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<!DOCTYPE HTML PUBLIC "-//W3C//DTD HTML 3.2//EN"> <HTML> <HEAD> <title>Author Index</title> </HEAD> <BODY BGCOLOR="ffffff"> <h1> 1995 AAS/AIAA Astrodynamics Specialists Conference Author Index</h1> <dl> <dt>Agrawal, B. N. <dd><a href="abstracts/95-321.html"><b>Active Vibration Control of a Deploying Appendage Using Piezoceramic Sensors and Actuators</b></a> <dt>Alfriend, K. T. <dd><a href="abstracts/95-351.html"><b>Attitude and Orbit Estimation of a Tether Satellite System</b></a> <dt>Alfriend, K. T. <dd><a href="abstracts/95-416.html"><b>A Magnetic Attitude Control System for Sun Pointing Satellites</b></a> <dt>Alonso, R. A. <dd><a href="abstracts/95-302.html"><b>Magnetometer Calibration for the First Argentine Spacecraft</b></a> <dt>Amirouche, F. <dd><a href="abstracts/95-394.html"><b>Treatment of Inelastic Phenomena in Multibody Dynamics</b></a> <dt>Anderson, D. S. <dd><a href="abstracts/95-410.html"><b>Inertial Propagation of an Earth-Fixed Point Using Perturbed Kepler Algorithms</b></a> <dt>Angrilli, F. <dd><a href="abstracts/95-355.html"><b>Non-Linear Dissipative Effects in Tethered Multilayer Systems for Space Missions</b></a> <dt>Anselmo, L. <dd><a href="abstracts/95-348.html"><b>The Contribution of Past Fragmentation Events to the Uncatalogued Orbital Debris Population</b></a> <dt>Bainum, P. M. <dd><a href="abstracts/95-320.html"><b>Actuator/Sensor Placement Using Degree of Controllability and Observability for Digitally Controlled Orbiting Platforms</b></a> <dt>Baldassini, J. <dd><a href="abstracts/95-384.html"><b>The Calibration and Characterization of IRAS Metric Resident Space Object Detections</b></a> <dt>Banerjee, A. K. <dd><a href="abstracts/95-318.html"><b>Minimum Time Fuel Efficient Maneuver of Flexible Spacecraft with Vibration Amplitude Constraint</b></a> <dt>Banerjee, A. K. <dd><a href="abstracts/95-398.html"><b>Recursive Formulation in Multibody Elastodynamics: Simulation and Ground Test</b></a> <dt>Barker, W. N. <dd><a href="abstracts/95-311.html"><b>Earth Gravitational Model Error Budget for Space Control</b></a> <dt>Barker, W. N. <dd><a href="abstracts/95-432.html"><b>The Accuracy of General Perturbations and Semianalytic Satellite Ephemeris Theories</b></a> <dt>Barnds, W. J. <dd><a href="abstracts/95-351.html"><b>Attitude and Orbit Estimation of a Tether Satellite System</b></a> <dt>Bartler, T. <dd><a href="abstracts/95-407.html"><b>Chaos in Artificial Satellite Motion Due to Third-Body Effects</b></a> <dt>Beck, R. A. <dd><a href="abstracts/95-373.html"><b>Complex Analytic Solutions for a Spinning Rigid Body Under Constant Transverse Torques</b></a> <dt>Beck, R. A. <dd><a href="abstracts/95-414.html"><b>Annihilation of Transverse Velocity Bias During Spinning-Up Maneuvers</b></a> <dt>Beckman, M. <dd><a href="abstracts/95-388.html"><b>Orbit Determination Support for the Clementine Mission During Lunar Orbit Phase</b></a> <dt>Belbruno, E. <dd><a href="abstracts/95-403.html"><b>The Dynamical Mechanism of Ballistic Lunar Capture Transfer in the Four-Body Problem and Weak Stability Boundaries</b></a> <dt>Bender, D. F. <dd><a href="abstracts/95-380.html"><b>Multiple Encounter Missions with the Trojan and Main Belt Asteroids</b></a> <dt>Bergamaschi, S. <dd><a href="abstracts/95-352.html"><b>TSS-1 Tensiometer Data Analysis</b></a> <dt>Bertiger, W. <dd><a href="abstracts/95-372.html"><b>GPS-LIKE TRACKING (GLT) OF GEOSYNCHRONOUS SATELLITES: ORBIT DETERMINATION RESULTS FOR TDRS and INMARSAT</b></a> <dt>Bhaskaran, S. <dd><a href="abstracts/95-387.html"><b>Demonstration of Autonomous