Journal of Guidance, Control, and Dynamics 1993: Vol 16 Index

9 Pages·1993·2.9 MB·English

JOURNAL OF GUIDANCE, CONTROL, AND DYNAMICS
Vol. 16, No. 6, November—December 1993
1993 Journal of Guidance, Control, and Dynamics Index
How to Use the Index
In the Subject Index, pages 1201-1206, each technical paper is listed under a maximum of three appropriate headings. Note
the number in boldface type following each paper title, and use that number to locate the paper in the Chronological Index. The
Author Index, pages 1207—1208, lists all authors associated with a given technical paper. The locating numbers are identical to
those in the Subject Index. The Chronological Index, pages 1209-1215, lists all papers by their unique code 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, as well as the “CP” or conference volume number if the paper was
published in a bound collection of meetings papers. 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 1993, that paper also will appear in both the Subject and Chro-
nological Indexes. Authors of Comments also are listed in the Author Index.
Subject Index
Aircraft Technology, Quantitative Feedback Theory Applied to the Vibration
Design of a Rotorcraft Flight Control System
Conventional, STOL/VTOL
G93-116 Performance of Higher Harmonic Control Algo-
Synthesis and Evaluation of an H, Control Law rithms for Helicopter Vibration Reduction
Aerodynamics
for a Hovering Helicopter G93-088 G93-125
Time-Variant Analysis of Rotorcraft Systems Eigenvalue and Eigenvector Derivatives of Non-
Validation of Engineering Methods for Predict-
Dynamics—An Exploitation of Vector Pro- linear Eigenproblems G93-123
ing Hypersonic Vehicle Control Forces and
Moments G93-118 cessors G93-013 Multiple-Input, Multiple-Output Time-Series
Three-Dimensional Modeling and Control of a Models from Short Data Records G93-084
Twin-Lift Helicopter System G93-012
Aeroelasticity and Aeroservoelasticity
Flight Simulator Fidelity Assessment in a Rotor- Fluid Dynamics
Order Reduction of Linear-Quadratic-Gaussian— craft Lateral Translation Maneuver G93-011
Designed Controllers G93-179 Design of Flight Control Systems to Meet Rotor- Aeroacoustics
Optimal Control Law Synthesis for Flutter Sup- craft Handling Qualities Specifications
pression Using Active Acoustic Excitations G93-010 Optimal Control Law Synthesis for Flutter Sup-
G93-017 pression Using Active Acoustic Excitations
Safety G93-017
Aerospace Plane
Optimal Recovery from Microburst Wind Shear
Computational F luid Dynamics
Analytical Solutions to Constrained Hypersonic G93-160
Flight Trajectories G93-147 Complex-Frequency Method for Computing the
Inverse Dynamics Approach to Trajectory Opti- Simulation Dynamics of Liquid in a Spinning Container
mization for an Aerospace Plane G93-113 G93-026
Inverse Simulation of Large-Amplitude Aircraft
Flight Control Integration Maneuvers G93-114 Hypersonic Flow
Optimal Open Multistep Discretization Formulas
Constrained Control Allocation G93-112 for Real-Time Simulation G93-085 Validation of Engineering Methods for Predicting
Optimal Recovery from Microburst Wind Shear Flight-Path Estimation in Passive Low-Altitude Hypersonic Vehicle Control Forces and Mo-
G93-160 Flight by Visual Cues G93-051 ments G93-118
Digital Simulation of Atmospheric Turbulence
Flight Mechanics for Dryden and von Kaérman Models G93-018 Rarefied Flows
Flight Simulator Fidelity Assessment in a Rotor-
Longitudinal Dynamics of a Towed Sailplane craft Lateral Translation Maneuver G93-011 Refinements in Determining Satellite Drag Coef-
G93-128 ficients: Method for Resolving Density Dis-
Guidance Law for Planar Hypersonic Descent to STOL/VTOL/STOVL crepancies G93-069
a Point G93-060
Nonlinear Smoothing Identification Algorithm Design and Piloted Simulation of Integrated Wave Motion and Sloshing
with Application to Data Consistency Checks Flight/Propulsion Controls for STOVL Air-
G93-048 craft G93-158 Dynamic Characteristics of Liquid Motion in Par-
tially Filled Tanks of a Spinning Spacecraft
Military Missions Structural Design (Including Loads) G93-101
Complex-Frequency Method for Computing the
New Analytical Solutions for Proportional Navi- Time-Variant Analysis of Rotorcraft Systems Dynamics of Liquid in a Spinning Container
gation G93-091 Dynamics—An Exploitation of Vector Pro- G93-026
cessors G93-013
Rotorcraft
Guidance, Control, and Dynamics
Testing, Flight and Ground
Performance of Higher Harmonic Control Algo- Technology
rithms for Helicopter Vibration Reduction Nonlinear Smoothing Identification Algorithm
G93-125 with Application to Data Consistency Checks Aircraft Dynamics
Linear Quadratic Gaussian/Loop Transfer Re- G93-048
covery Design for a Helicopter in Low-Speed Identification of Observer/Kalman Filter Markov Optimal Recovery from Microburst Wind Shear
Flight G93-117 Parameters: Theory and Experiments G93-046 G93-160
1201
1202 J. GUIDANCE, VOL. 16,NO.6: 1993 INDEX
Use of Neural Networks in Control of High-Al- Design of Insensitive Multirate Aircraft Control Robustness Analysis of a Multirate Flutter Sup-
pha Maneuvers G93-144 Using Optimized Eigenstructure Assignment pression System G93-142
Automatic Carrier Landing System Utilizing Air- G93-016 Controllability and Observability of Flexible
craft Sensors G93-141 Application of Feedback Linearization Method Structures with Proof-Mass Actuators
Longitudinal Dynamics of a Towed Sailplane in a Digital Restructurable Flight Control Sys- G93-138
G93-128 tem G93-015 Feedback Gain Sensitivities of Closed-Loop
Periodic Maximum Range Cruise with Singular Fixed-Order Dynamic Compensation for a High- Modal Parameters of Controlled Structures
Control G93-124 Performance Fighter Aircraft G93-014 G93-137
Inverse Simulation of Large-Amplitude Aircraft Three-Dimensional Modeling and Control of a Piezoelectric Actuator Design for Vibration Sup-
Maneuvers G93-114 Twin-Lift Helicopter System G93-012 pression: Placement and Sizing G93-133
Design of a Robust Estimator for Target Track- Active Control Technology for Large Space
ing G93-092 Artificial Intelligence Structures G93-127
