Automatic Control in Aerospace 2004

AvAlexander Nebylov

Häftad, Engelska, 2005

Del i serien IPV - IFAC Proceedings Volume

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Produktinformation

Utgivningsdatum:2005-07-19
Mått:210 x 298 x 0 mm
Vikt:1 110 g
Format:Häftad
Språk:Engelska
Serie:IPV - IFAC Proceedings Volume
Antal sidor:600
Förlag:Elsevier Science
ISBN:9780080440132

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VOLUME 1PLENARY PAPERSRussian Space Programs: Achievements and Prospects of Automatic Control ApplicationsControl and Navigation Aspects of the New ESA Earth Observation MissionsCurrent Status of Japanese Aerospace Programs - Focusing on the High Speed Flight DemonstrationNational Achievements in Control Theory (The Aerospace Perspective)Model-Based Fault Detection and Diagnosis - Status and ApplicationsSPACECRAFT ATTITUDE AND ORBIT CONTROL On the Precision Attitude Control ProblemsControl System of the Microsatellite “MicronVisual Feedback Attitude Control Experiment of a Bias Momentum Micro SatelliteGraph Models of Orbital Assembly and Dynamics of a Large Space StructurePosition Control Design and Validation Applied to ATV During Docking to ISSOn-Orbit Operation and Performance of Micro LabSat Attitude Control SubsystemNonlinear Dynamics of a Spacecraft Respinup by a Weak Internal ControlSystematic Approach to Achieve Fine Pointing Requirement of SOLAR-BOnboard Control Complex for Vehicles Implementation Concept by ISS ExampleA Novel Architecture for Magnetic Attitude Control of Gravity Gradient SatellitesAccurate Modes Design of the Darwin Precursor Formation Flying Demonstration MissionSpacecraft Disposal on a Graveyard Orbit: The In-Flight AOCS Performance for Eurostar 2000 and SPOT 1 during End-of-Life OperationsDevelopment of Attitude Control System of Micro LabSatSteering the Control Moment Gyroscope Clusters Onboard High-Agile SpacecraftMicrovibration Management and Pointing Stability Analysis of SELENE SatelliteThree DOF Optimal Thrusters Selection and Modulation for Space VehiclesLessons Learned from the Object-Oriented Design of the BIRD Attitude Control System SoftwareA Lyapunov-Typed Nonlinear Attitude Controller for SpacecraftIntegrated Power and Attitude Control Using VSCMGs for Small Agile SatelliteAdvance of Chinese Spacecraft Control TechnologiesAn Autonomous Celestial Navigation Method for Geosychronous SatelliteOrbit Dynamics and Kinematics with Full QuaternionsAUTONOMOUS CONTROL, MISSION CONTROL AND OPERATIONSOverview of Recent Control Technology for Japanese Scientific Space MissionsOverview of the Attitude and Orbit Control Systems (AOCS) Developed for NASDA/JAXA Engineering Test and Applications SatellitesAutonomous Navigation Concepts for Interplanetary MissionsMechanics and Motion Control of a Space Vehicle in the Project of Relict Substance Delivery on Earth (The Project “Phobos_Grunt)Orbit Acquisition of the Disaster Monitoring Constellation – Preliminary ResultsOn-Orbit Experiment of Motion Estimation and Tracking of Tumbling Object in SpaceElectric Propulsions as Actuators of the Spacecraft Flight Control SystemsSingle-Pulse Correction of the Re-Entry Point of a Payload ModuleEnd-to-End Modeling for Drag-Free Missions with Application to LISA PathfinderOrganization of an Intellectual Technological Searching Cycle to Support Making Decisions During a Space Vehicles (SV) Remote ControlCapabilities of Multiagent-Based Cargo Layout System for H-II Transfer VehicleDevelopment of Navigation Algorithm Architecture for Automatic Landing Based on Landmarks Image ProcessingDynamic Models of Comprehensive Scheduling for Ground-Based Facilities Communication with Navigation SpacecraftsCorrections of a Vestibular Function Under Extreme Conditions