Table Of Content

JOURNAL OF GUIDANCE, CONTROL, AND DYNAMICS Volume 27, No. 6, November—December 2004 2004 Journal of Guidance, Control, and Dynamics Index How to Use the Index In the Subject Index, pages 1109-1112, each technical paper is listed under a maximum of three appropriate headings. Note the locating number in boldface type preceding each paper title, and use that number to find the paper in the Chronological Index. The Author Index, page 1113, lists all authors associated with a given technical paper. The locating numbers are iden- tical to those in the Subject Index. The Chronologicai Index, pages 1114-1119, also lists all papers by their locating numbers. This listing contains titles, authors and their affiliations, and volume, issue number, and page where the paper appeared. It also gives the AIAA paper number, if any, on which the article was based. The book review index is listed on page 1119. Comments, Replies, and Errata are listed directly beneath the paper to which they refer. If the paper to which they refer was published prior to 2004, that paper also will appear in both the Subject and Chronological Indexes. Authors of Comments also are listed in the Author Index. Subject Index AIRCRAFT TECHNOLOGY, G04-108 Linear Theory of a Rotating Internal GUIDANCE, CONTROL, AND CONVENTIONAL, STOL/VTOL Part Projectile Configuration in Atmospheric DYNAMICS TECHNOLOGY Flight Aerodynamics G04-126 Retargeting Dynamics of a Linear Aircraft Dynamics Tethered Interferometer G04-044 Nanosatellite Attitude Stabilization G04-101 Time Simulations of the Response of Using Passive Aerodynamics and Active Mag- Performance Maneuvering Flexible Aircraft netic Torquing G04-035 Approximate Analytical Criterion for G04-110 Singular Perturbation Analysis of Opti- Aircraft Wing Rock Onset Aeroelasticity and Aeroservoelasticity mal Glide G04-038 Square Root Sigma Point Filtering for G04-004 Control of a Nonlinear Wing Section Rotorcraft Real-Time, Nonlinear Estimation Using Leading- and Trailing-Edge Surfaces G04-088 Unified Algebraic Approach to G04-028 Dynamics and Stability of an Autoro- G04-099 Aeroelasticity of Time-Delayed Feed- Approximation of Lateral-Directional Modes tating Rotor/Wing Unmanned Aircraft back Control of Two-Dimensional Supersonic and Departure Criteria Lifting Surfaces Simulation G04-099 Aeroelasticity of Time-Delayed Feed- G04-078 Computation of Controllability back Control of Two-Dimensional Supersonic Regions for Unstable Aircraft Dynamics G04-126 Retargeting Dynamics of a Linear Lifting Surfaces Tethered Interferometer G04-074 Tuning of Observer-Based Controllers Air Transportation G04-002 Synthesis of Optimal Control and G04-092. New Approach for Modeling, Analysis, Flight Testing of an Autonomous Circular Para- Aircraft Guidance and Control of Air Traffic Flow chute G04-053 Adaptive Neural Network Inverse Con- G04-131 Nonminimal Kane’s Impulse-Momen- troller for General Aviation Safety Communication and Air Traffic Control tum Relations G04-101 Time Simulations of the Response of Aircraft Stability and Control G04-092_ New Approach for Modeling, Analysis, Maneuvering Flexible Aircraft and Control of Air Traffic Flow G04-053 Adaptive Neural Network Inverse Con- Testing, Flight and Ground troller for General Aviation Safety Deceleration Systems G04-019 Flight Control Century: Triumphs of G04-002 Synthesis of Optimal Control and G04-002 Synthesis of Optimal Control and the Systems Approach Flight Testing of an Autonomous Circular Para- Flight Testing of an Autonomous Circular Para- G04-099 Aeroelasticity of Time-Delayed Feed- chute chute back Control of Two-Dimensional Supersenic G04-001 Evolution, Revolution, and Challenges Lifting Surfaces Flight Control Integration of Handling Qualities G04-087 Gain-Scheduling Stability Issues Using G04-019 Flight Control Century: Triumphs of Differential Inclusion and Fuzzy Systems ENERGY the Systems Approach G04-078 Computation of Controllability Regions for Unstable Aircraft Dynamics Flight Mechanics Flywhee!s G04-089 Limit Cycles and Domain of Stability G04-110 Singular Perturbation Analysis of Opti- G04-047 Singularity Analysis of Variable Speed in Unsteady Aeroelastic System mal Glide Control Moment Gyros G04-016 Partial Eigenstructure Assignment G04-003 Flight-Test Evaluation of Stability G04-105 Integrated Power and Attitude Control Approach for Robust Flight Control Augmentation Steering System for Aircraft with Spacecraft Flywheels and Control Moment G04-098 Adaptive Linear Parameter Varying Ground Handling Gyroscopes Control Synthesis for Actuator Failure 1109 1110 J. GUIDANCE, VOL. 27, NO. 6: 2004 INDEX G04-001 Evolution, Revolution, and Challenges G04-005 Gain-Phase Margin Analysis of Pilot- G04-048 Augmenting Adaptive Approach to of Handling Qualities Induced Oscillations for Limit-Cycle Prediction Control of Flexible Systems G04-035 Approximate Analytical Criterion for G04-023 Adaptive Control Design for Nonaffine G04-043 Dual Controller Approach to Three- Aircraft Wing Rock Onset Models Arising in Flight Control Dimensional Autonomous Formation Control G04-055 Aircraft Autopilot Analysis and Enve- 304-121 Efficient Minimax Control Design for Differential Games lope Protection for Operation Under Icing Con- Prescribed Parameter Uncertainty ditions G04-043 Dual Controller Approach to Three- G04-128 Genetic Algorithm Preprocessing for Artificial Intelligence Dimensional Autonomous Formation Control Numerical Solution of Differential Games Prob- G04-105 Integrated Power and Attitude Control lems G04-036 Learning-Based Sensor Validation with Spacecraft Flywheels and Control Moment G04-134 Trajectory Shaping in Linear Quadratic Scheme Within Flight Control Laws Gyroscopes Pursuit-Evasion Games G04-093 Neural-Network-Based Design of Astrodynamics Dynamics Optimal Controllers for Nonlinear Systems G04-025 Nonlinear Control of Librational G04-094 Human-Inspired Control Logic for G04-018 Nonlinear Modelling of Spacecraft Motion of Tethered Satellites in Elliptic Orbits Automated Maneuvering of Miniature Heli- Relative Motion in the Configuration Space G04-060 Second-Order Equations for Ren- copter G04-131 Nonminimal Kane’s Impulse-Momen- dezvous in a Circular Orbit G04-114 New Nonlinear Control Technique for tum Relations G04-065 Attitude Dynamics/Control of a Dual- Ascent Phase of Reusable Launch Vehicles G04-011 Robust Vibration Suppression in Flexi- BodySpacecraft with Variable-Speed Control G04-037 Application of Pseudospectral Meth- ble Systems Using Infinite Impulse Response Moment Gyros ods for Receding Horizon Control Digital Filters G04-059 Mars and Mercury Missions Using G04-065 Attitude Dynamics/Control of a Dual- G04-108 Linear Theory of a Rotating Internal Solar Sails and Solar Electric Propulsion BodySpacecraft with Variable-Speed Control Part Projectile Configuration in Atmospheric G04-020 History of Analytical Orbit Modeling Moment Gyros Flight in the U.S. Space Surveillance System G04-019 Flight Control Century: Triumphs of G04-065 Attitude Dynamics/Control of a Dual- G04-126 Retargeting Dynamics of a Linear the Systems Approach BodySpacecraft with Variable-Speed Control Tethered Interferometer G04-057_ mu Synthesis for a Small Commercial Moment Gyros G04-124 Transit-Orbit Search for Planar Aircraft: Design and Simulator Validation G04-031 First-Order Analytical Solution for Restricted Three-Body Problems with Perturba- Spacecraft Motion About (433) Eros tions Control System Effectors G04-018 Nonlinear Modelling of Spacecraft Flight Displays G04-029 Singularity Analysis