inertial-Navigation Avionics with GBAS and SBAS Augmentation<br> <br>GLONASS/GPS Monitoring Equipment <br><br>Author Index