Time-Optimal Reorientation Maneuvers for a Performance of Higher Harmonic Control Algo-
Combat Aircraft G93-034 Aircraft Failure Detection and Identification Us- rithms for Helicopter Vibration Reduction
Control of Wing-Rock Motion of Slender Delta ing Neural Networks G93-159 G93-125
Wings G93-033 Use of Neural Networks in Control of High-Al- Controller Design with Regional Pole Con-
Digital Simulation of Atmospheric Turbulence pha Maneuvers G93-144 straints: Hyperbolic and Horizontal Strip Re-
for Dryden and von Karman Models G93-018 Neurocontrol Design and Analysis for a Multi- gions G93-122
Three-Dimensional Modeling and Control of a variable Aircraft Control Problem G93-115 Linear Quadratic Gaussian/Loop Transfer Re-
Twin-Lift Helicopter System G93-012 covery Design for a Helicopter in Low-Speed
Astrodynamics Flight G93-117
Aircraft Guidance Quantitative Feedback Theory Applied to the
H, Optima! Halo Orbit Guidance G93-174 Design of a Rotorcraft Flight Control System
Design of Guaranteed Performance Controllers Optimal Cooperative Power-Limited Rendez- G93-116
for Systems with Varying Parameters vous Between Neighboring Circular Orbits Robust Sampled Data Eigenstructure Assign-
G93-186 G93-165 ment Using the Delta Operator G93-110
Automatic Carrier Landing System Utilizing Air- Optimal Weighting of a Priori Statistics in Robustness Bounds for Linear Systems Under
craft Sensors G93-141 Quick-Look Orbit Determination G93-157 Uncertainty: Eigenvalues Inside a Wedge
Neurocontrol Design and Analysis for a Multi- Sun-Perturbed Earth-to-Moon Transfers with G93-109
Ballistic Capture G93-119
variable Aircraft Control Problem G93-115 Vibration and Robust Control of Symmetric
Zero-Gravity Atmospheric Flight by Robust Maneuver and Vibration Control of Hybrid Co- Flexible Systems G93-107
ordinate Systems Using Lyapunov Stability
Nonlinear Inverse Dynamics G93-096 Maneuver and Vibration Control of Hybrid Co-
Theory G93-106
Real-Time Optimal Control of Aircraft Turn Tra- ordinate Systems Using Lyapunov Stability
Time-Closed Optimal Transfer by Two Impulses
jectories G93-054 Theory G93-106
Between Coplanar Elliptical Orbits G93-089
Elastomer Damper for a Freely Precessing Dual- Simultaneous Design of Active Vibration Con-
Stable Orbits About the Martian Moons
Spin Seeker G93-032 trol and Passive Viscous Damping G93-104
G93-068
Quaternion-Based Rate/Attitude Tracking Sys-
Aircraft Stability and Control tem with Application to Gimbal Attitude Con-
Computer Science
trol G93-097
Design of Guaranteed Performance Controllers Gain Scheduling Simplification by Simultaneous
Optimal Open Multistep Discretization Formulas
for Systems with Varying Parameters Control Design G93-095
for Real-Time Simulation G93-085
G93-186 Stabilizability of Linear Quadratic State Feed-
Flight Control Application of New Stability Ro- Control System Design back for Uncertain Systems G93-093
bustness Bounds for Linear Uncertain Sys- Synthesis and Evaluation of an H, Control Law
tems G93-163 Optimal Control System Design with Prescribed for a Hovering Helicopter G93-088
Flight-Determined Multivariable Stability Anal- Damping and Stability Characteristics Robustness Evaluation of a Flexible Aircraft
ysis and Comparison of a Control System G93-185 Control System G93-086
G93-162 Inversion-Based Nonlinear Control of Robot Quasi-Closed-Form Solution to the Time-Opti-
Aircraft Failure Detection and Identification Us- Arms with Flexible Links G93-181 mal Rigid Spacecraft Reorientation Problem
ing Neural Networks G93-159 Fuel-Optimal Slewing of an Experimental G93-071
Full Envelope Multivariable Control Law Syn- Hinged-Free Beam G93-180 Parametric Study of Adaptive Generalized Pre-
thesis for a High-Performance Test Aircraft H,, Norm Sensitivity Formula with Control Sys- dictive Controllers G93-062
G93-146 tem Design Applications G93-177 Factorization Approach to Control System Syn-
Application of Structured Singular Value Syn- H™ Robust Control Design for Linear Feedback thesis G93-061
thesis to a Fighter Aircraft G93-145 Systems G93-176 Pointing Control, with Tethers as Actuators, of a
Linear Quadratic Gaussian/Loop Transfer Re- H, Optimal Halo Orbit Guidance G93-174 Space Station Supported Platform G93-059
covery Design for a Helicopier in Low-Speed Classical and Robust H,, Control Redesign for Frequency-Weighted System Identification and
Flight G93-117 the Hubble Space Telescope G93-168 Linear Quadratic Controller Design G93-047
Neurocontrol Design and Analysis for a Multi- Input-Shaped Control of Three-Dimensional Ma- Q-Markov Covariance Equivalent Realization
variable Aircraft Control Problem G93-115 neuvers of Flexible Spacecraft G93-167 and its Application to Flexible Structure Iden-
Inverse Simulation of Large-Amplitude Aircraft Flight Control Application of New Stability Ro- tification G93-045
Maneuvers G93-114 bustness Bounds for Linear Uncertain Sys- Sensor-Actuator Placement for Flexible Struc-
Constrained Control Allocation G93-112 tems G93-163 tures with Actuator Dynamics G93-044
Zero-Gravity Atmospheric Flight by Robust Design and Piloted Simulation of Integrated Fuel-Optimal Propulsive Reboost of Flexible
Nonlinear Inverse Dynamics G93-096 Flight/Propulsion Controls for STOVL Air- Spacecraft G93-043
Gain Scheduling Simplification by Simultaneous craft G93-158 Gain-Scheduled Missile Autopilot Design Using
Control Design G93-095 Reduced Order Proportional Integral Observer Linear Parameter Varying Transformations
Stabilizability of Linear Quadratic State Feed- with Application G93-156 G93-037
back for Uncertain Systems G93-093 Buckling Control of a Flexible Beam Using Pi- Robust Flight-Path Control System Design with
New Robust and Flexible Parameter Estimation ezoelectric Actuators G93-153 Multiple-Delay Model Approach G93-035
Method G93-064 Disturbance Rejection in Flexible Structures via Optimal Control Law Synthesis for Flutter Sup-
Factorization Approach to Control System Syn- the Quantitative Feedback Theory 93-151 pression Using Active Acoustic Excitations