of the Aerospace FlightControl of the Times of Engine Shutdown by the Launch Safety CriterionObservability Analysis of a Geostationary Satellite Autonomous Navigation SystemAn Information Fusion Method for Satellite Autonomous Celestial NavigationSynergy in Power and Momentum Management for Spacecraft Using Double Gimbaled Solar ArraysThe Autonomous Constellation Formation-Keeping Control Exploiting Orbital Maneuver EfficiencyENVISAT Payload Operations Planning - The End-To-End View And ExperienceFormation of Special Balance Mode for a Return Space Vehicle in Dynamics of Atmospheric DescentAutonomous Orbit Control Strategy for Accurate Large Delta-V Manoeuvres in Planck Spinning S/CSPACE ROBOTICS AND MANIPULATORSQuantitative Feedback Theory Applied to Orbital RendezvousNew Direction on Robotic Hands Design for Space ApplicationsROKVISS – Space Robotics Dynamics and Control Performance Experiments at the ISSAutonomous Robot Navigation Using Traversability IndicesExperimental Demonstration of Coordinated Control for Multi-Vehicle TeamsCognitive Tools for Humanoid Robots in SpaceTrajectory Control of Autonomous Vehicles in Viscous MediaDynamical Analysis for Task Configuration of Redundant Flexible Space Manipulator on Space PlatformRobot/Balloon Facility for Autonomous Robotic Grasping of Objects in SpaceGUIDANCE AND CONTROL THEORY AND ANALYSISFiltering, Prediction and Smoothing with Point-Mass ApproachDecentralized Iterative Learning Control Schemes for Large Scale Systems Including Delayed State Perturbations in the InterconnectionsComparison of H-inf and Coefficient Diagram Method in AerospaceSynthesis of Optimal and Suboptimal Adaptive Control Systems Under Bounded DisturbancesLogic and Numerical Methods of Spacecraft Attitude Control and ReconfigurationOn the Refinement of Discretization for Optimal Control ProblemsComputer Aided Modelling and Analytical Synthesis of Control Algorithms for a Spacecraft with Discretely Changing StructureEnergy Speed-Gradient Control of Satellite OscillationsLongitudinal Anisotropy-Based Flight Control in a Wind Shearh- Robust Algorithms of Flight Control on Variable Asymmetrical LimitationsInfluence of Time Delay on Engagement Process Under Proportional Navigation LawSample Size Adaptation for Particle FiltersA Discrete-Time Adaptive Control Scheme Based on Interval PersistencyAn Improved Recursive Interacting Multi-Model Algorithm Based on Genetic AlgorithmUnified Approach for Open-Loop Optimal Control with Applications to Aerospace SystemsExplicit Guidance for an Oblate Gravitational FieldFLIGHT CONTROL FOR AIRCRAFT AND HELICOPTERSAWIATOR’s Study of a Wing Load Control: Design and Flight-Test ResultsAircraft-on-Ground Lateral Control for Low Speed ManeuversHybrid Model for Receding Horizon Guidance of Agile Autonomous RotorcraftController Design in Presence of Non-Smooth Nonlinearity: A Flight Control ExampleAn Agent Based Framework for Control of Merging Air-TrafficAircraft Guidance Law AnalysisAutomatically Controlled Ekranoplanes: Experience and ProblemsSome Problems of Design of Computer-Based Training Systems for Civil Aviation Pilots, Methods of their SolvingInvariant and Periodic Filters for Helicopter Vibration AttenuationAn Overview of Compressor Instabilities: Basic Concepts and ControlControl Design for F-16 Longitudinal MotionA System Identification Approach to Assessing Airline Pilot SkillsProblem of Optimal Control of the Local System of Aircrafts (LSA) Resources on the Basis of the Game ForecastRegulated Air Traffic Flow Simulation ToolNonlinear Dynamics of a Gyroplane RotorAir-Breathing Hypersonic Flight Control Dynamics of Coupled Flap-Lag Motion by the Helicopter Rotor BladesVOLUME 2MISSILE GUIDANCE, NAVIGATION AND CONTROLOn the