and Visualization Relative Motion in the Configuration Space for Single-Gimbal Control Moment Gyro Sys- G04-013 Frenet-Based Algorithm for Trajectory G04-135 Earth Escape by Ideal Sail and Solar- tems Prediction Photon Thrustor Spacecraft G04-004 Control of a Nonlinear Wing Section Flight Mechanics Autonomous Vehicles Using Leading- and Trailing-Edge Surfaces G04-100 Investigating The Role of Rate Limit- G04-088 Unified Algebraic Approach to G04-112_ Methods for Compensating for Control ing in Pilot-Induced Oscillations Approximation of Lateral-Directional Modes Allocator and Actuator Interactions G04-112 Methods for Compensating for Control and Departure Criteria G04-049 Pseudospectral Knotting Methods for Allocator and Actuator Interactions G04-028 Dynamics and Stability of an Autoro- Solving Nonsmooth Optimal Control Problems tating Rotor/Wing Unmanned Aircraft G04-086 Guidance of Unmanned Air Vehicles Control Theory G04-035 Approximate Analytical Criterion for Based on Fuzzy Sets and Fixed Waypoints G04-038 Square Root Sigma Point Filtering for G04-032 Jacobi Pseudospectral Method for Aircraft Wing Rock Onset Real-Time, Nonlinear Estimation Solving Optimal Control Problems G04-100 Investigating The Role of Rate Limit- G04-007 Decentralized Scheme for Spacecraft G04-049 Pseudospectral Knotting Methods for ing in Pilot-Induced Oscillations Formation Flying via the Virtual Structure Solving Nonsmooth Optimal Control Problems G04-117 Unpowered Approach and Landing Approach G04-087 Gain-Scheduling Stability Issues Using Guidance Using Trajectory Planning G04-094 Human-Inspired Control Logic for Differential Inclusion and Fuzzy Systems G04-115 Dynamic Lateral Entry Guidance Automated Maneuvering of Miniature Heli- G04-106 Periodic H2 Synthesis for Spacecraft Logic copter Attitude Control with Magnetorquers G04-114 New Nonlinear Control Technique for G04-116 Test Results for Entry Guidance Meth- G04-016 Partial Eigenstructure Assignment Ascent Phase of Reusable Launch Vehicles ods for Space Vehicles Approach for Robust Flight Control Handling Qualities G04-043 Dual Controller Approach to Three- G04-017 Linear System Input-Order Reduction Dimensional Autonomous Formation Control by Hankel Norm Maximization G04-100 Investigating The Role of Rate Limit- G04-096 Anytime Control Algorithm: Model ing in Pilot-Induced Oscillations Computer Science Reduction Approach G04-003 Flight-Test Evaluation of Stability G04-096 Anytime Control Algorithm: Model G04-098 Adaptive Linear Parameter Varying Augmentation Steering System for Aircraft Reduction Approach Control Synthesis for Actuator Failure Ground Handling G04-005 Gain-Phase Margin Analysis of Pilot- G04-001 Evolution, Revolution, and Challenges Control System Design Induced Oscillations for Limit-Cycle Prediction of Handling Qualities G04-017 Linear System Input-Order Reduction G04-076 Robust Tracking Control Design for Information Processing by Hankel Norm Maximization Spacecraft Under Control Input Saturation G04-016 Partial Eigenstructure Assignment G04-129 Circular Navigation Missile Guidance G04-096 Anytime Control Algorithm: Model Approach for Robust Flight Control with Incomplete Information and Uncertain Reduction Approach G04-015 Nonlinear Adaptive Control for Slew- Autopilot Model G04-041 Covariance Control for Sensor Man- ing Flexible Active Structures G04-125 Low Thrust Minimum-Fuel Orbital agement in Cluttered Tracking Environments G04-123 Dynamic Control Allocation Using Transfer: A Homotopic Approach Intelligent Control Constrained Quadratic Programming G04-052 State-Space Approach to Computing G04-074 Tuning of Observer-Based Controllers Spacecraft Pointing Jitter G04-087 Gain-Scheduling Stability Issues Using G04-078 Computation of Controllability G04-050 Nonlinear Missile Autopilot Design Differential Inclusion and Fuzzy Systems Regions for Unstable Aircraft Dynamics with Theta-D Technique G04-006 Optimization of Interplanetary Solar G04-076 Robust Tracking Control Design for G04-025 Nonlinear Control of Librationai Sailcraft Trajectories Using Evclutionary Neuro- Spacecraft Under Control Input Saturation Motion of Tethered Satellites in Elliptic Orbits control G04-003 Flight-Test Evaluation of Stability G04-132 Differentiator-Free Nonlinear Propor- G04-008 Rule-Based Cooperative Control of Augmentation Steering System for Aircraft tional-Integral Controllers for Rigid-Body Atti- Optically Linked Model Spacecraft: Experimen- Ground Handling tude Stabilization tal Study J. GUIDANCE, VOL. 27, NO. 6: 2004 INDEX G04-116 Test Results for Entry Guidance Meth- G04-113 Generation of Launch Vehicle Abort Spacecraft Guidance and Control ods for Space Vehicles Trajectories Using a Hybrid Optimization G04-076 Robust Tracking Control Design for G04-048 Augmenting Adaptive Approach to Method Spacecraft Under Control Input Saturation Control of Flexible Systems G04-121 Efficient Minimax Control Design for G04-009 Toward a Stellar Gyroscope for Space- G04-093 Neural-Network-Based Design of Prescribed Parameter Uncertainty craft Attitude Determination Optimal Controllers for Nonlinear Systems G04-128 Genetic Algorithm Preprocessing for G04-027 Precise Cassini Navigation During G04-053 Adaptive Neural Network Inverse Con- Numerical Solution of Differential Games Prob- Solar Conjunctions Through Multifrequency troller for General Aviation Safety lems Plasma Calibrations G04-106 Periodic H2 Synthesis for Spacecraft Launch Vehicle Guidance and Control Attitude Control with Magnetorquers G04-007 Decentralized Scheme for Spacecraft Formation Flying via the Virtual Structure G04-116 Test Results for Entry Guidance Meth- G04-123 Dynamic Control Allocation Using Approach ods for Space Vehicles Constrained Quadratic Programming G04-047 Singularity Analysis of Variable Speed G04-114_ New Nonlinear Control Technique for G04-122 Nonlinear Control Allocation Using Control Moment Gyros Ascent Phase of Reusable Launch Vehicles Piecewise Linear Functions G04-052 State-Space Approach to Computing G04-117 Unpowered Approach and Landing G04-109 Method for Determination of Nonlin- Spacecraft Pointing Jitter Guidance Using Trajectory Planning ear Attainable Moment Sets G04-010 Interspacecraft Optical Communica- G04-113 Generation of Launch Vehicle Abort G04-049 Pseudospectral Knotting Methods for tion and Navigation Using Modulating Retrore- Trajectories Using a Hybrid Optimization Solving Nonsmooth Optimal Control Problems flectors Method G04-032 Jacobi Pseudospectral Method for G04-106 Periodic H2 Synthesis for Spacecraft G04-112 Methods for Compensating for Control Solving Optimal Control Problems Attitude Control with Magnetorquers Allocator and Actuator Interactions Pointing Systems G04-025 Nonlinear Control of Librational G04-118 Integrated Adaptive Guidance and Motion of Tethered Satellites in Elliptic Orbits Control for Re-Entry Vehicles with Flight Test G04-052 State-Space Approach to Computing G04-132 Differentiator-Free Nonlinear Propor- Results Spacecraft Pointing Jitter tional-Integral Controllers for Rigid-Body Atti- Missile Dynamics G04-008 Rule-Based Cooperative Control of tude Stabilization Optically Linked Model Spacecraft: Experimen- G04-115 Dynamic Lateral Entry Guidance G04-012 Integrated Guidance and Control of tal Study Logic Moving-Mass Actuated Kinetic Warheads Redundancy Management G04-037 Application of Pseudospectral Meth- G04-108 Linear Theory of a Rotating Internal ods for Receding Horizon Control Part Projectile Configuration in Atmospheric G04-109 Method for Determination of Nonlin- G04-060 