thesis G93-061 Full Envelope Multivariable Control Law Syn- G93-017
U-Parameter Design for Terrain-Following thesis for a High-Performance Test Aircraft Design of Insensitive Multirate Aircraft Control
Flight Control G93-055 G93-146 Using Optimized Eigenstructure Assignment
Refined H”-Optimal Approach to Rotorcraft Application of Structured Singular Value Syn- G93-016
Flight Control G93-036 thesis to a Fighter Aircraft G93-145 Application of Feedback Linearization Method
Control of Wing-Rock Motion of Slender Delta Trajectory Control for a Low-Lift Re-Entry Ve- in a Digital Restructurable Flight Control Sys-
Wings G93-033 hicle G93-143 tem G93-015
J. GUIDANCE, VOL. 16,NO.6: 1993 INDEX 1203
Fixed-Order Dynamic Compensation for a High- Robust Sampled Data Eigenstructure Assign- Attitude Dynamics and Control of a Vertical In-
Performance Fighter Aircraft G93-014 ment Using the Delta Operator G93-110 terferometric Radar Tethered Altimeter
Design of Flight Control Systems to Meet Rotor- Reaction Wheel Low-Speed Compensation Us- G93-038
craft Handling Qualities Specifications ing a Dither Signal G93-098 Attitude Control with Realization of Linear Error
G93-010 Zero-Gravity Atmospheric Flight by Robust Dynamics G93-025
Designing Reduced-Order Linear Multivariable Nonlinear Inverse Dynamics G93-096 Trajectory Design, Feedforward, and Feedback
Controllers Using Experimentally Derived Stabilizability of Linear Quadratic State Feed- Stabilization of Tethered Spacecraft Retrieval
Plant Data G93-008 back for Uncertain Systems G93-093 G93-022
Newton Algorithm for Fitting Transfer Functions Largest Hypersphere of Stability for Polynomials Time-Variant Analysis of Rotorcraft Systems
to Frequency Response Measurements with Perturbed Coefficients G93-090 Dynamics—An Exploitation of Vector Pro-
G93-005 Optimal Open Multistep Discretization Formulas cessors G93-013
Real Parameter Margin Computation for Uncer- for Real-Time Simulation G93-085
tain Structural Dynamic Systems G93-004 Saturating and Time-Optimal Feedback Con- Flight Mechanics
Experimental Study of Robustness in Adaptive trols G93-083
Control for Large Flexible Structures G93-002 Optimal Discrete-Time Dynamic Output-Feed- Analytical Solutions to Constrained Hypersonic
Experiments in Multivariable Adaptive Control back Design: A w-Domain Approach Flight Trajectories G93-147
of a Large Flexible Structure G93-001 G93-082 Use of Neural Networks in Control of High-Al-
Active Vibration Control of Flexible Structures pha Maneuvers G93-144
Control System Effectors with Acceleration Feedback G93-065 Periodic Maximum Range Cruise with Singular
Model Reduction of Mechanical Systems Control G93-124
Controllability and Observability of Flexible G93-063 Enhancement of Endurance Performance by Pe-
Structures with Proof-Mass Actuators Parametric Study of Adaptive Generalized Pre- riodic Optimal Camber Control G93-087
G93-138 dictive Controllers G93-062 Time-Optimal Reorientation Maneuvers for a
Validation of Engineering Methods for Predict- Factorization Approach to Control System Syn- Combat Aircraft G93-034
ing Hypersonic Vehicle Control Forces and thesis G93-061
Moments G93-118 U-Parameter Design for Terrain-Following Handling Qualities
Constrained Control Allocation G93-112 Flight Control G93-055
Real-Time Optimal Control of Aircraft Turn Tra- Design and Piloted Simulation of Integrated
Control System Sensors jectories G93-054 Flight/Propulsion Controls for STOVL Air-
Missile Autopilot Robustness Using the Real craft G93-158
Sensor Failure Detection and Isolation in Flexi- Multiloop Stability Margin G93-050 Quantitative Feedback Theory Applied to the
bie Structures Using System Realization Re- Q-Markov Covariance Equivalent Realization Design of a Rotorcraft Flight Control System
dundancy G93-076 and its Application to Flexible Structure Iden- G93-116
Two-Axis Dry Tuned-Rotor Gyroscopes: Design tification G93-045 Analytical Development of an Equivalent Sys-
and Technology G93-066 Gain-Scheduled Missile Autopilot Design Using tem Mismatch Function G93-111
Elastomer Damper for a Freely Precessing Dual- Linear Parameter Varying Transformations Synthesis and Evaluation of an H, Control Law
Spin Seeker G93-032 G93-037 for a Hovering Helicopter G93-088
Control of Wing-Rock Motion of Slender Delta Flight Simulator Fidelity Assessment in a Rotor-
Control Theory Wings G93-033 craft Lateral Translation Maneuver G93-011
Fuel-Optimal Rendezvous in a General Central Design of Flight Control Systems to Meet Rotor-
Invariant Set Analysis of the Hub-Appendage Force Field G93-029 craft Handling Qualities Specifications
Problem G93-188 Attitude Control with Realization of Linear Error G93-010
Design of Guaranteed Performance Controllers Dynamics G93-025
for Systems with Varying Parameters Design of Insensitive Multirate Aircraft Control Launch Vehicle Dynamics
G93-186 Using Optimized Eigenstructure Assignment
Optimal Control System Design with Prescribed G93-016 Rotational Motion and Guidance System Ap-
Damping and Stability Characteristics Fixed-Order Dynamic Compensation for a High- proximations in Optimizable Operational
G93-185 Performance Fighter Aircraft G93-014 Launch Vehicle Simulations G93-074
Path-Constrained Trajectory Optimization Using
New Proof of the Jacobi Necessary Condition
Sparse Sequential Quadratic Programming Launch Vehicle Guidance and Control
G93-183
G93-009
Inversion-Based Nonlinear Control of Robot
Shaping of System Responses with Minimax Op- Optimal Rocket Steering in Terms of Angular
Arms with Flexible Links G93-181
timization in the Time Domain G93-006 Velocity of the Primer Vector G93-187
Order Reduction of Linear-Quadratic-Gaussian— Real Parameter Margin Computation for Uncer- Analytical Solutions to Constrained Hypersonic
Designed Controllers G93-179 tain Structural Dynamic Systems G93-004 Flight Trajectories G93-147
H™ Robust Control Design for Linear Feedback Goddard Problem in Presence of a Dynamic
Systems G93-176 Dynamics Pressure Limit G93-120
Classical and Robust H,, Control Redesign for Inverse Dynamics Approach to Trajectory Opti-