Orbit Determination Around Small Bodies</b></a> <dt>Bhat, R. S. <dd><a href="abstracts/95-366.html"><b>An Analysis of the TOPEX/Poseidon Operational Orbit: Observed Variations and Why</b></a> <dt>Bishop, R. H. <dd><a href="abstracts/95-418.html"><b>Indirect Adaptive Nonlinear Attitude Control and Momentum Management of Spacecraft Using Feedback Linearization</b></a> <dt>Boelitz, C. <dd><a href="abstracts/95-344.html"><b>Orbit Analysis Software Survey</b></a> <dt>Bolender, L. <dd><a href="abstracts/95-339.html"><b>SAFER Mass Properties Determination: Results from On-Orbit Data</b></a> <dt>Braun, R. D. <dd><a href="abstracts/95-379.html"><b>Mars Pathfinder Atmospheric Entry Trajectory Design</b></a> <dt>Bright, L. E. <dd><a href="abstracts/95-307.html"><b>Design of High-Accuracy Multiple Flyby Trajectories Using Constrained Optimization</b></a> <dt>Broucke, R. A. <dd><a href="abstracts/95-406.html"><b>Long-Term Lunar Effects on High-Altitude Earth Satellites</b></a> <dt>Byrnes, D. V. <dd><a href="abstracts/95-307.html"><b>Design of High-Accuracy Multiple Flyby Trajectories Using Constrained Optimization</b></a> <dt>Byrnes, D. V. <dd><a href="abstracts/95-315.html"><b>Dactyl Orbit Determination Analysis</b></a> <dt>Byrnes, D. V. <dd><a href="abstracts/95-381.html"><b>Navigation Strategy for the Galileo Jupiter Encounter and Orbital Tour</b></a> <dt>Caleffi, T. <dd><a href="abstracts/95-454.html"><b>Monte Carlo Performance Analysis of the Brazilian Satellite Launcher Vehicle Last Stage</b></a> <dt>Cangahuala, L. A. <dd><a href="abstracts/95-368.html"><b>TOPEX/Poseidon Precision Orbit Determination: 'Quick-Look' Operations with GPS and SLR Data</b></a> <dt>Cappellari, J. O. <dd><a href="abstracts/95-441.html"><b>Goddard Space Flight Center Flight Dynamics Division Ascent Acquisition Support of Space Shuttle Rendezvous Missions</b></a> <dt>Carpenter, D. <dd><a href="abstracts/95-409.html"><b>A General Purpose Family of Numerical Integration Procedures for Astrodynamics Applications</b></a> <dt>Carrico, J. <dd><a href="abstracts/95-323.html"><b>Operational Use of Swingby-an Interactive Trajectory Design and Maneuver Planning Tool - for Mission to the Moon and Beyond</b></a> <dt>Carter, T. E. <dd><a href="abstracts/95-452.html"><b>Optimal Rendezvous of a Spacecraft with Multiple Power-Limited Thrusters Having Upper and Lower Bounds</b></a> <dt>Casali, S. J. <dd><a href="abstracts/95-311.html"><b>Earth Gravitational Model Error Budget for Space Control</b></a> <dt>Casalino, D. <dd><a href="abstracts/95-305.html"><b>Indirect Optimization Method for Round-Trip Mars Trajectories</b></a> <dt>Casalino, L. <dd><a href="abstracts/95-450.html"><b>Optimal Aeroassisted GEO-to-LEO Transfer by an Indirect Method</b></a> <dt>Casey, J. <dd><a href="abstracts/95-386.html"><b>Application of Precision Orbit Determination Techniques to Tracking and Prediction of Multiple Space Objects</b></a> <dt>Cassell, C. R. <dd><a href="abstracts/95-405.html"><b>LAMDA: A Software Tool for Lunar-Assist Escape Missions</b></a> <dt>Cefola, P. J. <dd><a href="abstracts/95-428.html"><b> Parallel Orbit Propagation and the Analysis of Satellite Constellations </b></a> <dt>Cefola, P. J. <dd><a href="abstracts/95-340.html"><b>Refinement of a Sun-Synchronous, Critically Inclined Orbit for a Global Personal Communications System</b></a> <dt>Cefola, P. J. <dd><a href="abstracts/95-371.html"><b>The Determination of Precision Mean Element Sets from GPS Receiver On-board Navigation Solutions</b></a> <dt>Chan, J. C. <dd><a href="abstracts/95-312.html"><b>Precision Orbit Determination and Gravity Field Improvement Derived From TDRSS Orbit Determination</b></a> <dt>Chao, C. C. <dd><a href="abstracts/95-333.html"><b>The Optimization of Initial Inclination for a Desired Sun-synchronous Orbit</b></a> <dt>Chao, C. C. <dd><a href="abstracts/95-343.html"><b>A Prototype Onboard Processor for LEO Control Using a GPS Receiver</b></a> <dt>Chen, Y.