Second-Order Equations for Ren- Flight ear Attainable Moment Sets dezvous in a Circular Orbit G04-030 Miss Distance Error Analysis of Exoat- G04-122 Nonlinear Control Allocation Using G04-044 Nanosatellite Attitude Stabilization mospheric Interceptors Piecewise Linear Functions Using Passive Aerodynamics and Active Mag- G04-123 Dynamic Control Allocation Using netic Torquing Missile Guidance and Control Constrained Quadratic Programming G04-093 Neural-Network-Based Design of G04-030 Miss Distance Error Analysis of Exoat- G04-029 Singularity Analysis and Visualization Optimal Controllers for Nonlinear Systems mospheric Interceptors for Single-Gimbal Control Moment Gyro Sys- G04-051 Optimal-REQUEST Algorithm G04-022 Boost-Phase Identification of Theater tems Attitude Determination Ballistic Missiles Using Radar Measurements Robotics State Estimation G04-111 Modern Explicit Guidance Law for High-Order Dynamics G04-063 Vehicle Motion Planning with Time- G04-051 Optimal-REQUEST Algorithm for G04-133 Lyapunov-Based Nonlinear Missile Varying Constraints Attitude Determination Guidance G04-011 Robust Vibration Suppression in Flexi- G04-054 Optimal State Estimation With Failed G04-050 Nonlinear Missile Autopilot Design ble Systems Using Infinite Impulse Response Sensor Discrimination and Identification with Theta-D Technique Digital Filters G04-022 Boost-Phase Identification of Theater G04-119 Lambert Guidance Routine Designed Ballistic Missiles Using Radar Measurements Signal Processing To Match Position And Velocity of A Ballistic G04-064 Extended Kalman Filtering for Satel- Target G04-129 Circular Navigation Missile Guidance lite Orbital Attitude Estimation Based on Gibbs G04-129 Circular Navigation Missile Guidance with Incomplete Information and Uncertain Vector with Incomplete Information and Uncertain Autopilot Model G04-058 Simple Structure for a High Perfor- Autopilot Model G04-051 Optimal-REQUEST Algorithm for mance Three-Dimensional Tracking Filter G04-012 Integrated Guidance and Control of Attitude Determination G04-014 Nonlinear Recursive Minimum Model Moving-Mass Actuated Kinetic Warheads G04-054 Optimal State Estimation With Failed Error Estimation G04-130 Optimal Dual-Rate Digital Redesign Sensor Discrimination and Identification G04-026 Global Magnetometer-Based Space- with Application to Missile Control craft Attitude and Rate Estimation G04-134 Trajectory Shaping in Linear Quadratic Spacecraft Dynamics G04-038 Square Root Sigma Point Filtering for Pursuit-Evasion Games G04-105 Integrated Power and Attitude Control Real-Time, Nonlinear Estimation Navigation with Spacecraft Flywheels and Control Moment Structural Control Gyroscopes G04-086 Guidance of Unmanned Air Vehicles G04-044 Nanosatellite Attitude Stabilization G04-011 Robust Vibration Suppression in Flexi- Based on Fuzzy Sets and Fixed Waypoints Using Passive Aerodynamics and Active Mag- ble Systems Using Infinite Impulse Response G04-027 Precise Cassini Navigation During netic Torquing Digital Filters Solar Conjunctions Through Multifrequency G04-132 Differentiator-Free Nonlinear Propor- G04-048 Augmenting Adaptive Approach to Plasma Calibrations tional-Integral Controllers for Rigid-Body Atti- Control of Flexible Systems G04-030 Miss Distance Error Analysis of Exoat- tude Stabilization G04-101 Time Simulations of the Response of mospheric Interceptors G04-029 Singularity Analysis and Visualization Maneuvering Flexible Aircraft G04-064 Extended Kalman Filtering for Satel- for Single-Gimbal Control Moment Gyro Sys- System Identification lite Orbital Attitude Estimation Based on Gibbs tems Vector G04-047 Singularity Analysis of Variable Speed G04-022 Boost-Phase Identification of Theater Control Moment Gyros Ballistic Missiles Using Radar Measurements Optimization Techniques G04-026 Global Magnetometer-Based Space- G04-014 Nonlinear Recursive Minimum Model G04-075 Simulated Annealing for Missile Opti- craft Attitude and Rate Estimation Error Estimation mization: Developing Method and Formulation G04-104 Control of a Rotating Variable-Length G04-061 Sequential Computation of Total Least- Techniques Tethered System Squares Parameter Estimates 1112 J. GUIDANCE, VOL. 27, NO. 6: 2004 INDEX Trajectory Optimization Atmospheric and Space Sciences G04-124 Transit-Orbit Search for Planar Restricted Three-Body Problems with Perturba- G04-063 Vehicle Motion Planning with Time- G04-055 Aircraft Autopilot Analysis and Enve- tions Varying Constraints lope Protection for Operation Under Icing Con- G04-125 Low Thrust Minimum-Fuel Orbital G04-032 Jacobi Pseudospectral Method for ditions Transfer: A Homotopic Approach Solving Optimal Control Problems Multidisciplinary Design Optimization G04-062 Optimal Interplanetary Trajectories G04-118 Integrated Adaptive Guidance and Using Constant Radial Thrust and Gravitational Control for Re-Entry Vehicles with Flight Test G04-033 Interferometric Observatories in Earth Assists Results Orbit G04-118 Integrated Adaptive Guidance and G04-135 Earth Escape by Ideal Sail and Solar- G04-075 Simulated Annealing for Missile Opti- Control for Re-Entry Vehicles with Flight Test Photon Thrustor Spacecraft mization: Developing Method and Formulation Results G04-120 Trajectory Planning for Autonomous Techniques G04-135 Earth Escape by Ideal Sail and Solar- Aerospace Vehicles amid Known Obstacles and Conflicts Safety Photon Thrustor Spacecraft G04-033 Interferometric Observatories in Earth G04-042 Systematic Method for Constructing G04-055 Aircraft Autopilot Analysis and Enve- Orbit Earth-Mars Cyclers Using Free-Return Trajecto- lope Protection for Operation Under Icing Con- G04-059 Mars and Mercury Missions Using ries ditions Solar Sails and Solar Electric Propulsion G04-006 Optimization of Interplanetary Solar Sailcraft Trajectories Using Evolutionary Neuro- Sensor Systems Space Systems control G04-054 Optimal State Estimation With Failed G04-128 Genetic Algorithm Preprocessing for G04-107 Libration Control of Flexible Tethers Sensor Discrimination and Identification Numerical Solution of Differential Games Prob- Using Electromagnetic Forces and Movable lems Attachment G04-125 Low Thrust Minimum-Fuel Orbital LAUNCH VEHICLE AND MIS- G04-062 Optimal Interplanetary Trajectories Transfer: A Homotopic Approach SILE (LV/M) TECHNOLOGY Using Constant Radial Thrust and Gravitational G04-111 Modern Explicit Guidance Law for Assists High-Order Dynamics Missile Systems G04-034 New, Fast Numerical Method for Solv- Spacecraft Attitude Determination G04-050 Nonlinear Missile Autopilot Design ing Two-Point Boundary-Value Problems with Theta-D Technique G04-026 Global Magnetometer-Based Space- G04-037 Application of Pseudospectral Meth- ods for Receding Horizon Control G04-012 Integrated Guidance and Control of craft Attitude and Rate Estimation Moving-Mass Actuated Kinetic Warheads G04-064 Extended Kalman Filtering for Satel- G04-059 Mars and Mercury Missions Using lite Orbital Attitude Estimation Based on Gibbs Solar Sails and Solar Electric Propulsion Simulation Vector G04-113 Generation of Launch Vehicle Abort G04-119 Lambert Guidance Routine Designed Trajectories Using a Hybrid Optimization To Match Position And Velocity of A Ballistic Spacecraft Communication Method Target G04-110 Singular Perturbation Analysis of Opti- G04-027 Precise Cassini Navigation During mal Glide Trajectories and Tracking Systems Solar Conjunctions Through Multifrequency G04-075 Simulated Annealing for Missile Opti- Plasma Calibrations mization: Developing Method and Formulation G04-058 Simple Structure for