the Hubble Space Telescope G93-168 Equimomental System of Rigidly Connected mization for an Aerospace Plane G93-113
Flight Control Application of New Stability Ro- Equal Particles G93-189 General Adaptive Guidance Using Nonlinear
bustness Bounds for Linear Uncertain Sys- Block-Diagonal Equations for Multibody Elasto- Programming Constraint-Solving Methods
tems G93-163 dynamics with Geometric Stiffness and Con- G93-080
Flight-Determined Multivariable Stability Anal- straints G93-171
ysis and Comparison of a Control System State Equations for Maneuvering and Control of Missile Dynamics
G93-162 Flexible Bodies Using Quasimomenta
Reduced Order Proportional Integral Observer G93-136 Missile Autopilot Robustness Using the Real
with Application G93-156 Passive Dynamic Controllers for Nonlinear Me- Multiloop Stability Margin G93-050
Control and Filtering of Wide-Band Noise Driv- chanical Systems G93-131
en Linear Systems G93-155 Nonrecursive Order N Formulation of Multibody Missile Guidance and Control
Robust Time-Optimal Control of Uncertain Dynamics G93-130
Structural Dynamic Systems G93-154 Eigenvalue and Eigenvector Derivatives of Non- Exact Closed-Form Solution of Generalized Pro-
Optimal Pointing Control of Robotic Manipula- linear Eigenproblems G93-123 portional Navigation G93-149
tors with State Inequality Constraints G93-150 Averaging of Second-Order Hamiltonian Oscil- Robust Sampled Data Eigenstructure Assign-
Asymptotic Stability Theorem for Autonomous lators with a Slowly Varying Parameter ment Using the Delta Operator G93-110
Systems G93-148 G93-121 Minimum-Effort Interception of Multiple Tar-
State Equations for Maneuvering and Control of Sun-Perturbed Earth-to-Moon Transfers with gets G93-094
Flexible Bodies Using Quasimomenta Ballistic Capture G93-119 New Analytical Solutions for Proportional Navi-
G93-136 Q-Markov Covariance Equivalent Realization gation G93-091
Sun-Perturbed Earth-to-Moon Transfers with and its Application to Flexible Structure Iden- Generalized Guidance Law for Collision
Ballistic Capture G93-119 tification G93-045 Courses G93-079
1204 J. GUIDANCE, VOL. 16, NO. 6: 1993 INDEX
Two-Axis Dry Tuned-Rotor Gyroscopes: Design Quasi-Closed-Form Solution to the Time-Opti- GSTAR III Attitude for Inclined Geostationary
and Technology G93-066 mal Rigid Spacecraft Reorientation Problem Orbit G93-039
Guidance Law for Planar Hypersonic Descent to G93-071 Complex-Frequency Method for Computing the
a Point G93-060 Sensor-Actuator Placement for Flexible Struc- Dynamics of Liquid in a Spinning Container
Maneuvering Target Tracking via Smoothing tures with Actuator Dynamics G93-044 G93-026
and Filtering Through Measurement Concate- Fuel-Optimal Propulsive Reboost of Flexible Innovative Approach to the Momentum Manage-
nation G93-053 Spacecraft G93-043 ment Control for Space Station Freedom
Designing Nonlinear Filters Based on Daum’s Fuel-Optimal Reorientation of Axisymmetric G93-024
Theory G93-052 Spin-Stabilized Satellites G93-030
Missile Autopilot Robustness Using the Real Path-Constrained Trajectory Optimization Using Spacecraft Guidance and Control
Multiloop Stability Margin G93-050 Sparse Sequential Quadratic Programming
Time-Optimal Attitude Control Scheme for a G93-009 H, Optimal Halo Orbit Guidance G93-174
Spinning Missile G93-049 Deployment and Retrieval Optimization of a
Some Aspects of a Realistic Three-Dimensional Shaping of System Responses with Minimax Op- Tethered Satellite System G93-170
Pursuit-Evasion Game G93-042 timization in the Time Domain G93-006 Optima! Periodic Control for Spacecraft Pointing
Gain-Scheduled Missile Autopilot Design Using Newton Algorithm for Fitting Transfer Functions and Attitude Determination G93-169
Linear Parameter Varying Transformations to Frequency Response Measurements Classical and Robust H,, Control Redesign for
G93-037 G93-005 the Hubble Space Telescope G93-168
Application of Quantitative Feedback Theory to Differential Angle Tracking for Close Geosta-
a Class of Missiles G93-007 Pointing Systems tionary Satellites G93-166
Optimal Cooperative Power-Limited Rendez-
Navigation Optimal Pointing Control of Robotic Manipula- vous Between Neighboring Circular Orbits
tors with State Inequality Constraints G93-150 G93-165
Two-Error Covariance Analysis Algorithms for Gain Adaptive Tracking G93-134 Asymptotic Stability Theorem for Autonomous
Suboptimal Decentralized Kalman Filters Control/Structure Interactions of Space Station Systems G93-148
G93-140 Solar Dynamic Modules G93-099 Trajectory Control for a Low-Lift Re-Entry Ve-
Autonomous Position and Velocity Determina- Design of a Robust Estimator for Target Track- hicle G93-143
tion in Interplanetary Space G93-126 ing G93-092 Active Control Technology for Large Space
Reaction Wheel Low-Speed Compensation Us- Star Trackers, Star Catalogs, and Attitude Deter- Structures G93-127
ing a Dither Signal G93-098 mination: Probabilistic Aspects of System De- Singular Control in Minimum Time Spacecraft
Star Trackers, Star Catalogs, and Attitude Deter- sign G93-077 Reorientation G93-108
mination: Probabilistic Aspects of System De- Time-Optimal Three-Axis Reorientation of a Quaternion-Based Rate/Attitude Tracking Sys-
sign G93-077 Rigid Spacecraft G93-070 tem with Application to Gimbal Attitude Con-
Attitude Determination in Higher Dimensions Time-Optimal Attitude Control Scheme for a trol G93-097
G93-058 Spinning Missile G93-049 General Adaptive Guidance Using Nonlinear
Exact Conversion of Earth-Centered, Earth- Programming Constraint-Solving Methods
Ground Verification for Satellite High-Accuracy
Fixed Coordinates to Geodetic Coordinates G93-080
Onboard Antenna Drive Control Systems
G93-056 Guidance for an Aerocapture Maneuver
G93-031
Ground Tests of Magnetometer-Based Autono- G93-078
mous Navigation (MAGNAV) for Low-Earth- Precision Attitude Control for Tethered Satel- Quasi-Closed-Form Solution to the Time-Opti-
Orbiting Spacecraft G93-028 lites G93-023 mal Rigid Spacecraft Reorientation Problem
Application of the Global Positioning System for Designing Reduced-Order Linear Multivariable G93-071