Optimal Estimator of Randomly Maneuvering Targets for Terminal GuidanceMulti-Objective Frequency Loop-Shaping of a Lateral Missile Autopilot3D Nonlinear H2/H¥ Adaptive Guidance Law for Homing MissilesHigh-Precision Navigation and Guidance Systems of Aerial Vehicles is the Use of Computer Vision TechnologiesShunting Method for Control of Homing Missiles with Uncertain ParametersVariable Speed Missile Guidance Law Against a Maneuvering TargetDifferential Geometric Guidance Based on the Involute of the Target’s Trajectory: 3-D AspectExtensive Comparison Between Quantitative Pursuit Evasion Game Guidance Law and PNSTerminal Missile Guidance Using a Semi-Markov Target ModelThe Multiple Hypothesis Extension of the Information Set-Based Tracking Algorithm for Multi-Target EnvironmentIntegrated Guidance and Control of Missiles with è-D MethodZero Miss Interception Guidance: Cheap Control ApproachAdvanced Fuzzy Side Force Control for Missile Against Hypersonic TargetAvionic of Fifth-Generation for Seekers of Smart WeaponOptimal Guidance Law for Impact Angle Control3-D Biased PNG for Evasive Maneuver of Anti-Ship Missiles Against CIWSAutopilot Design for Agile Missile Using Time-Varying Control TechniqueFeedback Control of MEMS Gyroscope to Achieve the Tactical-Grade SpecificationsROBUST CONTROL FOR AEROSPACE APPLICATIONSQFT/H¥ Control of a Small Solar Thermal Transfer Vehicle (SOTV) with Inflatable AppendagesRobust Digital Control of Drag-Free SatellitesRobust Nonlinear Control of a Spacecraft during Landing Maneuvers on a PlanetThe m-Synthesis Applied to a Launcher ControlThe Generalized (µ, MU )-Iteration Illustrated by Flexible Aircraft Robust ControlAn Alternative to Circumvent HJI Computation Difficulty in Nonlinear Robustness AnalysisRobustness Analysis of a Nonlinear Missile Autopilot via Integral Quadratic ConstraintsAeroservoelastic Analysis of Missile Control Surfaces via Robust Control MethodsRobust Computer Image Analysis for Flight Vehicles Navigation and GuidanceRobust GPS C/A Code Tracking Based on H¥ ControlHigh-Precision Attitude Control of Remote Sensing SatelliteVOLUME 3SENSORS, ON-BOARD EQUIPMENT AND SIGNAL PROCESSING3-Axes Attitude Estimation Experiments Using CCD Earth SensorDEIS UAV: GNC Design and Avionics Implementation IssuesA Rendezvous and Docking Sensor Using a Videometer SpaceWire Satellite Onboard Data-Handling NetworksIntegrated Sensor/Actuator FDI Based on RKF Insensitive to Sensor FailuresExperimental Evaluation of the Micro-Tech.-Sensor for Attitude and Orbit DeterminationStationkeeping and Slewing Control of a Multi-Tethered AerostatThe Conception of Electric Propulsion Systems Vector ControlModelling Real-Time Behaviour of Soft Computations within Integrated Avionics SystemsThe Data Flow and Distributed Calculations Intelligence Information Technology for Decision Support Embeded System in Real TimeIntegrated Modular Spacecraft Avionics.Architecture and SpaceWire-Based ImplementationNutation Stability Study of Flywheel Rotor Supported by AMBNonlinear Filtering, Interpolation and Extrapolation in Stochastic Systems Under Continuous and Discrete Observations with MemoryAutomatic Real-Time Star Detection TechniqueThe Problems of Characteristic Stabilization for Micromechanical GyroscopesMCFLIGHT™ – Systems-on-Chip for Aerospace ApplicationsMicro Sun Sensor for Spacecraft Attitude ControlFeedback Controller Design for the Basic Science Mode of the LISA Pathfinder MissionMeasuring Microaccelerations Aboard Spacecrafts FAULT-TOLERANT CONTROL SYSTEMS FOR AEROSPACE APPLICATIONSDevelopment and Evaluation of Fault-Tolerant Flight Control for RLV by Mutual Compensation with Available AerosurfacesSensor Fault Diagnosis of Singularly Perturbed Systems Applied to F-8 Flight