a High Perfor- G04-010 Interspacecraft Optical Communica- Techniques mance Three-Dimensional Tracking Filter tion and Navigation Using Modulating Retrore- G04-119 Lambert Guidance Routine Designed flectors To Match Position And Velocity of A Ballistic SPACE TECHNOLOGY Target Aerobraking Flight Mechanics Spacecraft Sensor Systems UAVs G04-115 Dynamic Lateral Entry Guidance G04-009 Toward a Stellar Gyroscope for Space- G04-094 Human-Inspired Control Logic for Logic craft Attitude Determination Automated Maneuvering of Miniature Heli- copter Mission Design and Analysis G04-028 Dynamics and Stability of an Autoro- STRUCTURAL MECHANICS G04-033 Interferometric Observatories in Earth tating Rotor/Wing Unmanned Aircraft Orbit AND MATERIALS G04-086 Guidance of Unmanned Air Vehicles G04-062 Optimal Interplanetary Trajectories Based on Fuzzy Sets and Fixed Waypoints Aeroelasticity and Control Using Constant Radial Thrust and Gravitational G04-120 Traiectory Planning for Autonomous Assists G04-004 Control of a Nonlinear Wing Section Aerospace Vehicles amid Known Obstacles and Conflicts G04-124 Transit-Orbit Search for Planar Using Leading- and Trailing-Edge Surfaces Restricted Three-Body Problems with Perturba- G04-089 Limit Cycles and Domain of Stability tions in Unsteady Aeroelastic System INTERDISCIPLINARY TOPICS G04-042 Systematic Method for Constructing Earth-Mars Cyclers Using Free-Return Trajecto- Analytical and Numerical Methods ries Flexible and Active Structures G04-018 Nonlinear Modelling of Spacecraft G04-074 Tuning of Observer-Based Controllers Mission Trajectories (Earth and Relative Motion in the Configuration Space G04-015 Nonlinear Adaptive Control for Slew- Interplanetary) G04-061 Sequential Computation of Total Least- ing Flexible Active Structures Squares Parameter Estimates G04-042 Systematic Method for Constructing G04-107 Libration Control of Flexible Tethers G04-031 First-Order Analytical Solution for Earth-Mars Cyclers Using Free-Return Trajecto- Using Electromagnetic Forces and Movable Spacecraft Motion About (433) Eros ries Attachment J. GUIDANCE. VOL. 27, NO. 6: 2004 INDEX Author Index Abad, Alberto, G04-031 Fahroo, Fariba, G04-049 Li, Sai-Ming, G04-076 Santono, Fabio, G04-046 Agrawal, Brij N., G04-065 Feron, E., G04-094 Liu, Pengxiang, G04-127 Satoh, Atsushi, G04-016 Akella, Maruthi R., G04-132 Feron, Eric, G04-056 Lopez, C. A., G04-028 Savkin, Andrey V., G04-129 Alazard, D., G04-074 Ferrari, Silvia, G04-097 Lorenzini, Enrico C., G04-126 Sayegh, E. G., G04-008 Almogi-Nadler, Meirav, G04-022 Fravolini, M. L., G04-036 Lu, Ping, G04-115 Schaub, Hanspeter, G04-103 Amato, Francesco, G04-057 Frazzoli, Emilio, G04-055 Lutze, Frederick H., G04-060 Scheeres, Daniel J., G04-031 Ananthkrishnan, N., G04-035 Frost, Geoffrey, G04-108 Mahon, Rita, G04-010 Scheeres, D. J., G04-033, G04-083 Anderson, Kurt, G04-090 Fujii, Hironori A., G04-025, G04-107 Malyevac, D. S., G04-012 Scherock, Jeff J., G04-119 Antoniadis, I., G04-011 Gandhi, Neha, G04-118 Manchester, Ian R., G04-129 Schierman, John D., G04-118 Arad, David, G04-073 Gavrilets, V., G04-094 Mannchen, Thomas, G04-095 Schmidt, David K., G04-001 Avanzini, Giulio, G04-013 Gergaud, Joseph, G04-125 Marcos, Andrés, G04-024 Schumacher Jr., Paul W., G04-020 Azuma, Akira, G04-068, G04-069 Ge, Zhiqiang, G04-014 Martinon, Pierre, G04-125 Shah, Parikshit M., G04-035 Bajodah, Abdulrahman, G04-131 Gilbreath, G. Charmaine, G04-010 Marullo, Antonio, G04-087 Shapira, Ilana, G04-110 Balakrishnan, S. N., G04-050, G04-114 Giulietti, Fabrizio, G04-088 Marzocca, Piergiovanni, G04-099 Sharma, Vikrant, G04-055 Balas, Gary J., G04-024, G04-096 Glover, Robert A., G04-020 Mason, David H., G04-001 Shen, Zuojun, G04-115 Bar-Itzhack, I. Y., G04-051 Goetz, Peter G., G04-010 Mason, William J., G04-062 Shinar, Josef, G04-134 Bayard, David S., G04-052 Goman, M. G., G04-078 Masuko, Yoichiro, G04-043 Shin, Jong-Yeob, G04-098 Beard, Randal, G04-007 Gopal, Vipin, G04-072 Mavroidis, C., G04-011 Singh, Sahjendra N., G04-089 Belcastro, Christine, G04-098 Go, Tiauw Hiong, G04-079 McRuer, Duane, G04-019 Singh, Tarunraj, G04-121 Ben-Asher, Joseph Z., G04-022, Graham, Dunstan, G04-019 Meehan, Timothy J., G04-010 Soijer, Marco W., G04-061 G04-110, G04-134 Gromov, Konstantin, G04-009 Mehra, Raman K., G04-023, Spencer, David, G04-124 Beppu, Goro, G04-068, G04-069 Guibout, V. M., G04-083 G04-076 Speyer, Jason L., G04-017, G04-021 Bhat, M. Seetharama, G04-077 Gujjula, Sushma, G04-089 Meirovitch, Leonard, G04-101 Stansbery, Donald T., G04-050 Bhattacharya, Raktim, G04-096 Gurfil, Pini, G04-018 Meller, David Matthew, G04-009 Starr, G. P., G04-015 Biegler, Lorenz T., G04-072 Haberkorn, Thomas, G04-125 Mengali, Giovanni, G04-088, Steck, James E., G04-053 Bilimoria, K. D., G04-092 Hablani, Hari B., G04-030 G04-135 Stengel, Robert F., G04-097 Bingol, Muge, G04-075 Hadaegh, F. Y., G04-008 Menon, P. K., G04-012, G04-092 Stoustrup, Jakob, G04-106 Blanksby, Chris, G04-025, G04-107 Hall, Christopher D., G04-104 Mettler, Bernard, G04-056, G04-094 Strganac, Thomas W., G04-004 Bolender, Michael A., G04-109, Hamaiainen, Raimo P., G04-080 Mirmirani, Maj. D., G04-102 Subbarao, Kamesh, G04-132 G04-122 Hanson, John M., G04-116 Mishne, David, G04-082 Subramanian, Dharmashankar, G04-072 Bombardelli, Claudio, G04-126 Harkegard, Ola, G04-123 Mita, Tsutomu, G04-043 Sugimoto, Kenji, G04-016 Bordi, J. J., G04-027 Hexner, G., G04-058 Mitchell, David G., G04-001, G04-100 Sweriduk, G. D., G04-012, G04-092 Bose, David M., G04-105 Hodges, Dewey H., G04-131 Moorhouse, David J., G04-001 Tekinalp, Ozan, G04-075 Boskovic, Jovan D., G04-023, G04-076 Holsapple, Raymond W., G04-034 Mosca, Edoardo, G04-084 Tenne, Dirk, G04-121 Brandt, Nico, G04-113 Hoots, Felix R., G04-020 Napolitano, M. R., G04-036 Thornblom, Mark N., G04-054 Bruner, Hugh Samuel, G04-053 Horie, Kazuhiro, G04-128 Ocampo, Cesar A., G04-042 Tortora, P., G04-027 Brunke, Shelby, G04-038 Hori, Noriyuki, G04-130 Ohlmeyer, E. J., G04-012 Tortora, Paolo, G04-046 Bullo, Francesco, G04-063 Hovakimyan, Naira, G04-085 Ohlmeyer, Ernest J., G04-050 Trask, Aaron J., G04-062 Burns, Steven P., G04-119 Huang, Peikang, G04-014 Oppenheimer, Michael, G04-118 Trivailo, Pavel, G04-025, G04-107 Calise, Anthony J., G04-048, G04-085, Hull, Jason R., G04-118 Oppenheimer, Michael W., G04-112 Tsiotras, Panagiotis, G04-047 G04-113 Hussein, I. I., G04-033 Oshman, Y., G04-051 Turra, Demetrio, G04-086 Cameron, Jonathan M., G04-070 Hyland, D. C., G04-033 Oshman, Yaakov, G04-022, G04-046, Tuzcu, Ilhan, G04-101 Campa, G., G04-036 lamratanakul, Dhanakorn, G04-071 G04-073 Unnikrishnan, Suraj, G04-035 Campbell, Mark, G04-038 Idan, Moshe, G04-085 Parker, G. G., G04-015 Vasquez, John A., G04-010 Casalino, Lorenzo, G04-081 lervolino, Raffaele, G04-057 Pearson, David W., G04-030 Venkataraman, Ram, G04-034 Casavola, Alessandro, G04-084 less, L., G04-027 Peck, M., G04-091 Vilcheck, Michael J., G04-010 Cerven, W. Todd, G04-063 Innocenti, Mario, G04-086, G04-087 Perez, Hector, G04-071 Virtanen, Kai, G04-080 Chen, Lingji, G04-023 Ioannou, Petros A., G04-102 Perhinschi, M., G04-036 Voulgaris, Petros G., G04-055 Chen, Robert H., G04-017, G04-021 Ishikawa, Hiroaki, G04-068, G04-069 Perng, Jau-Woei, G04-005 Wang, P. K. C., G04-008 Chen, Ye-Hwa, G04-131 Iwasaki, Masatake, G04-025 Pesonen, Urpo J., G04-053 Ward, David G., G04-118 Chiappa, C., G04-074 Jalali-Naini, S. H., G04-111 Phan, Minh Q., G04-093 Watanabe, Takeo, G04-107 Choukroun, D., G04-051 Jones, Robert E., G04-116 Platanitis, George, G04-004 Weil, Klaus H., G04-095 Circi, Christian, G04-059 