Hermes Rendezvous Navigation G93-027 Controllers Using Experimentally Derived Time-Optimal Three-Axis Reorientation of a
Visual Display Aid for Orbital Maneuvering: Ex- Plant Data G93-008 Rigid Spacecraft G93-070
perimental Evaluation G93-020 Optimal Impulsive Intercept with Low-Thrust
Visual Display Aid for Orbital Maneuvering: De- Signal Processing Rendezvous Return G93-067
sign Considerations G93-019 Model Reduction of Mechanical Systems
Optimal Weighting of a Priori Statistics in G93-063
Optimization Techniques Quick-Look Orbit Determination G93-157 Attitude Determination in Higher Dimensions
G93-058
Optimal Rocket Steering in Terms of Angular Software Technology Frequency-Weighted System Identification and
Velocity of the Primer Vector G93-187 Linear Quadratic Controller Design G93-047
Optimal Control System Design with Prescribed Recursive Dynamics Algorithm for Multibody Automatic Spacecraft Docking Using Computer
Damping and Stability Characteristics Systems with Prescribed Motion G93-129 Vision-Based Guidance and Control Tech-
G93-185 niques G93-041
Riccati Solution for the Minimum Model Error Spacecraft Dynamics GSTAR III Attitude for Inclined Geostationary
Algorithm G93-184 Orbit G93-039
New Proof of the Jacobi Necessary Condition Deployment and Retrieval Optimization of a Fuel-Optimal Reorientation of Axisymmetric
G93-183 Tethered Satellite System G93-170 Spin-Stabilized Satellites G93-030
H., Norm Sensitivity Formula with Control Sys- Input-Shaped Control of Three-Dimensional Ma- Fuel-Optimal Rendezvous in a General Central
tem Design Applications G93-177 neuvers of Flexible Spacecraft G93-167 Force Field G93-029
Deployment and Retrieval Optimization of a Passive Dynamic Controllers for Nonlinear Me- Application of the Global Positioning System for
Tethered Satellite System G93-170 chanical Systems G93-131 Hermes Rendezvous Navigation G93-027
Optimal Pointing Control of Robotic Manipula- Recursive Dynamics Algorithm for Multibody Innovative Approach to the Momentum Manage-
tors with State Inequality Constraints G93-150 Systems with Prescribed Motion G93-129 ment Control for Space Station Freedom
Goddard Problem in Presence of a Dynamic Nutational Stability and Core Energy of a Qua- G93-024
Pressure Limit G93-120 sirigid Gyrostat G93-102 Precision Attitude Control for Tethered Satel-
Robustness Bounds for Linear Systems Under lites G93-023
Uncertainty: Eigenvalues Inside a Wedge Dynamic Characteristics of Liquid Motion in Trajectory Design, Feedforward, and Feedback
G93-109 Partially Filled Tanks of a Spinning Space- Stabilization of Tethered Spacecraft Retrieval
Singular Control in Minimum Time Spacecraft craft G93-101 G93-022
Reorientation G93-108 Pointing Accuracy of a Dual-Spin Satellite due to Visual Display Aid for Orbital Maneuvering: Ex-
Simultaneous Design of Active Vibration Con- Torsional Appendage Vibrations G93-100 perimental Evaluation G93-020
trol and Passive Viscous Damping G93-104 Control/Structure Interactions of Space Station Visual Display Aid for Orbital Maneuvering: De-
Minimum-Effort Interception of Multiple Tar- Solar Dynamic Modules G93-099 sign Considerations G93-019
gets G93-094 Pointing Control, with Tethers as Actuators, of a
Disturbance Model for Control/Structure Opti- Space Station Supported Platform G93-059 State Estimation
mization with Full State Feedback G93-081 Automatic Spacecraft Docking Using Computer
First-Order Models for Satellite Survivability Vision-Based Guidance and Control Tech- Riccati Solution for the Minimum Model Error
Optimization G93-072 niques G93-041 Algorithm G93-184
J. GUIDANCE, VOL. 16, NO. 6: 1993 INDEX 1205
Optimal Periodic Control for Spacecraft Pointing Control/Structure Interactions of Space Station Time-Optimal Three-Axis Reorientation of a
and Attitude Determination G93-169 Solar Dynamic Modules G93-099 Rigid Spacecraft G93-070
Identification of Aerodynamic Coefficients Us- Saturating and Time-Optimal Feedback Con- Optimal Impulsive Intercept with Low-Thrust
ing Computational Neural Networks G93-161 trols G93-083 Rendezvous Return G93-067
Aircraft Failure Detection and Identification Us- Disturbance Model for Control/Structure Opti- Guidance Law for Planar Hypersonic Descent to
ing Neural Networks G93-159 mization with Full State Feedback G93-081 a Point G93-060
Optimal Weighting of a Priori Statistics in Sensitivity-Based Characterization and Optimi- Equation for Optimal Power-Limited Spacecraft
Quick-Look Orbit Determination G93-157 zation of Viscoelastically Damped Honey- Trajectories G93-057
Reduced Order Proportional Integral Observer comb Structures G93-075 U-Parameter Design for Terrain-Following
with Application G93-156 Control of Nonlinear Structural Dynamic Sys- Flight Control G93-055
Control and Filtering of Wide-Band Noise Driv- tems: Chaotic Vibrations G93-073
Real-Time Optimal Control of Aircraft Turn Tra-
en Linear Systems G93-155 Sensor-Actuator Placement for Flexible Struc-
jectories G93-054
Two-Error Covariance Analysis Algorithms for tures with Actuator Dynamics G93-044
Suboptimal Decentralized Kalman Filters Active Vibration Damping of the Space Shuttle Time-Optimal Reorientation Maneuvers for a
G93-140 Remote Manipulator System G93-040 Combat Aircraft G93-034
Estimation of Kalman Filter Gain from Output Fuel-Optimal Reorientation of Axisymmetric Fuel-Optimal Rendezvous in a General Central
Residuals G93-139 Spin-Stabilized Satellites G93-030 Force Field G93-029
Gain Adaptive Tracking G93-134 Designing Reduced-Order Linear Multivariable Trajectory Design, Feedforward, and Feedback
Autonomous Position and Velocity Determina- Controllers Using Experimentally Derived Stabilization of Tethered Spacecraft Retrieval
tion in Interplanetary Space G93-126 Plant Data G93-008 G93-022
Reaction Wheel Low-Speed Compensation Us- Shaping of System Responses with Minimax Op- Path-Constrained Trajectory Optimization Using
ing a Dither Signal G93-098 timization in the Time Domain G93-006 Sparse Sequential Quadratic Programming