-H. <dd><a href="abstracts/95-423.html"><b>Flight Envelopes for Hypersonic Aero-Rendezvous at Various Constant Altitudes</b></a> <dt>Chern, J.-S. <dd><a href="abstracts/95-423.html"><b>Flight Envelopes for Hypersonic Aero-Rendezvous at Various Constant Altitudes</b></a> <dt>Chern, J.-S. <dd><a href="abstracts/95-449.html"><b>Effect of Laser Power Limitation on Single-Stage to GEO Launch</b></a> <dt>Chernuka, M. W. <dd><a href="abstracts/95-374.html"><b>Power Flow Finite Element Analysis of Flexible Space Structures</b></a> <dt>Cho, S. <dd><a href="abstracts/95-316.html"><b>Attitude and Configuration Control of Flexible Multi-Body Spacecraft</b></a> <dt>Christensen, E.J. <dd><a href="abstracts/95-368.html"><b>TOPEX/Poseidon Precision Orbit Determination: 'Quick-Look' Operations with GPS and SLR Data</b></a> <dt>Chuba, W. A. <dd><a href="abstracts/95-385.html"><b>Stochastic Clock Model for Definitive Sequential Orbit Determination</b></a> <dt>Cicci, D. A. <dd><a href="abstracts/95-350.html"><b>Orbit Determination of a Tethered Satellite</b></a> <dt>Cieslak, C. J. <dd><a href="abstracts/95-442.html"><b>Operational Maneuver Support for Low-Earth Orbiting Spacecraft at the Goddard Space Flight Center Flight Dynamics Division</b></a> <dt>Cochran, J. E. <dd><a href="abstracts/95-316.html"><b>Attitude and Configuration Control of Flexible Multi-Body Spacecraft</b></a> <dt>Coffey, S. L. <dd><a href="abstracts/95-351.html"><b>Attitude and Orbit Estimation of a Tether Satellite System</b></a> <dt>Coffey, S. L. <dd><a href="abstracts/95-426.html"><b>An Analytic Orbit Propagation Program for Satellite Catalog Maintenance</b></a> <dt>Colasurdo, G. <dd><a href="abstracts/95-305.html"><b>Indirect Optimization Method for Round-Trip Mars Trajectories</b></a> <dt>Colasurdo, G. <dd><a href="abstracts/95-450.html"><b>Optimal Aeroassisted GEO-to-LEO Transfer by an Indirect Method</b></a> <dt>Conway, D. <dd><a href="abstracts/95-323.html"><b>Operational Use of Swingby-an Interactive Trajectory Design and Maneuver Planning Tool - for Mission to the Moon and Beyond</b></a> <dt>Conway, B. <dd><a href="abstracts/95-401.html"><b>Optimal Low-Thrust Three-Body Earth-Moon Orbit Transfers</b></a> <dt>Cordelli, A. <dd><a href="abstracts/95-348.html"><b>The Contribution of Past Fragmentation Events to the Uncatalogued Orbital Debris Population</b></a> <dt>Coverstone-Carroll, V. <dd><a href="abstracts/95-413.html"><b>Detumbling and Reorienting Underactuated Rigid Spacecraft</b></a> <dt>Cox, C. <dd><a href="abstracts/95-312.html"><b>Precision Orbit Determination and Gravity Field Improvement Derived From TDRSS Orbit Determination</b></a> <dt>Cox, E. L. <dd><a href="abstracts/95-442.html"><b>Operational Maneuver Support for Low-Earth Orbiting Spacecraft at the Goddard Space Flight Center Flight Dynamics Division</b></a> <dt>Crouse, P. <dd><a href="abstracts/95-424.html"><b>Result of a Feasibility Study on the Use of High Lift to Drag Vehicles for Aerocapture for Non-Optimized Trajectories</b></a> <dt>Culp, R. D. <dd><a href="abstracts/95-345.html"><b>An Optical Analysis of the 6470 Hypervelocity Debris Fragments</b></a> <dt>Culp, R. D. <dd><a href="abstracts/95-347.html"><b>The Investigation of Space Debris Generation and Associated Long-Term