Automatic Control in Aerospace 2004 book cover

Automatic Control in Aerospace 2004

Paperback, 600 Pages

Published: July 2005

Imprint: Elsevier

ISBN: 978-0-08-044013-2

Contents

  • VOLUME 1PLENARY PAPERSRussian 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 OPERATIONSOverview 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 MANIPULATORSQuantitative 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 ANALYSISFiltering, 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 HELICOPTERSAWIATOR’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 2MISSILE GUIDANCE, NAVIGATION AND CONTROLOn the Optimal Estimator of Randomly Maneuvering Targets for Terminal Guidance
    Multi-Objective Frequency Loop-Shaping of a Lateral Missile Autopilot
    3D Nonlinear H2/HÂ¥ 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 APPLICATIONSQFT/HÂ¥ 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 HÂ¥ Control
    High-Precision Attitude Control of Remote Sensing Satellite
    VOLUME 3SENSORS, ON-BOARD EQUIPMENT AND SIGNAL PROCESSING3-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 APPLICATIONSDevelopment 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 PROJECTSSystem 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 CONTROLLauncher 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 MONITORINGCorrelated 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 CONTROLA 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 APPLICATIONCommercial 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

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