Design of a Robust Estimator for Target Track- Experiments in Multivariable Adaptive Control G93-009
ing G93-092 of a Large Flexible Structure G93-001
Attitude Determination in Higher Dimensions Interdisciplinary Topics
G93-058 System Identification
Maneuvering Target Tracking via Smoothing Application of a Periodic Lattice Filter for Iden- Analytical and Numerical Methods
and Filtering Through Measurement Concate-
tifying Flexible Structures G93-173
nation G93-053 Identification of Aerodynamic Coefficients Us- Block-Diagonal Equations for Multibody Elasto-
Designing Nonlinear Filters Based on Daum’s ing Computational Neural Networks G93-161 dynamics with Geometric Stiffness and Con-
Theory G93-052 Estimation of Kalman Filter Gain from Output straints G93-171
Identification of Observer/Kalman Filter Markov Residuals G93-139 Averaging of Second-Order Hamiltonian Oscil-
Parameters: Theory and Experiments G93-046 Consistent-Mode Indicator for the Eigensystem lators with a Slowly Varying Parameter
Ground Tests of Magnetometer-Based Autono- Realization Algorithm G93-132 G93-121
mous Navigation (MAGNAV) for Low-Earth- Multiple-Input, Multiple-Output Time-Series Extremal Vehicle Reorientation Maneuvers:
Orbiting Spacecraft G93-028 Models from Short Data Records G93-084 Symmetries and Group Properties G93-103
Zero Locus of a Beam with Varying Sensor and
New Robust and Flexible Parameter Estimation Nutational Stability and Core Energy of a Qua-
Actuator Locations G93-003
Method G93-064 sirigid Gyrostat G93-102
Nonlinear Smoothing Identification Algorithm Digital Simulation of Atmospheric Turbulence
Structural Control
with Application to Data Consistency Checks for Dryden and von K4érma4n Models G93-018
G93-048
Control of a Structure with Two Closely Spaced
Frequencies G93-182 Frequency-Weighted System Identification and Atmospheric and Space Sciences
Linear Quadratic Controller Design G93-047
Order Reduction of Linear-Quadratic-Gaussian—
Designed Controllers G93-179 Identification of Observer/Kalman Filter Markov Refinements in Determining Satellite Drag Coef-
H,, Optimized Wave-Absorbing Control: Analyt- Parameters: Theory and Experiments G93-046 ficients: Method for Resolving Density Dis-
ical and Experimental Results G93-178 Newton Algorithm for Fitting Transfer Functions crepancies G93-069
to Frequency Response Measurements
H.,, Norm Sensitivity Formula with Control Sys-
tem Design Applications G93-177 G93-005 Human Factors
Zero Locus of a Beam with Varying Sensor and
Discrete-Time Model Reduction in Limited Fre-
quency Ranges G93-175 Actuator Locations G93-003 Flight-Path Estimation in Passive Low-Altitude
Inpnuetu-vSehrsa peodf FCloenxtirbolle oSfp aTchercerea-ftD imensionGa9l3 -1M6a7- Trajectory Optimization VisFulailg htD isbpyl aVyi suAaild Cfuore sO rbital ManeuverinGg93:- 0E5x1-
Buckling Control of a Flexible Beam Using Pi- Optimal Rocket Steering in Terms of Angular perimental Evaluation G93-020
ezoelectric Actuators G93-153 Velocity of the Primer Vector G93-187 Visual Display Aid for Orbital Maneuvering: De-
Robust Control of Flexible Structures Using Re- Optimal Cooperative Power-Limited Rendez- sign Considerations G93-019
sidual Mode Filters G93-152 vous Between Neighboring Circular Orbits
Estimation of Kalman Filter Gain from Output G93-165 Sensor Systems
Residuals G93-139 Automatic Carrier Landing System Utilizing Air-
State Equations for Maneuvering and Control of craft Sensors G93-141 Two-Axis Dry Tuned-Rotor Gyroscopes: Design
Flexible Bodies Using Quasimomenta Periodic Maximum Range Cruise with Singular and Technology G93-066
G93-136 Control G93-124
Minimum Time Pulse Response Based Control Goddard Problem in Presence of a Dynamic Launch Vehicle and Missile
of Flexible Structures G93-135 Pressure Limit G93-120
(LV/M) Technology
Piezoelectric Actuator Design for Vibration Sup- Inverse Dynamics Approach to Trajectory Opti-
pression: Placement and Sizing G93-133 mization for an Aerospace Plane G93-113
Passive Dynamic Controllers for Nonlinear Me- Singular Control in Minimum Time Spacecraft Launch Vehicle and Sounding Rocket
chanical Systems G93-131 Reorientation G93-108 Systems
Active Control Technology for Large Space Extremal Vehicle Reorientation Maneuvers:
Structures G93-127 Symmetries and Group Properties G93-103 Rotational Motion and Guidance System Ap-
Robustness Bounds for Linear Systems Under Minimum-Effort Interception of Multiple Tar- proximations in Optimizable Operational
Uncertainty: Eigenvalues Inside a Wedge gets G93-094 Launch Vehicle Simulations G93-074
G93-109 Time-Closed Optimal Transfer by Two Impulses
Vibration and Robust Control of Symmetric Between Coplanar Elliptical Orbits G93-089 Missile Systems
Flexible Systems G93-107 Enhancement of Endurance Performance by Pe-
Passive Damping for Robust Feedback Control riodic Optimal Camber Control G93-087 New Analytical Solutions for Proportional Navi-
of Flexible Structures G93-105 Rotational Motion and Guidance System Ap- gation G93-091
Simultaneous Design of Active Vibration Con- proximations in Optimizable Operational Elastomer Damper for a Freely Precessing Dual-
trol and Passive Viscous Damping G93-104 Launch Vehicle Simulations G93-074 Spin Seeker G93-032
1206 J. GUIDANCE, VOL. 16, NO.6: 1993 INDEX
Simulation Active Vibration Damping of the Space Shuttle Multiple-Input, Multiple-Output Time-Series
Remote Manipulator System G93-040 Models from Short Data Records G93-084
Some Aspects of a Realistic Three-Dimensional Sensor Failure Detection and Isolation in Flexi-
Pursuit-Evasion Game G93-042 Space Systems ble Structures Using System Realization Re-
dundancy G93-076
Trajectories and Tracking Systems First-Order Models for Satellite Survivability Control of Nonlinear Structural Dynamic Sys-
Optimization G93-072 tems: Chaotic Vibrations G93-073
Exact Conversion of Earth-Centered, Earth- Automatic Spacecraft Docking Using Computer
Model Reduction of Mechanical Systems
Fixed Coordinates to Geodetic Coordinates Vision-Based Guidance and Control Tech-
G93-063
G93-056 niques G93-041
Experimental Study of Robustness in Adaptive
