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Publications » Technology » Automation

Automatic Control in Aerospace 2004 (3 Volume Set)

Price £220.00

temporarily out of stock

Automatic Control in Aerospace 2004 (3 Volume Set)

Alexander Nebylov

ISBN 0080440134
Pages 600

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