Kalandros, Michael, G04-041, Polites, Michael E., G04-054 Weiss, H., G04-058 Cochran, John E., G04-045 G04-034, G04-090 Pollini, Lorenzo, G04-086, G04-087 Weiss, Haim, G04-134 Colasurdo, Guido, G04-081 Kaminer, Isaac I., G04-002 Powly, A. A., G04-077 Wells, V. L., G04-028 Conway, Bruce A., G04-128 Kang, Ja- Young, G04-045 Psiaki, Mark L., G04-026, G04-044 Wie, Bong, G04-029, G04-066, Costello, Mark, G04-108 Karlgaard, Christopher D., G04-060, Quadrelli, Marco B., G04-070, G04-067 Coverstone, Victoria L., G04-062, G04-105 G04-126 Williams, Paul, G04-032, G04-037, G04-063 Kasdin, N. Jeremy, G04-018 Quarta, Alessandro A., G04-135 G04-107 Craig, James I., G04-048 Kerzhanovich, Viktor, G04-070 Rabbath, C. A., G04-130, G04-133 Wilson, D. G., G04-015 Creamer, N. Glenn, G04-010 Key, David L., G04-001 Rabinovich, William S., G04-010 Wisniewski, Rafal, G04-106 Cumer, C., G04-074 Kim, Mischa, G04-104 Raghunathan, Arvind U., G04-072 Witzberger, Kevin E., G04-054 Dachwald, Bernd, G04-006 Kluever, Craig A., G04-117 Raivio, Tuomas, G04-080 Wu, Bing-Fei, G04-005 Dellicker, Scott H., G04-002 Klyde, David H., G04-001, G04-003, Ramnath, Rudrapatna V., G04-079 Wu, N. Eva, G04-098 Delmond, F., G04-074 G04-100 Raney, David L., G04-001 Xin, Ming, G04-050, G04-114 Demenkov, M. N., G04-078 Kojima, Hirohisa, G04-025 Rao, Vittal $., G04-127 Xu, Haojian, G04-102 Deng, ZhengLong, G04-064 Kokolios, Alexander, G04-003 Reinsberg, James G., G04-003 Yakimenko, Oleg A., G04-002 Devasia, Santosh, G04-071 Kulkarni, Nilesh V., G04-093 Ren, Wei, G04-007 Yamato, Hideaki, G04-124 Dever, Chris, G04-056 Kumar, Renjith R., G04-105 Robinett, R. D., G04-015 Yang, Bong-Jun, G04-048 Dobrokhodov, Vladimir N., G04-002 Lane, Christopher M., G04-054 Roithmayr, Carlos M., G04-105 Yang, Erfu, G04-043 Doman, David, G04-034 Lara, Martin, G04-031 Rokhsaz, Kamran, G04-053 Yang, Hong, G04-120 Doman, David B., G04-001, G04-109, Lechevin, N., G04-133 Romano, Marcello, G04-065 Yasuda, Kunio, G04-068, G04-069 G04-112, G04-118, G04-122 Lechevin, Nicolas, G04-130 Ross, I. Michael, G04-049 Yee, J., G04-008 Douglas, Randal K., G04-017 Leggett, David B., G04-001 Roth, D. C., G04-027 Yim, Wooson, G04-089 Drake, David, G04-114 Levinson, Sergei, G04-134 Russell, Ryan P., G04-042 Yoon, Hyungjoo, G04-047 Duerksen, Noel, G04-053 Librescu, Liviu, G04-099 Samad, Tariq, G04-072 Yuan, Yuan, G04-099 Economou, D., G04-011 Liebe, Carl Christian, G04-009 San-Juan, Juan F., G04-031 Yu, Pei, G04-099 Ekelund, J. E., G04-027 Lin, YuRong, G04-064 Sanders, Erica, G04-003 Zhao, Yiyuan, G04-120 J. GUIDANCE, VOL. 27, NO. 6: 2004 INDEX Chronological Index G98-002 Erratum for “Strapdown Inertial Navigation G04-011 Robust Vibration Suppression in Flexible Systems Integration Algorithm Design Part 2: Velocity and Position Using Infinite Impulse Response Digital Filters. D. Economou, Algorithms” by Paul G. Savage (27, 2, p. 318) Erratum National Technical University of Athens, Greece; C. Mavroidis, Rutgers University; and I. Antoniadis, National Technical G03-076 Erratum for “Using Fractional Gaussian Noise University of Athens, Greece (27, 1, p. 107) Article Models in Orbit Determination” by Winston C. Chow and Paul W. Schumacher, Jr. (27, 2, p. 319) Erratum G04-012 Integrated Guidance and Control of Moving-Mass Actuated Kinetic Warheads. P. K. Menon and G. D. Sweriduk, G04-001 Evolution, Revolution, and Challenges of Handling Optimal Synthesis Inc.; E. J. Ohlmeyer and D. S. Malyevac, Naval Qualities. David G. Mitchell, Hoh Aeronautics, Inc.; David B. Surface Warfare Center (27, |, p. 118) Article Doman, U.S. Air Force; David L. Key, Key Qualities; David H. Klyde, Systems Technology, Inc.; David B. Leggett and David J. G04-013 Frenet-Based Algorithm for Trajectory Prediction. Moorhouse, U.S. Air Force; David H. Mason, The Boeing Giulio Avanzini, Polytechnic of Turin, Italy (27, 1, p. 127) Article Company; David L. Raney, NASA Langley Research Center; and David K. Schmidt, University of Colorado (27, 1, p. 12) History of G04-014 Nonlinear Recursive Minimum Model Error Key Technologies based on AIAA Paper 2003-5465 Estimation. Zhigiang Ge, Beijing Institute of Remote Sensing and Equipment, China (prc); and Peikang Huang, National G04-002 Synthesis of Optimal Control and Flight Testing of an Electromagnetic Scattering Laboratory, China (PRC) (27, 1, Autonomous Circular Parachute. Oleg A. Yakimenko, Vladimir p. 136) Article N. Dobrokhodoy, and Isaac I. Kaminer, Naval Postgraduate School; and Scott H. Dellicker, U.S. Army Yuma Proving Ground (27, 1, G04-015 Nonlinear Adaptive Control for Slewing Flexible p. 29) Article Active Structures. D. G. Wilson, Sandia National Laboratories; G. P. Starr, University of New Mexico; G. G. Parker, Michigan G04-003 Flight-Test Evaluation of Stability Augmentation Technological University; and R. D. Robinett, Sandia National Steering System for Aircraft Ground Handling. David H. Klyde, Laboratories (27, 1, p. 142) Technical Note Systems Technology, Inc.; James G. Reinsberg, The Boeing Company; Erica Sanders and Alexander Kokolios, Naval Air G04-016 Partial Eigenstructure Assignment Approach for Systems Command (27, 1, p. 41) Article based on AIAA Paper Robust Flight Control. Atsushi Satoh and Kenji Sugimoto, Nara 2003-5318 Institute of Science and Technology, Japan (27, 1, p. 145) Technical Note G04-004 Control of a Nonlinear Wing Section Using Leading- and Trailing-Edge Surfaces. George Platanitis and Thomas W. G04-017 Linear System Input-Order Reduction by Hankel Strganac, Texas A&M University (27, 1, p. 52) Article Norm Maximization. Randal K. Douglas, The Aerospace Corporation; Robert H. Chen, The University of California; and G04-005 Gain-Phase Margin Analysis of Pilot-Induced Jason L. Speyer, The University of California, Los Angeles (27, 1, Oscillations for Limit-Cycle Prediction. Bing-Fei Wu and Jau- p. 150) Technical Note Woei Perng, National Chiao Tung University, Taiwan (ROC) (27, 1, p. 59) Article G04-018 Nonlinear Modelling of Spacecraft Relative Motion in the Configuration Space. Pini Gurfil and N. Jeremy Kasdin, G04-006 Optimization of Interplanetary Solar Sailcraft Princeton University (27, 1, p. 154) Technical Note Trajectories Using Evolutionary Neurocontrol. Bernd Dachwald, DLR, German Aerospace Center, Germany (27, |, p. 66) G04-019 Flight Control Century: Triumphs of the Systems Article Approach. Duane McRuer and Dunstan Graham, Systems Techology, Inc. (27, 2, p. 161) History of Key Technologies G04-007 Decentralized Scheme for Spacecraft Formation Flying via the Virtual Structure Approach. Wei Ren and Randal G04-020 History of Analytical Orbit Modeling in the U.S. Beard, Brigham Young University (27, |, p. 73) Article Space Surveillance System. Felix R. Hoots, AT&T; Paul W. Schumacher Jr., Naval Network and Space Operations Command; G04-008 Rule-Based Cooperative Control of Optically Linked and Robert A. Glover, AT&T (27, 2, p. 174) Article Model Spacecraft: Experimental Study. P. K. C. Wang, J. Yee, and E. G. Sayegh, University of California, Los Angeles; and F. Y. G04-021 Sensor and Actuator Fault Reconstruction. Robert H. Hadaegh, Jet Propulsion Laboratory (27, 1, p. 83) Article Chen and Jason L. Speyer, University of California, Los Angeles (27, 2, p. 186) Article G04-009 Toward a Stellar Gyroscope for Spacecraft Attitude Determination. Carl C. Liebe, Konstantin Gromov, and David M. G04-022 Boost-Phase Identification of Theater Ballistic Meller, Jet Propulsion Laboratory (27, 1, p. 91) Article Missiles Using Radar Measurements. Meirav Almogi-Nadler, Yaakov Oshman, and Joseph Z. Ben-Asher, Technionfilsrael