Automatic Control in Aerospace 2004

Automatic Control in Aerospace 2004

1st Edition - July 19, 2005

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  • Editor: Alexander Nebylov
  • Paperback ISBN: 9780080440132

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Table of Contents

  • VOLUME 1


    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


    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


    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


    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


    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


    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


    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


    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


    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


    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


    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 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


    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


    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


    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

Product details

  • No. of pages: 600
  • Language: English
  • Copyright: © Elsevier Science 2005
  • Published: July 19, 2005
  • Imprint: Elsevier Science
  • Paperback ISBN: 9780080440132

About the Editor

Alexander Nebylov

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