Effects in the Geosynchronous Region</b></a> <dt>D'Amario, L. A. <dd><a href="abstracts/95-315.html"><b>Dactyl Orbit Determination Analysis</b></a> <dt>D'Amario, L. A. <dd><a href="abstracts/95-381.html"><b>Navigation Strategy for the Galileo Jupiter Encounter and Orbital Tour</b></a> <dt>Da Forno, R. <dd><a href="abstracts/95-355.html"><b>Non-Linear Dissipative Effects in Tethered Multilayer Systems for Space Missions</b></a> <dt>Danielson, D. A. <dd><a href="abstracts/95-431.html"><b>Comparison of Orbit Propagators in the Research and Development Goddard Trajectory Determination System (R & D GTDS). Part I: Simulated Data</b></a> <dt>Davis, W. S. <dd><a href="abstracts/95-303.html"><b>In-Flight Calibration of the Field of View Distortion for Spacecraft Attitude Sensors</b></a> <dt>de Carufel, J. <dd><a href="abstracts/95-358.html"><b>Single and Dual Arm Robot Control for Free and Contact Motion</b></a> <dt>DeLazzari, A. <dd><a href="abstracts/95-352.html"><b>TSS-1 Tensiometer Data Analysis</b></a> <dt>Denn, F. M. <dd><a href="abstracts/95-329.html"><b>Orbital Analysis of LidarSat for Synergistic Measurements With the Earth Observing System (EOS) Satellite</b></a> <dt>Der, G. J. <dd><a href="abstracts/95-420.html"><b>Runge-Kutta Integration Methods for Trajectory Propagation Revisited</b></a> <dt>Dorairajan, V. <dd><a href="abstracts/95-448.html"><b>Combined Launch Trajectory and Vehicle Design Optimization</b></a> <dt>Draim, J. <dd><a href="abstracts/95-340.html"><b>Refinement of a Sun-Synchronous, Critically Inclined Orbit for a Global Personal Communications System</b></a> <dt>Dunham, D. W. <dd><a href="abstracts/95-378.html"><b>NEAR-Eros 1996: Mission Overview and Trajectory Design</b></a> <dt>Dyar, W. D. <dd><a href="abstracts/95-431.html"><b>Comparison of Orbit Propagators in the Research and Development Goddard Trajectory Determination System (R & D GTDS). Part I: Simulated Data</b></a> <dt>Eke, F. O. <dd><a href="abstracts/95-335.html"><b>Effect of Mass Variation on the Dynamics of Mechanical Systems</b></a> <dt>Ely, T. A. <dd><a href="abstracts/95-341.html"><b>East-West Stationkeeping of Satellite Orbits with Resonant Tesseral Harmonics</b></a> <dt>Ericsson, A. J. <dd><a href="abstracts/95-320.html"><b>Actuator/Sensor Placement Using Degree of Controllability and Observability for Digitally Controlled Orbiting Platforms</b></a> <dt>Farinella, P. <dd><a href="abstracts/95-348.html"><b>The Contribution of Past Fragmentation Events to the Uncatalogued Orbital Debris Population</b></a> <dt>Farquhar, R. W. <dd><a href="abstracts/95-378.html"><b>NEAR-Eros 1996: Mission Overview and Trajectory Design</b></a> <dt>Fell, P. <dd><a href="abstracts/95-301.html"><b>A Preliminary Study of Satellite Attitude Determination For Future Landsat Spacecraft</b></a> <dt>Flashner, H. <dd><a href="abstracts/95-308.html"><b>A Conceptual Automatic Landing System for Spacecraft Using Pulse-Modulated Propulsion</b></a> <dt>Folta, D. C. <dd><a href="abstracts/95-323.html"><b>Operational Use of Swingby-an Interactive Trajectory Design and Maneuver Planning Tool - for Mission to the Moon and Beyond</b></a> <dt>Folta, D. C. <dd><a href="abstracts/95-325.html"><b>Evaluation of Spacecraft End-of-Life Disposal to Meet NASA Management Instruction (NMI) Guidelines</b></a> <dt>Fonte, D. J. <dd><a href="abstracts/95-431.html"><b>Comparison of Orbit Propagators in the Research and Development Goddard Trajectory Determination System (R & D GTDS). Part I: Simulated Data</b></a> <dt>Frauenholz, R. B. <dd><a href="abstracts/95-366.html"><b>An Analysis of the TOPEX/Poseidon