G04-010 Interspacecraft Optical Communication and Institute of Technology, Israel (27, 2, p. 197) Article Navigation Using Modulating Retroreflectors. N. G. Creamer, G. C. Gilbreath, Timothy J. Meehan, Michael J. Vilcheck, John A. G04-023 Adaptive Control Design for Nonaffine Models Vasquez, William S. Rabinovich, and Peter G. Goetz, U.S. Naval Arising in Flight Control. Jovan D. Boskovic, Lingji Chen, and Research Laboratory; and Rita Mahon, Jaycor Inc., (27, 1, p. 100) Raman K. Mehra, Scientific Systems Company, Inc. (27, 2, p. 209) Article Article J. GUIDANCE, VOL. 27, NO. 6: 2004 INDEX 1115 G04-024 Development of Linear-Parameter-Varying Models G04-038 Square Root Sigma Point Filtering for Real-Time, for Aircraft. Andrés Marcos and Gary J. Balas, University of Nonlinear Estimation. Shelby Brunke, University of Washington: Minnesota (27, 2, p. 218) Article and Mark Campbell, Cornell University (27, 2, p. 314) Technical Note G04-025 Nonlinear Control of Librational Motion of Tethered Satellites in Elliptic Orbits. Hirohisa Kojima, Masatake Iwasaki, G04-039 Covariance Control for Sensor Management in and Hironori A. Fujii, Tokyo Metropolitan Institute of Technology, Cluttered Tracking Environments. Michael Kalandros and Lucy Japan; Chris Blanksby and Pavel Trivailo, Royal Melbourne Y. Pao, University of Colorado (27, 3, p. 493 ) Technical Note Institute of Technology, Australia (27, 2, p. 229) Article G04-040 Systematic Method for Constructing Earth-Mars G04-026 Global Magnetometer-Based Spacecraft Attitude and Cyclers Using Free-Return Trajectories. Ryan P. Russell and Rate Estimation. Mark L. Psiaki, Cornell University (27, 2, p. 240) Cesar A. Ocampo, University of Texas at Austin (27, 3, p. 321) Article Article based on AIAA Paper 03-145 G04-027 Precise Cassini Navigation During Solar G04-041 Dual Controller Approach to Three-Dimensional Conjunctions Through Multifrequency Plasma Calibrations. P. Autonomous Formation Control. Erfu Yang, Tokyo Institute of Tortora, University of Bologna, Italy; L. less, University of Rome, Technology, Japan; Yoichiro Masuko, Mitsubishi Heavy Industries, Italy; J. J. Bordi, J. E. Ekelund, and D. C. Roth, Jet Propulsion Ltd., Japan; and Tsutomu Mita, Tokyo Institute of Technology, Laboratory, California Institute of Technology (27, 2, p. 251) Japan (27, 3, p. 336) Article Article based on AIAA Paper 03-200 G04-042 Nanosatellite Attitude Stabilization Using Passive G04-028 Dynamics and Stability of an Autorotating Aerodynamics and Active Magnetic Torquing. Mark L. Psiaki, Rotor/Wing Unmanned Aircraft. C. A. Lopez and V. L. Wells, Cornell University (27, 3, p. 347) Article Arizona State University (27, 2, p. 258) Article G04-043 Resonant Motion of a Spin-Stabilized Thrusting G04-029 Singularity Analysis and Visualization for Single- Spacecraft. Ja- Young Kang, Hankuk Aviation University; and John Gimbal Control Moment Gyro Systems. Bong Wie, Arizona E. Cochran, Auburn University (27, 3, p. 356) Article State University (27, 2, p. 271) Article G04-044 Spacecraft Angular Rate Estimation from G04-030 Miss Distance Error Analysis of Exoatmospheric Magnetometer Data Only Using an Analytic Predictor. Paolo Interceptors. Hari B. Hablani and David W. Pearson, The Boeing Tortora, University of Bologna; Yaakov Oshman, Technion—Israel Company (27, 2, p. 283) Article Institute of Technology; and Fabio Santono, University of Rome (27, 3, p. 365) Article G04-031 First-Order Analytical Solution for Spacecraft Motion About (433) Eros. Juan F. San-Juan, Universidad de la G04-045 Singularity Analysis of Variable Speed Control Rioja, Spain; Alberto Abad, Universidad de Zaragoza, Spain; Moment Gyros. Hyungjoo Yoon and Panagiotis Tsiotras, Georgia Martin Lara, Real Observatorio de la Armada, Spain; and Daniel J. Institute of Technology (27, 3, p. 374) Article Scheeres, The University of Michigan (27, 2, p. 290) Article G04-046 Augmenting Adaptive Approach to Control of Flexible G04-032 Jacobi Pseudospectral Method for Solving Optimal Systems. Anthony J. Calise, Bong-Jun Yang, and James I. Craig, Control Problems. Paul Williams, Royal Melbourne Institute of Georgia Institute of Technology (27, 3, p. 387) Article Technology, Australia (27, 2, p. 293) Technical Note G04-047 Pseudospectral Knotting Methods for Solving G04-033 Interferometric Observatories in Earth Orbit. |. I. Nonsmooth Optimal Control Problems. I. M. Ross and Fariba Hussein, D. J. Scheeres, and D. C. Hyland, University of Michigan Fahroo, Naval Postgraduate School (27, 3, p. 397) Article (27, 2, p. 297) Technical Note G04-048 Nonlinear Missile Autopilot Design with Theta-D G04-034 New, Fast Numerical Method for Solving Two-Point Technique. Ming Xin and S. N. Balakrishnan, University of Boundary-Value Problems. Raymond W. Holsapple and Ram Missouri—Rolla; Donald T. Stansbery, Boeing Company; and Ernest Venkataraman, Texas Tech University; David Doman, US AFRL J. Ohlmeyer, Naval Surface Weapon Center (27, 3, p. 406) (27, 2, p. 301) Technical Note Article G04-035 Approximate Analytical Criterion for Aircraft Wing G04-049 Optimal-REQUEST Algorithm for Attitude Rock Onset. N. Ananthkrishnan, Parikshit M. Shah, and Suraj Determination. D. Choukroun, I. Y. Bar-Itzhack, and Y. Oshman, Unnikrishnan, Indian Institute of Technology Bombay, India (27, 2, Technion—Israel Institute of Technology (27, 3, p. 418) Article p. 304) Technical Note based on AIAA Paper 2003-5304 G04-050 State-Space Approach to Computing Spacecraft G04-036 Learning-Based Sensor Validation Scheme Within Pointing Jitter. David S. Bayard, Jet Propulsion Laboratory (27, 3, Flight Control Laws. M. L. Fravolini, Perugia University, Italy; p. 426) Article based on AIAA Paper 2003-5782 G. Campa, M. R. Napolitano, and M. Perhinschi, West Virginia University (27, 2, p. 307) Article G04-051 Adaptive Neural Network Inverse Controller for General Aviation Safety. Urpo J. Pesonen, James E. Steck, and G04-037 Application of Pseudospectral Methods for Receding Kamran Rokhsaz, Wichita State University, Hugh S. Bruner and Horizon Control. Paul Williams, Royal Melbourne Institute of Noel Duerksen, Raytheon Aircraft Company (27, 3, p. 434) Article Technology, Australia (27, 2, p. 310) Technical Note based on AIAA Paper 2003-578 1116 J. GUIDANCE, VOL. 27, NO. 6: 2004 INDEX 704-052 Optimai State Estimation With Failed Sensor G04-066 Flight Dynamics of the Boomerang, Part 1: Discrimination and Identification. Michael E. Polites, Kevin E. Fundamental Analysis. Akira Azuma, University of Tokyo, Japan; Witzberger, Christopher M. Lane, and Mark N. Thornblom, Goro Beppu and Hiroaki Ishikawa, Tokai University, Japan; and University of Alabama (27, 3, p. 444) Article Kunio Yasuda, Nihon University, Japan (27, 4, p. 545) Article G04-053 Aircraft Autopilot Analysis and Envelope Protection G04-067 Flight Dynamics of the Boomerang, Part Two: Effects for Operation Under Icing Conditions. Vikrant Sharma, Petros of Initial Condition and Geometrical Configuration. Goro G. Voulgaris, and Emilio Frazzoli, Coordinated Science Lab, Beppu and Hiroaki Ishikawa, Tokai University, Japan; Akira University of Illinois at Urbana-Champaign (27, 3, p. 454) Article Azuma, University of Tokyo, Japan; and Kunio Yasuda, Nihon University, Japan (27, 4, p. 555) Article G04-054 Scaling Effects and Dynamic Characteristics of Miniature Rotorcraft. Bernard Mettler, Chris Dever, and Eric G04-068 Multibody Dynamics of Parachute and Balloon Flight Feron, Massachusetts Institute of Technology (27, 3, p. 466) Article Systems for Planetary Exploration. Marco