Propulsion Spacecraft Attitude Determination Control for Large Flexible Structures G93-002
Experiments in Multivariable Adaptive Control
Optimal Periodic Control for Spacecraft Pointing of a Large Flexible Structure G93-001
Electric and Advanced Space Propulsion
and Attitude Determination G93-169
Nutational Stability and Core Energy of a Qua- Structural Design
Equation for Optimal Power-Limited Spacecraft
sirigid Gyrostat G93-102
Trajectories G93-057
Star Trackers, Star Catalogs, and Attitude Deter- Eigenvalue and Eigenvector Derivatives of Non-
mination: Probabilistic Aspects of System De- linear Eigenproblems G93-123
Space Technology sign G93-077
Two-Axis Dry Tuned-Rotor Gyroscopes: Design Structural Dynamics and
Aerobraking Configurations/ and Technology G93-066 Characterization
Aerothermodynamics Attitude Dynamics and Control of a Vertical In-
terferometric Radar Tethered Altimeter Component Modes Damping Assignment Meth-
Six-Degree-of-Freedom Guidance and Control G93-038 odology for Articulated, Multiflexible Body
Analysis of Mars Aerocapture G93-164
Structures G93-172
Spacecraft Communication
Aerobraking Flight Mechanics Block-Diagonal Equations for Multibody Elasto-
GSTAR III Attitude for Inclined Geostationary dynamics with Geometric Stiffness and Con-
Six-Degree-of-Freedom Guidance and Control Orbit G93-039 straints G93-171
Analysis of Mars Aerocapture G93-164 Feedback Gain Sensitivities of Closed-Loop
General Adaptive Guidance Using Nonlinear Spacecraft Propulsion System Integration Modal Parameters of Controlled Structures
Programming Constraint-Solving Methods G93-137
G93-080 Fuel-Optimal Slewing of an Experimental Minimum Time Puise Response Based Control
Guidance for an Aerocapture Maneuver Hinged-Free Beam G93-180 of Flexible Structures G93-135
G93-078 Fuel-Optimal Propulsive Reboost of Flexible Consistent-Mode Indicator for the Eigensystem
Spacecraft G93-043 Realization Algorithm G93-132
Mission Design and Analysis
Nonrecursive Order N Formulation of Multibody
Structural Mechanics and Dynamics G93-130
First-Order Models for Satellite Survivability
Optimization G93-072 Materials Sensor Failure Detection and Isolation in Flexi-
Stable Orbits About the Martian Moons ble Structures Using System Realization Re-
G93-068 Dynamic Model Analysis dundancy G93-076
Stationkeeping Method for Libration Point Tra- Sensitivity-Based Characterization and Optimi-
jectories G93-021 Maneuver and Vibration Control of Hybrid Co- zation of Viscoelastically Damped Honey-
ordinate Systems Using Lyapunov Stability comb Structures G93-075
Mission Trajectories (Earth and Theory G93-106 Control of Nonlinear Structural Dynamic Sys-
Interplanetary) tems: Chaotic Vibrations G93-073
Flexible and Active Structures Active Vibration Damping of the Space Shuttle
Differential Angle Tracking for Close Geosta- Remote Manipulator System G93-040
tionary Satellites G93-166 Inversion-Based Nonlinear Control of Robot
Autonomous Position and Velocity Determina- Arms with Flexible Links G93-181 Structural Finite Elements
tion in Interplanetary Space G93-126 Fuel-Optimal Slewing of an Experimental
Stable Orbits About the Martian Moons Hinged-Free Beam G93-180 Nonrecursive Order N Formulation of Multibody
G93-068 Buckling Control of a Flexible Beam Using Pi- Dynamics G93-130
Optimal Impulsive Intercept with Low-Thrust ezoelectric Actuators G93-153
Rendezvous Return G93-067 Controllability and Observability of Flexible
Equation for Optimal Power-Limited Spacecraft Structures with Proof-Mass Actuators Structural Modeling
Trajectories G93-057 G93-138
Exact Conversion of Earth-Centered, Earth- Feedback Gain Sensitivities of Closed-Loop Component Modes Damping Assignment Meth-
Fixed Coordinates to Geodetic Coordinates Modal Parameters of Controlled Structures odology for Articulated, Multiflexible Body
G93-056 G93-137 Structures G93-172
Stationkeeping Method for Libration Point Tra- Minimum Time Pulse Response Based Control
jectories G93-021 of Flexible Structures G93-135 Structural Optimization
Piezoelectric Actuator Design for Vibration Sup-
Space Experiments pression: Placement and Sizing G93-133 Disturbance Model for Control/Structure Opti-
Consistent-Mode Indicator for the Eigensystem mization with Full State Feedback G93-081
Refinements in Determining Satellite Drag Coef- Realization Algorithm G93-132 Sensitivity-Based Characterization and Optimi-
ficients: Method for Resolving Density Dis- Recursive Dynamics Algorithm for Multibody zation of Viscoelastically Damped Honey-
crepancies G93-069 Systems with Prescribed Motion G93-129 comb Structures G93-075
J. GUIDANCE, VOL. 16, NO. 6: 1993 INDEX
Author Index
Achaibou, A. K., G93-096, Dorato, P., G93-055 Kumar, R. R., G93-108, G93-183 Napolitano, M. R., G93-159
G93-186 Durham, W. C., G93-112 Kung, M.-C., G93-064 Nassirharand, A., G93-061
Adams, R. J., G93-146 Dvornychenko, V. N., G93-187 Kurdila, A. J., G93-130 Nayfeh, A. H., G93-083
Agrawal, B. N., G93-101 Eisler, G. R., G93-060 Lacchini, C., G93-066 Naylor, S., G93-159
Ahmed, A., G93-001, G93-002 Elliott, K. B., G93-132 Lan, C. E., G93-033 Netzer, E., G93-170
Al-Sunni, F. M., G93-095 Ellis, S. R., G93-019, G93-020 Lawden, D. F., G93-089 Nissim, E., G93-179
Alt, T. R., G93-109 Engelland, S. A., G93-158 Lee, A.-C., G93-107 Ochi, Y., G93-015
Ambrosius, B. A. C., G93-027 Fabunmi, J. A., G93-137 Lee, A. Y., G93-172 Ohtsuka, T., G93-006
Amirouche, F. M. L., G93-013 Fleurisson, E. J., G93-022 Lee, S., G92-218 Ozoroski, L., G93-118
Anderson, M. R., G93-086, Fox, S. M., G93-028 Lee, S. W., G93-065 Paden, B., G93-133, G93-153
G93-111 Frarklin, J. A., G93-158 Lee, Y. J., G93-003, G93-173 Paielli, R. A., G93-025
Andrisani, D., II, G93-092 Frazier, W. G., G93-008 Lembeck, C. A., G93-067 Pappa, R. S., G93-132
Atencio, A., Jr., G93-011 Fujii, H., G93-006, G93-178 Lesch, K., G93-124 Park, M. S., G93-151
Baba, Y., G93-079 Gao, C., G91-137, G93-114 Lewis, F. L., G93-095 Parvez, S. A., G93-039
Bach, R. E., G93-025 Garg, S., G93-115 Liebst, B. S., G93-104 Patel, Y., G93-016
Bagley, R. L., G93-104 Garrard, W. L., G93-010 Lim, K. B., G93-138, G93-177 Patton, R. J., G93-016