Operational Orbit: Observed Variations and Why</b></a> <dt>Frayssinhes, E. <dd><a href="abstracts/95-334.html"><b>Designing Clusters of Satellites for Radiolocalisation Purposes</b></a> <dt>Fujimura, T. <dd><a href="abstracts/95-425.html"><b>The Low-Thrust Flyby Guidance and an Extended Optimal Spacing Rule</b></a> <dt>Gaposchkin, E. M. <dd><a href="abstracts/95-384.html"><b>The Calibration and Characterization of IRAS Metric Resident Space Object Detections</b></a> <dt>Gaposchkin, E. M. <dd><a href="abstracts/95-445.html"><b>Autonomous Visible-Band Tracking for the Midcourse Space Experiment (MSX)</b></a> <dt>Garber, A. R. <dd><a href="abstracts/95-303.html"><b>In-Flight Calibration of the Field of View Distortion for Spacecraft Attitude Sensors</b></a> <dt>Garner, G. <dd><a href="abstracts/95-324.html"><b>Satellite Tour Design at Saturn Using an Excel Spreadsheet</b></a> <dt>Gibson, G. G. <dd><a href="abstracts/95-329.html"><b>Orbital Analysis of LidarSat for Synergistic Measurements With the Earth Observing System (EOS) Satellite</b></a> <dt>Gilbreath, G. C. <dd><a href="abstracts/95-369.html"><b>Using a Single SLR Site to Validate GPS Receiver Navigation</b></a> <dt>Ginn, D. <dd><a href="abstracts/95-323.html"><b>Operational Use of Swingby-an Interactive Trajectory Design and Maneuver Planning Tool - for Mission to the Moon and Beyond</b></a> <dt>Gist, R. G. <dd><a href="abstracts/95-328.html"><b>Time Parameterization of Oval and Lemniscate Surface Trajectories</b></a> <dt>Gist, R. G. <dd><a href="abstracts/95-333.html"><b>The Optimization of Initial Inclination for a Desired Sun-synchronous Orbit</b></a> <dt>Gist, R. G. <dd><a href="abstracts/95-343.html"><b>A Prototype Onboard Processor for LEO Control Using a GPS Receiver</b></a> <dt>Glover, R. A. <dd><a href="abstracts/95-427.html"><b>Analytic Orbit Model for U.S. Naval Space Surveillance: An Overview</b></a> <dt>Glover, R. A. <dd><a href="abstracts/95-430.html"><b>Testing of Naval Space Command New Analytic Orbit Model</b></a> <dt>Good, S. M. <dd><a href="abstracts/95-442.html"><b>Operational Maneuver Support for Low-Earth Orbiting Spacecraft at the Goddard Space Flight Center Flight Dynamics Division</b></a> <dt>Gottlieb, R. G. <dd><a href="abstracts/95-412.html"><b>The Effect of Energy Parameter Selection on a Variation of Parameters Method</b></a> <dt>Graat, E.J. <dd><a href="abstracts/95-368.html"><b>TOPEX/Poseidon Precision Orbit Determination: 'Quick-Look' Operations with GPS and SLR Data</b></a> <dt>Gravseth, I. J. <dd><a href="abstracts/95-345.html"><b>An Optical Analysis of the 6470 Hypervelocity Debris Fragments</b></a> <dt>Guelman, M. <dd><a href="abstracts/95-451.html"><b>Electric Propulsion for Orbit Transfer in a Resistive Medium</b></a> <dt>Guinn, J.R. <dd><a href="abstracts/95-368.html"><b>TOPEX/Poseidon Precision Orbit Determination: 'Quick-Look' Operations with GPS and SLR Data</b></a> <dt>Haines, B. <dd><a href="abstracts/95-372.html"><b>GPS-LIKE TRACKING (GLT) OF GEOSYNCHRONOUS SATELLITES: ORBIT DETERMINATION RESULTS FOR TDRS and INMARSAT</b></a> <dt>Hall, C. D. <dd><a href="abstracts/95-337.html"><b>Parametric Excitation of Two-Rotor Gyrostats with Damping</b></a> <dt>Harrington, T. <dd><a href="abstracts/95-442.html"><b>Operational Maneuver Support for Low-Earth Orbiting Spacecraft at the Goddard Space Flight Center Flight Dynamics Division</b></a> <dt>Harrison, E. F. <dd><a href="abstracts/95-329.html"><b>Orbital Analysis of LidarSat for Synergistic Measurements With the Earth Observing System (EOS) Satellite</b></a> <dt>Hashmall, J. A. <dd><a