B. Quadrelli, Jonathan M. Cameron, and Viktor Kerzhanovich, Jet Propulsion Laboratory, G04-055 mu Synthesis for a Small Commercial Aircraft: California Institute of Technology (27, 4, p. 564) Article Design and Simulator Validation. Francesco Amato, Universita degli Studi Magna Graecia di Catanzaro; and Raffaele Iervolino, G04-069 Minimum-Energy Output Transitions for Linear University of Naples (27, 3, p. 479) Article Discrete-Time Systems: Flexible Structure Applications. Dhanakorn Iamratanakul, Hector Perez, and Santosh Devasia, G04-056 Simple Structure for a High Performance Three- University of Washington (27, 4, p. 572) Article Dimensional Tracking Filter. H. Weiss, Technion-Israel Institute of Technology; and G. Hexner, RAFAEL Armament Development G04-070 Dynamic Optimization Strategies for Three- Authority (27, 3, p. 491) Article Dimensional Conflict Resolution of Multiple Aircraft. Arvind U. Raghunathan, Carnegie Mellon University; Vipin Gopal, United G04-057 Mars and Mercury Missions Using Solar Sails and Technologies Research Center; Dharmashankar Subramanian, Solar Electric Propulsion. Christian Circi, University of Rome, Honeywell International; Lorenz T. Biegler, Carnegie Mellon Italy (27, 3, p. 496) Technical Note University; and Tariq Samad, Honeywell International (27, 4, p. 586) Article G04-058 Second-Order Equations for Rendezvous in a Circular Orbit. Christopher D. Karlgaard, Analytical Mechanics G04-071 Enhanced Air-to-Air Missile Tracking Using Target Associates, Inc.; and Frederick H. Lutze, Virginia Polytechnic Orientation Observations. Yaakov Oshman and David Arad, Institute and State University (27, 3, p. 499) Technical Note Technionolsrael Institute of Technology (27, 4, p. 595) Article G04-059 Sequential Computation of Total Least-Squares G04-072 Tuning of Observer-Based Controllers. C. Cumer and Parameter Estimates. Marco W. Soijer, Delft University of F. Delmond, ONERA-Centre d’Etudes et de Recherches de Technology, Germany (27, 3, p. 501) Technical Note Toulouse, France; D. Alazard and C. Chiappa, SUPAERO, France (27, 4, p. 607) Article based on AIAA Paper 2001-4102 G04-060 Optimal Interplanetary Trajectories Using Constant Radial Thrust and Gravitational Assists. Aaron J. Trask, Naval G04-073 Simulated Annealing for Missile Optimization: Research Laboratory; William J. Mason and Victoria L. Developing Method and Formulation Techniques. Ozan Coverstone, University of Illinois at Urbana-Champaign (27, 3, Tekinalp, Middle East Technical University, Aerospace Engineering p. 503) Technical Note based on AIAA Paper 2002-4731 Department, Turkey; and Muge Bingol, Middle East Technical University, Turkey (27, 4, p. 616) Article G04-061 Vehicle Motion Planning with Time-Varying Constraints. W. T. Cerven, Francesco Bullo, and Victoria L. G04-074 Robust Tracking Control Design for Spacecraft Under Coverstone, University of Illinois at Urbana-Champaign (27, 3, Control Input Saturation. Jovan D. Boskovic, Sai-Ming Li, and p. 506) Technical Note Raman K. Mehra, Scientific Systems Company, Inc. (27, 4, p. 627) Article G04-062 Extended Kalman Filtering for Satellite Orbital Attitude Estimation Based on Gibbs Vector. YuRong Lin and G04-075 Missile Autopilot Design Using Discrete-Time ZhengLong Deng, Harbin Institute of Technology (27, 3, p. 509) Variable Structure Controller with Sliding Sector. A. A. Powly Technical Note and M. S. Bhat, Indian Institute of Science, India (27, 4, p. 634) Article G04-063 Attitude Dynamics/Control of a Dual-BodySpacecraft with Variable-Speed Control Moment Gyros. Marcello Romano G04-076 Computation of Controllability Regions for Unstable and Brij N. Agrawal, Naval Postgraduate School (27, 4, p. 513) Aircraft Dynamics. M. G. Goman and M. N. Demenkov, De Article Montfort University, Great Britain (27, 4, p. 647) Article based on AIAA Paper 2002-4749 G04-064 Solar Sail Attitude Control and Dynamics, Part 1. Bong Wie, Arizona State University (27, 4, p. 526) Article G04-077 Analytical Theory of Three-Degree-of-Freedom Aircraft Wing Rock. Tiauw Hiong Go and Rudrapatna V. G04-065 Solar Sail Attitude Control and Dynamics, Part Two. Ramnath, Massachusetts Institute of Technology (27, 4, p. 657) Bong Wie, Arizona State University (27, 4, p. 536) Article Article J. GUIDANCE, VOL. 27, NO. 6: 2004 INDEX 1117 G04-078 Modeling Pilot’s Sequential Maneuvering Decisions G04-091 Neural-Network-Based Design of Optimal Controllers by a Multistage Influence Diagram. Kai Virtanen, Tuomas for Nonlinear Systems. Nilesh V. Kulkarni and Minh Q. Phan. Raivio, and Raimo P. Hamalainen, Helsinki University of Dartmouth College (27, 5, p. 745) Article based on AIAA Paper Technology, Finland (27, 4, p. 665) Article 2002-4664 G04-079 Optimization of Variable-Specific-Impulse G04-092 Human-Inspired Control Logic for Automated Interplanetary Trajectories. Lorenzo Casalino and Guido Maneuvering of Miniature Helicopter. V. Gavrilets, Bernard Colasurdo, Politecnico di Torina, Italy (27, 4, p. 678) Article Mettler, and E. Feron, Massachusetts Institute of Technology (27, 5, p. 752) Article G04-080 Formation Control of Satellites Subject to Drag Variations and J2 Perturbations. David Mishne, Techniondlsrael G04-093 Helicopter Vibration Reduction and Damping Institute of Technology (27, 4, p. 685) Article Enhancement Using Individual Blade Control. Thomas Mannchen and Klaus H. Weil, University of Stuttgart (27, 5, p. 760) G04-081 Solving Relative Two-Point Boundary Value Article Problems: Spacecraft Formulation Flight Transfers Application. V. M. Guibout and D. J. Scheeres, University of G04-094 Anytime Control Algorithm: Model Reduction Michigan (27, 4, p. 693) Article Approach. Raktim Bhattacharya, California Institute of Technology; and Gary J. Balas, University of Minnesota (27, 5, G04-082 Bank-to-Turn Missile Autopilot Design Via Observer- p. 767) Article Based Command Governor Approach. Alessandro Casavola, Universita della Calabria; and Edoardo Mosca, Universita di G04-095 Online Adaptive Critic Flight Control. Silvia Ferrari, Firenze (27, 4, p. 705) Technical Note Duke University; and Robert F. Stengel, Princeton University (27, 5, p. 777) Article G04-083 Adaptive Output Feedback Control Methodology: Theory and Practical Implementation Aspects. Moshe Idan, G04-096 Adaptive Linear Parameter Varying Control Technionolsrael Institute of Technology, Israel; Anthony J. Calise, Synthesis for Actuator Failure. Jong-Yeob Shin, National Georgia Institute of Technology; and Naira Hovakimyan, Virginia Institute of Aerospace; N. Eva Wu, Binghamton University; and Polytechnic Institute and State University (27, 4, p. 710) Technical Christine Belcastro, NASA Langley Research Center (27, 5, p. 787) Note Article G04-084 Guidance of Unmanned Air Vehicles Based on Fuzzy G04-097 Aeroelasticity of Time-Delayed Feedback Control Sets and Fixed Waypoints. Mario Innocenti and Lorenzo Pollini, of Two-Dimensional Supersonic Lifting Surfaces. Yuan Yuan, University of Pisa, Italy; and Demetrio Turra, University of Pisa Memorial University of Newfoundland, Canada; Pei Yu, The (27, 4, p. 715) Technical Note based on AIAA Paper 2002-4993 University of Western Ontario, Canada; Liviu Librescu, Virginia Polytechnic Institute and State University: and G04-085 Gain-Scheduling Stability Issues Using Differential Piergiovanni Marzocca, Clarkson University (27, 5, p. 795) Inclusion and Fuzzy Systems. Mario Innocenti, Lorenzo Pollini, Article and Antonio Marullo, University of Pisa, Italy (27, 4, p. 720) Technical Note G04-098 Investigating The Role of Rate Limiting in