Automatic Control in Aerospace 2004

Edited By

  • Alexander Nebylov

 

Book information

  • Published: July 2005
  • Imprint: ELSEVIER
  • ISBN: 978-0-08-044013-2


Table of 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