href="abstracts/95-303.html"><b>In-Flight Calibration of the Field of View Distortion for Spacecraft Attitude Sensors</b></a> <dt>Hastrup, R. <dd><a href="abstracts/95-326.html"><b>Relay Satellite Orbit Selection Considerations for Future Robotics Missions to Explore Venus</b></a> <dt>Herman, A. L. <dd><a href="abstracts/95-401.html"><b>Optimal Low-Thrust Three-Body Earth-Moon Orbit Transfers</b></a> <dt>Hokamoto, S. <dd><a href="abstracts/95-322.html"><b>Dynamics and Control of Mobile Flexible Manipulators with Slewing and Deployable Links</b></a> <dt>Hong, Z.-C. <dd><a href="abstracts/95-423.html"><b>Flight Envelopes for Hypersonic Aero-Rendezvous at Various Constant Altitudes</b></a> <dt>Hong, Z.-C. <dd><a href="abstracts/95-449.html"><b>Effect of Laser Power Limitation on Single-Stage to GEO Launch</b></a> <dt>Hough, M. E. <dd><a href="abstracts/95-327327.html"><b>Integral Surfaces With Space-Time Coordinates In the Gravitational Field of a Rotating System</b></a> <dt>Hough, M. E. <dd><a href="abstracts/95-421.html"><b>Optimal Guidance and Nonlinear Estimation for Estimation of Accelerating Targets</b></a> <dt>Howell, K. C. <dd><a href="abstracts/95-341.html"><b>East-West Stationkeeping of Satellite Orbits with Resonant Tesseral Harmonics</b></a> <dt>Huang, Y.-C. <dd><a href="abstracts/95-338.html"><b>The Source of the Often Observed Property of Initial Convergence Followed by Divergence in Learning and Repetitive Control</b></a> <dt>Huang, Y.-C. <dd><a href="abstracts/95-419.html"><b>Frequency Response Characteristics of the Alternating Sign Learning Control Law</b></a> <dt>Hughes, P. <dd><a href="abstracts/95-.html"><b>LFSS:How Much Control Do We Need?</b></a> <dt>Hujsak, R. S. <dd><a href="abstracts/95-369.html"><b>Using a Single SLR Site to Validate GPS Receiver Navigation</b></a> <dt>Huston, R. L. <dd><a href="abstracts/95-390.html"><b>Recent Advances in Modeling Flexible Multibody Systems</b></a> <dt>Jackson, J. <dd><a href="abstracts/95-443.html"><b>Tracking and Data Relay Satellite System (TDRSS) Support of User Spacecraft Without TDRSS Transponders</b></a> <dt>Jang, H. S. <dd><a href="abstracts/95-319.html"><b>An Update on a Monotonic Learning Control Law and Some Fuzzy Logic Learning Gain Adjustment Techniques</b></a> <dt>Jassemi, R. <dd><a href="abstracts/95-358.html"><b>Single and Dual Arm Robot Control for Free and Contact Motion</b></a> <dt>Junkins, J. L. <dd><a href="abstracts/95-417.html"><b>Globally Stable Feedback Laws for Near-Minimum-Fuel and Near-Minimum-Time Pointing Maneuvers for a Landmark-Tracking Spacecraft</b></a> <dt>Kalaycioglu, S. <dd><a href="abstracts/95-358.html"><b>Single and Dual Arm Robot Control for Free and Contact Motion</b></a> <dt>Kalaycioglu, S. <dd><a href="abstracts/95-360.html"><b>Robotics Evaluation and Characterization (REACH) of the SSRMS</b></a> <dt>Kang, H. K. <dd><a href="abstracts/95-303.html"><b>In-Flight Calibration of the Field of View Distortion for Spacecraft Attitude Sensors</b></a> <dt>Kangas, J. <dd><a href="abstracts/95-367.html"><b>Statistical Performance of TOPEX/POSEIDON Prime Mission Ground and On-Board Ephemerides and Consequences for the Extended Mission</b></a> <dt>Kangas, J. <dd><a href="abstracts/95-411.html"><b>Semi-Autonomous Spacecraft On-Board Ephemeris Propagation</b></a> <dt>Kawaguchi, J. <dd><a href="abstracts/95-425.html"><b>The Low-Thrust Flyby Guidance and an Extended Optimal Spacing Rule</b></a> <dt>Kechichian, J. A. <dd><a href="abstracts/95-342.html"><b>Orbit Plane Control Strategies for Inclined Geosynchronous Satellite Constellation</b></a> <dt>Kechichian, J. A. <dd><a