Banda, S. S., G93-145, G93-146 Gaudreault, M. L. D., G93-104 Lin, C. E., G93-036 Pernicka, H. J., G93-021
Banerjee, A. K., G93-059, Gawronski, W., G93-138 Lin, C.-F., G93-053 Phan, M., G93-046, G93-047, G93-
G93-171 Giesy, D. P., G93-177 Lin, C.-L., G93-152 131, G93-139
Bang, H., G93-106 Gilbert, M. G., G93-040 Lin, K.-C., G91-137 Pines, D. J., G93-022
Bashirov, A. E., G93-155 Gorder, P. J., G93-116 Linse, D. J., G93-161 Pittelkau, M. E., G93-169
Bauer, F., G93-168 Grassi, M., G93-038 Liu, C.-Y., G93-064 Piou, J. E., G93-110
Bayard, D. S., G93-001, G93-002 Gribble, J. J., G93-117 Liu, K., G93-045 Powell, J. D., G93-023
Bayo, E., G93-133 Grunwald, A. J., G93-019, Liu, Q., G93-154, G93-168 Powell, R. W., G93-164
Beal, T. R., G93-018 G93-020, G93-051 Liu, Z.-s., G93-123 Prasad, J. V. R., G93-012
Belbruno, E. A., G93-119 Gueler, R., G93-105 Long, L., G93-118 Prussing, J. E., G93-057,
Ben-Asher, J. Z., G93-094 Gurley, J. G., G93-078 Longman, R. W., G93-046, G93-067, G93-165
Bennighof, J. K., G93-135 Ha, C., G93-082 G93-047, G93-127, G93-131, Psiaki, M. L., G93-028
Benshabat, D. G., G93-007 Hall, C. D., G93-121 G93-175 Quinn, R. D., G93-099
Berg, M. C., G93-082, G93-142 Hall, E. K., I, G93-121, G93-073 Low, E., G93-010 Rao, M. N., G93-091
Bernstein, D. S., G93-122 Hall, S. R., G93-125 Lu, J., G93-004 Redmond, J., G93-030, G93-043
Betts, J. T., G93-009 Han, S.-D., G93-062 Lu, P., G93-113, G93-147 Rodriguez, G., G93-129
Bikdash, M., G93-083 Hanagud, S. V., G93-073 Lu, P.-J., G93-017 Roenneke, A. J., G93-143
Bilimoria, K. D., G93-070 Hesper, E. T., G93-027 Luke, R. A., G93-074 Rokhsaz, K., G93-144
Bishop, R. H., G93-174 Hess, R. A., G91-137, G93-011, Luo, J., G93-033 Ross, I. M., G93-102
Bocvarov, S., G93-034, G93-103 G93-114, G93-116, Lutze, F. H., G93-034, G93-103 Sachs, G., G93-087, G93-124
Braun, R. D., G93-164 Ho, C.-C. J., G93-041 Ly, U.-L., G93-082 Saif, M., G93-156
Breida, M., G93-063 Hollkamp, J. J., G93-084 Lyde, T. L., G93-076 Schenk, A., G93-132
Brogan, W. L., G93-062 Horta, L. G., G93-046, G93-047, Maghami, P. G., G93-044 Schlack, A. L., G93-100
Burken, J. J., G93-162 G93-175 Malsbury, T., G93-011 Schmidt, G. C., G93-052
Burrows, S. P., G93-016 Howard, M. L., G93-072 Mansour, W. M., G93-066 Scott, M. A., G93-040
Byers, R. M., G93-071 Howe, R. M., G93-049, G93-079 Mapar, J., G93-024 Scott, P. R., G93-026
Byrns, E. V., Jr., G93-014 Howell, K. C., G93-021 Martin, M., G93-080 Sehitoglu, H., G93-185
Calise, A. J., G93-014, G93-085 Hsu, S.-C., G93-149 Mason, G. S., G93-142 Seywald, H., G93-108, G93-120,
Chaid, K. Q., G93-090 Huang, L., G93-028 Mason, P. A. C., G93-184 G93-183
Chait, Y., G93-007, G93-151 Huang, L.-J., G93-017 Matsuda, K., G93-178 Shamma, J. S., G93-037
Chang, C.-O., G93-032 Huang, N. C., G93-189 Maughmer, M., G93-118 Shareef, N. H., G93-013
Chang, S.-H. M., G93-135 Huffman, W. P., G93-009 McClamroch, N. H., G93-041 Shen, C.-L., G93-055
Chen, C. L., G93-159 Hull, D. G., G93-060 McGrath, J. M., G93-141 Shuster, M. D., G93-058
Chen, C.-W., G93-139 Humi, M., G93-029 McLaren, M. D., G93-081 Siciliano, B., G93-181
Chen, D., G93-148 Hutchins, R. G., G93-134 Mehlhorn, R., G93-087 Silverberg, L., G93-030,
Chen, J.-C., G93-064 Hyland, D. C., G93-127 Meirovitch, L., G93-136 G93-043, G93-180
Chen, M. P., G93-032 Idan, M., G93-048 Menon, P. K. A., G92-027 Sim, E., G93-065
Chen, S.-h., G93-123 Igusa, T., G93-182 Menon, R. G., G93-130 Singh, T., G93-167
Chen, S.-T., G93-107 th, C.-H. C., G93-001, G93-002 Meressi, T., G93-133, G93-153 Sinha, R., G93-154
Chiang, S.-M., G93-064 Imado, F., G93-042 Merrill, W., G93-115 Skalecki, L., G93-080
Chuang, C.-H., G93-150 Irwin, R. D., G93-008 Meyer, J. L., G93-180 Skelton, R. E., G93-045
Cicci, D. A., G93-157 Jabbari, F., G93-109 Miller, J. K., G93-119 Slater, G. L., G93-081
Clements, J. C., G93-054 Jahangir, E., G93-049 Mingori, D. L., G93-005 Sobel, K. M., G93-110
Clemmons, P., G93-085 Jain, A., G93-129 Misra, P. K., G93-039 Spanos, J. T., G93-005
Cliff, E. M., G93-034, G93-083, Jones, B. L., G93-174 Mittal, M., G93-012 Sparks, A., G93-145, G93-146
G93-103, G93-120, G93-183 Joshi, S. M., G93-044 Miyazawa, Y., G93-035 Speyer, J. L., G93-003, G93-173
Cloutier, J. R., G93-037, Juang, J.-N., G93-046, G93-047, Moccia, A., G93-038 Stabb, M. C., G93-100
G93-053 G93-131, G93-139, G93-175 Moe, K., G93-069 Steck, J. E., G93-144
Cornwell, P. J., G93-143 Junkins, J. L., G92-218, Moe, M. M., G93-069 Stengel, R. F., G93-160, G93-161
Coverstone-Carroll, V., G93-165 G93-106, G93-127, G93-188 Moerder, D. D., G93-085 Stetson, J. B., Jr., G93-098
Crassidis, J. L., G93-141, Kane, T. R., G93-059, G93-170 Molnar, J., G93-075 Straussfogel, D., G93-118
G93-184 Kawakami, Y., G93-031 Mook, D. J., G93-141, G93-184 Subramaniam, M., G93-135
Da, R., G93-140 Kawase, S., G93-166 Mora-Camino, F., G93-096, G93- Sulla, J. L., G93-047
De Luca, A., G93-181 Kim, E. T., G93-092 186 Sunkel, J. W., G93-130
de Matteis, G., G93-128 Kline-Schoder, R. J., G93-023 Mukherjee, R., G93-148, Sworder, D. D., G93-134
Demeo, M. E., G93-040 Kodiyalam, S., G93-075 G93-188 Takahashi, M. D., G93-088
Devasia, S., G93-133 Kohn, S., G93-051 Mulgund, S. S., G93-160 Tan, D. G. H., G93-026
1208 J. GUIDANCE, VOL. 16, NO. 6: 1993 INDEX
Tanaka, H., G93-031 Wallace, S. D., G93-069 Wie, B., G93-004, G93-070, G93- Yedavalli, R. K., G93-163
Troudet, T., G93-115 Wang, R.-J., G93-093 154, G93-168 Yeung, K. S., G93-090
Vadali, S. R.,, G93-071, G93-167 Wang, S. J., G93-001, G93-002 Wiesel, W. E., G93-068 Young, J.-S., G93-036
Vedder, J. D., G93-077, G93-126 Wang, W.-J., G93-093 Wise, K. A., G93-050 Yousuff, A., G93-063
Vetrella, S., G93-038 Wang, Y. W., G93-122 Wu, S.-C., G93-131 Yuan, P.-J., G93-149
Vojak, R., G93-134 Warnitchai, P., G93-182 Xie, M., G93-013 Yunis, I. S., G93-099
von Flotow, A. H., G93-022, Warren, W., G93-004 Xu, K., G93-182 Zhu, J., G93-056
G93-105 Wei, Y., G93-055 Yamaguchi, M., G93-079 Zimmerman, D. C., G93-076
Vos, D. W., G93-105 Weiss, H., G93-097 Yang, C., G93-053
Wakker, K. F., G93-027 Wereley, N. M., G93-125 Yang, J.-S., G93-176