Pilot- Induced Oscillations. David H. Klyde, Systems Technology, Inc.: G04-086 Unified Algebraic Approach to Approximation of and David G. Mitchell, Hoh Aeronautics, Inc. (27, 5, p. 804) Article Lateral-Directional Modes and Departure Criteria. Giovanni based on AIAA Paper 2003-5463 Mengali, University of Pisa, Italy; and Fabrizio Giulietti, University of Bologna, Italy (27, 4, p. 724) Technical Note G04-099 Time Simulations of the Response of Maneuvering Flexible Aircraft. Leonard Meirovitch and Ilhan Tuzcu, Virginia G04-087 Limit Cycles and Domain of Stability in Unsteady Polytechnic Institute and State University (27, 5, p. 814) Article Aeroelastic System. Sushma Gujjula and Sahjendra N. Singh, based on AIAA Paper 2003-1403 University of Nevada, Las Vegas; and Wooson Yim, University of Nevada, Las Vegas (27, 4, p. 728) Article G04-100 Adaptive Sliding Mode Control Design for a Hypersonic Flight Vehicle. Haojian Xu, University of Southern G04-088 Review of Formulas for Dynamic Analysis. Kurt California; Maj. D. Mirmirani, California State University; and Anderson, Rensselaer Polytechnic Institute (27, 4, p. 733) Book Petros A. Ioannou, University of Southern California (27, 5, p. 829) Review Article G04-089 Review of Newton’s Tyranny: The Suppressed G04-101 Relative Orbit Geometry Through Classical Orbit Scientific Discoveries of Stephen Gray and John Flamsteed. M. Element Differences. Hanspeter Schaub, Virginia Polytechnic Peck, Honeywell Space Systems (27, 4, p. 734) Book Review Institute and State University (27, 5, p. 839) Article G04-090 New Approach for Modeling, Analysis, and Control of G04-102 Control of a Rotating Variable-Length Tethered Air Traffic Flow. P. K. Menon and G. D. Sweriduk, Optimal System. Mischa Kim and Christopher D. Hall, Virginia Synthesis Inc.; and K. D. Bilimoria, NASA Ames Research Center Polytechnic Institute and State University (27, 5, p. 849) (27, 5, p. 737) Article based on AIAA Paper 2001-5012 Article 1118 J. GUIDANCE, VOL. 27, NO. 6: 2004 INDEX G04-103 Integrated Power and Attitude Control with G04-116 Integrated Adaptive Guidance and Control for Re- Spacecraft Flywheels and Control Moment Gyroscopes. Carlos Entry Vehicles with Flight Test Results. John D. Schierman, M. Roithmayr, NASA Langley Research Center; Christopher D. David G. Ward, Jason R. Hull, and Neha Gandhi, Barron Karlgaard, Renjith R. Kumar, and David M. Bose, Analytical Associates, Inc.; David B. Doman and Michael Oppenheimer, Air Mechanics Associates, Inc. (27, 5, p. 859) Article based on AIAA Force Research Laboratory (27, 6, p. 975) Article Paper 03-124 G04-117 Lambert Guidance Routine Designed To Match G04-104 Periodic H2 Synthesis for Spacecraft Attitude Control Position And Velocity Of A Ballistic Target. Steven P. Burns and with Magnetorquers. Rafal Wisniewski and Jakob Stoustrup, Jeff J. Scherock, Johns Hopkins University, Applied Physics Aalborg University, Denmark (27, 5, p. 874) Article Laboratory (27, 6, p. 989) Article G04-105 Libration Control of Flexible Tethers Using G04-118 Trajectory Planning for Autonomous Aerospace Electromagnetic Forces and Movable Attachment. Paul Vehicles amid Known Obstacles and Conflicts. Hong Yang and Williams, Royal Melbourne Institute of Technology, Australia; Yiyuan Zhao, University of Minnesota (27, 6, p. 997) Article Takeo Watanabe, Tokyo Metropolitan Institute of Technology, Japan, Chris Blanksby and Pavel Trivailo, Royal Melbourne G04-119 Efficient Minimax Control Design for Prescribed Institute of Technology, Australia; and Hironori A. Fujii, Tokyo Parameter Uncertainty. Dirk Tenne and Tarunraj Singh, State Metropolitan Institute of Technology, Japan (27, 5, p. 882) Article University of New York at Buffalo (27, 6, p. 1009) Article based on AIAA Paper 2003-5781 G04-120 Nonlinear Control Allocation Using Piecewise Linear G04-106 Linear Theory of a Rotating Internal Part Functions. Michael A. Bolender and David B. Doman, U.S. Air Projectile Configuration in Atmospheric Flight. Geoffrey Force Research Laboratory (27, 6, p. 1017) Article Frost and Mark Costello, Oregon State University (27, 5, p. 898) Article G04-121 Dynamic Control Allocation Using Constrained Quadratic Programming. Ola Hiarkegird, Linkping University, G04-107 Method for Determination of Nonlinear Attainable Sweden (27, 6, p. 1028) Article Moment Sets. Michael A. Bolender and David B. Doman, Air Force Research Laboratory (27, 5, p. 907) Article G04-122 Transit-Orbit Search for Planar Restricted Three- Body Problems with Perturbations. Hideaki Yamato, The G04-108 Singular Perturbation Analysis of Optimal Glide. Pennsylvania State University, Japan; and David Spencer, The Ilana Shapira and Joseph Z. Ben-Asher, Technion—Israel Institute of Pennsylvania State University (27, 6, p. 1035) Article Technology, Israel (27, 5, p. 915) Technical Note based on AIAA Paper 2002-4406 G04-123 Low Thrust Minimum-Fuel Orbital Transfer: A Homotopic Approach. Thomas Haberkorn, Pierre Martinon, and G04-109 Modern Explicit Guidance Law for High-Order Joseph Gergaud, Centre National de la Recherche Scientifique, Dynamics. S. H. Jalali-Naini, Aerospace Research Institute, Iran France (27, 6, p. 1046) Article (27, 5, p. 918) Technical Note G04-124 Retargeting Dynamics of a Linear Tethered G04-110 Methods for Compensating for Control Allocator and Interferometer. Claudio Bombardelli, University of Padova, Italy; Actuator Interactions. Michael W. Oppenheimer and David B. Enrico C. Lorenzini, Harvard-Smithsonian Center for Doman, U.S. Air Force Research Laboratory (27, 5, p. 922) Astrophysics; and Marco B. Quadrelli, Jet Propulsion Laboratory, Technical Note California Institute of Technology (27, 6, p. 1061) Article based on AIAA Paper 222-03 G04-111 Generation of Launch Vehicle Abort Trajectories Using a Hybrid Optimization Method. Anthony J. Calise, G04-125 Design of Reduced-Order Robust Controllers for Georgia Institute of Technology; and Nico Brandt, Georgia Institute Smart Structural Systems. Pengxiang Liu and Vittal S. Rao, of Technology, Germany (27, 6, p. 929) Article based on AIAA University of Missouri—Rolla (27, 6, p. 1068) Article Paper 2002-4560 G04-126 Genetic Algorithm Preprocessing for Numerical G04-112 New Nonlinear Control Technique for Ascent Phase of Solution of Differential Games Problems. Kazuhiro Horie, Reusable Launch Vehicles. David Drake, Ming Xin, and S. N. University of Illinois at Urbana-Champaign; and Bruce A. Balakrishnan, University of Missouri—Rolla (27, 6, p. 930) Article Conway, University ofI llinois (27, 6, p. 1075) Technical Note G04-113 Dynamic Lateral Entry Guidance Logic. Zuojun Shen G04-127 Circular Navigation Missile Guidance’ with and Ping Lu, Jowa State University (27, 6, p. 949) Article Incomplete Information and Uncertain Autopilot Model. Ian R. Manchester and Andrey V. Savkin, University of New South Wales, G04-114 Test Results for Entry Guidance Methods for Space Australia (27, 6, p. 1078) Technical Note Vehicles. John M. Hanson, NASA Marshall Space Flight Center; and Robert E. Jones, Sverdrup Technology, Inc. (27, 6, p. 960) G04-128 Optimal Dual-Rate Digital Redesign with Application Article based on AIAA Paper 2004-0701 to Missile Control. C. A. Rabbath, Defence Research and Development Canada-Valcartier, Canada; Nicolas Lechevin, G04-115 Unpowered Approach and Landing Guidance Using Université du Quebec a Trois-Riviéres, Canada; and Noriyuki Trajectory Planning. Craig A. Kluever, University of Missouri- Hori, University of Tsukuba, Japan (27, 6, p. 1083) Technical Columbia (27, 6, p. 967) Article Note