href="abstracts/95-422.html"><b>The Use of Nonsingular Elements In Trajectory Optimization In Terms of True Longitude</b></a> <dt>Keshmiri, M. <dd><a href="abstracts/95-354.html"><b>Control of a Chain of Flexible Bodies Using Lyapunov's Stability Theory</b></a> <dt>Kirhofer, W. E. <dd><a href="abstracts/95-381.html"><b>Navigation Strategy for the Galileo Jupiter Encounter and Orbital Tour</b></a> <dt>Kirk, C. <dd><a href="abstracts/95-397.html"><b>Slewing Dynamics and Vibration Control of Flexible Space Shuttle Remote Manipulator</b></a> <dt>Kluever, C. A. <dd><a href="abstracts/95-399.html"><b>Optimal Earth-Moon Trajectories Using Nuclear Electric Propulsion</b></a> <dt>Knowles, S. H. <dd><a href="abstracts/95-429.html"><b>A Comparison of Geocentric Propagators for Operational Use</b></a> <dt>Lane, M. T. <dd><a href="abstracts/95-384.html"><b>The Calibration and Characterization of IRAS Metric Resident Space Object Detections</b></a> <dt>Langlois, B. <dd><a href="abstracts/95-361.html"><b>A Trajectory Planning and Object Avoidance System for Kinematically Redundant Manipulators: An Experimental Evaluation</b></a> <dt>Lansard, E. <dd><a href="abstracts/95-334.html"><b>Designing Clusters of Satellites for Radiolocalisation Purposes</b></a> <dt>Lee, A. <dd><a href="abstracts/95-393.html"><b>Component Model Reduction Methodology For Articulated Multi-Flexible-Body Structure</b></a> <dt>Lemoine, F. G. <dd><a href="abstracts/95-312.html"><b>Precision Orbit Determination and Gravity Field Improvement Derived From TDRSS Orbit Determination</b></a> <dt>Lemoine, F. G. <dd><a href="abstracts/95-313.html"><b>Results from the Clementine Lunar Geodesy Investigation</b></a> <dt>Lewis, M. <dd><a href="abstracts/95-424.html"><b>Result of a Feasibility Study on the Use of High Lift to Drag Vehicles for Aerocapture for Non-Optimized Trajectories</b></a> <dt>Lichten, S. <dd><a href="abstracts/95-372.html"><b>GPS-LIKE TRACKING (GLT) OF GEOSYNCHRONOUS SATELLITES: ORBIT DETERMINATION RESULTS FOR TDRS and INMARSAT</b></a> <dt>Liu, J.-M. <dd><a href="abstracts/95-449.html"><b>Effect of Laser Power Limitation on Single-Stage to GEO Launch</b></a> <dt>Longman, R. W. <dd><a href="abstracts/95-319.html"><b>An Update on a Monotonic Learning Control Law and Some Fuzzy Logic Learning Gain Adjustment Techniques</b></a> <dt>Longman, R. W. <dd><a href="abstracts/95-338.html"><b>The Source of the Often Observed Property of Initial Convergence Followed by Divergence in Learning and Repetitive Control</b></a> <dt>Longman, R. W. <dd><a href="abstracts/95-376.html"><b>The Use of the Euler Operator in Learning and Repetitive Control</b></a> <dt>Longman, R. W. <dd><a href="abstracts/95-377.html"><b>Use of Non-Causal Digital Signal Processing in Learning and Repetitive Control</b></a> <dt>Longman, R. W. <dd><a href="abstracts/95-419.html"><b>Frequency Response Characteristics of the Alternating Sign Learning Control Law</b></a> <dt>Longuski, J. M. <dd><a href="abstracts/95-306.html"><b>V� Leveraging for Interplanetary Missions: Multiple - Revolution Orbit Techniques</b></a> <dt>Longuski, J. M. <dd><a href="abstracts/95-373.html"><b>Complex Analytic Solutions for a Spinning Rigid Body Under Constant Transverse Torques</b></a> <dt>Longuski, J. M. <dd><a href="abstracts/95-414.html"><b>Annihilation of Transverse Velocity Bias During Spinning-Up Maneuvers</b></a> <dt>Longuski, J. M. <dd><a href="abstracts/95-353.html"><b>A General Approach to Aerobraking Tether Design</b></a> <dt>Lundberg, J. B. <dd><a href="abstracts/95-408.html"><b>Mitigation of Orbit Errors Resulting from the Numerical Integration Across Shadow Boundaries</b></a> <dt>Luthcke, S. B. <dd><a href="abstracts/95-312.html"><b>Precision Orbit Determination and Gravity Field Improvement Derived From TDRSS Orbit Determination</b></a> <dt>Lynch, J. P. <dd><a href="abstracts/95-441.html"><b>Goddard Space Flight Center Flight Dynamics Division Ascent Acquisition Support of Space Shuttle Rendezvous Missions</b></a> <dt>Ma, D.