DynamicFault Detection and Diagnosis of a Linear Hydraulic Servo AxisFDI for Inertial Sensor using Single Antenna GPS ReceiverResidual Generator Computation for Fault Detection of a General Aviation AircraftExtended Parity Space Approach Considering Two-FaultsDesign and Analysis of Helicopter Fault-Tolerant Flight Control SystemSTUDENT AEROSPACE PROJECTSSystem Design and Attitude Control Analyses for the Pico-Satellite UWE-1Russian Multifunctional Education-Research Students’ Satellite “Mozhaetz on the OrbitUniversity of Tokyo's Student Nano-Satellite Project CubeSat-XI and Its On-Orbit Experiment ResultsApplication of the Robust Approach to the Problem of Airborne GravimetryMicro-Gravity Isolation using Only Electo-Magnetic ActuatorsAutonomous Parafoil Control Experiment as “Comeback Competition for Effective First Step Training Towards Satellite DevelopmentMethod of Conflict-Optimum Guidance of the Wing of Two Aircrafts on the Basis of the Stable-Effective CompromiseTokyo Tech 1kg Pico-Satellite CUTE-I - Development, Launch & OperationsKansas Universities’ Technology Evaluation Satellite ProgramThe Spatial Reconstruction of Earth Surface by StereoimagesThe AAU-Cubesat Student Satellite Project: Architectural Overview and Lessons LearnedActive Angular Stabilization of the GAIA Space Telescope Through Laser InterferometryLAUNCHER CONTROLLauncher Attitude Control: Some Answers to the Robustness IssueRobust Impulse-to-Peak Synthesis: Application to the Control of an Aerospace LauncherMathematical Models and Software for Flexible Vehicle SimulationFlexible Launch Vehicle Attitude Control Design Using Coevolutionary AlgorithmLoad Relief Control of H-IIA Launch VehicleSemi- Active Vibration Isolation System for Launch VehiclesControl Aspects of Aerospace Plane Docking and Undocking with Moving EkranoplaneRobust Control of a Space Launcher by Introducing LQG/LTR Ideas in the NCF Robust Stabilisation ProblemAn Adaptive Tuning Strategy of PID Attitude Control SystemModelling and Simulation of Flexibility Induced Disturbances for a Flying RocketAnalytical Method for Computing Controller Gains of a Satellite LauncherA Proof-of-Concept Approach for Horizontal Take-Off/Landing Rocket PlaneGAS TURBINE ENGINE HEALTH MONITORINGCorrelated Fault Modelling for Diagnostics and Monitoring of GTE Control SystemsCondition Monitoring of Gas Turbine Engine TransmissionInvestigation of Genetic Algorithms On-Line Application for Aero Engine Modelling and Condition MonitoringGas-Turbine Engine Control System of the Unmanned AirplaneLinearization and Identification of Aircraft Turbofan Engine ModelsDevelopment of a Condition Monitoring Module for Aircraft Engines and it’s Experimental InvestigationCOOPERATIVE CONTROLA Formal Approach for Decentralised Co-Ordination Among UAVs Using Hybrid ControlAsynchronous Switching Decentralized Controllers for Spacecraft FormationsTarget Arrival Coordination in Boid Based Formation FlightA Command Governor Approach to Formation Flying Control ProblemsOn-Line Evolutionary Algorithm Guidance for Multiple Missiles Against Multiple TargetsSATELLITE NAVIGATION SYSTEMS GPS/GLONASS APPLICATIONCommercial Use of GNSS Signals in GEOA Miniaturised GPS Receiver for Space ApplicationFDI Algorithms for GPS Signals: A Different Perspective of a Known ProblemFlight Data Analysis of ADEOS-II GPS ReceiversA New Error Compensation Scheme for INS Vertical ChannelPreliminary Tests of GPS/HAPS Positioning System Using a Pseudolite on HelicopterLAAS Ground Facility and Navigation Virtual Laboratory Integration Aspects: A Mixed Real/Simulated Environment to Test DGNSS AvionicsFlight Evaluation of GPS Aided Inertial-Navigation Avionics with GBAS and SBAS AugmentationGLONASS/GPS Monitoring EquipmentAuthor Index