-M. <dd><a href="abstracts/95-330.html"><b>Low Earth Orbit Constellations Design with Good Dilution of Precision</b></a> <dt>Maher, M. <dd><a href="abstracts/95-443.html"><b>Tracking and Data Relay Satellite System (TDRSS) Support of User Spacecraft Without TDRSS Transponders</b></a> <dt>Mao, T. C. <dd><a href="abstracts/95-335.html"><b>Effect of Mass Variation on the Dynamics of Mechanical Systems</b></a> <dt>March, L. <dd><a href="abstracts/95-441.html"><b>Goddard Space Flight Center Flight Dynamics Division Ascent Acquisition Support of Space Shuttle Rendezvous Missions</b></a> <dt>Markopoulos, N. <dd><a href="abstracts/95-453.html"><b>Power-Limited Transfers Between Two Coplanar Conics, Under Continuous Keplerian Thrust</b></a> <dt>Marr, G. C. <dd><a href="abstracts/95-441.html"><b>Goddard Space Flight Center Flight Dynamics Division Ascent Acquisition Support of Space Shuttle Rendezvous Missions</b></a> <dt>Marr, G. C. <dd><a href="abstracts/95-443.html"><b>Tracking and Data Relay Satellite System (TDRSS) Support of User Spacecraft Without TDRSS Transponders</b></a> <dt>Marshall, J. A. <dd><a href="abstracts/95-312.html"><b>Precision Orbit Determination and Gravity Field Improvement Derived From TDRSS Orbit Determination</b></a> <dt>Matsuo, H. <dd><a href="abstracts/95-425.html"><b>The Low-Thrust Flyby Guidance and an Extended Optimal Spacing Rule</b></a> <dt>McAdams, J. V. <dd><a href="abstracts/95-378.html"><b>NEAR-Eros 1996: Mission Overview and Trajectory Design</b></a> <dt>McGrath, J.F. <dd><a href="abstracts/95-455.html"><b>A Simulation Method for Multibody Dynamics</b></a> <dt>McInnes, C. R. <dd><a href="abstracts/95-446.html"><b>Distributed Control for On-Orbit Assembly</b></a> <dt>McInnes, C. R. <dd><a href="abstracts/95-447.html"><b>Potential Function Methods for Autonomous Spacecraft Guidance and Control</b></a> <dt>McNamara, R. <dd><a href="abstracts/95-347.html"><b>The Investigation of Space Debris Generation and Associated Long-Term Effects in the Geosynchronous Region</b></a> <dt>McOmber, R. <dd><a href="abstracts/95-326.html"><b>Relay Satellite Orbit Selection Considerations for Future Robotics Missions to Explore Venus</b></a> <dt>McQuade, F. <dd><a href="abstracts/95-446.html"><b>Distributed Control for On-Orbit Assembly</b></a> <dt>Meister, L. <dd><a href="abstracts/95-300.html"><b>Estimation of Rotating Body Attitude by Quaternion Filter</b></a> <dt>Melton, R. G. <dd><a href="abstracts/95-415.html"><b>Multiple Rigid Body Reorientation Using Relative Motion With Constrained Final System Configuration</b></a> <dt>Menn, M. D. <dd><a href="abstracts/95-343.html"><b>A Prototype Onboard Processor for LEO Control Using a GPS Receiver</b></a> <dt>Miller, A. <dd><a href="abstracts/95-304.html"><b>The New SKYMAP Master Catalog (Version 4.0)</b></a> <dt>Miller, T. <dd><a href="abstracts/95-309.html"><b>Trajectory Optimization for Solar Electric Propulsion Missions to GEO Considering the Radiation and Shadow Environments</b></a> <dt>Minnie, C. <dd><a href="abstracts/95-388.html"><b>Orbit Determination Support for the Clementine Mission During Lunar Orbit Phase</b></a> <dt>Misra, A. K. <dd><a href="abstracts/95-354.html"><b>Control of a Chain of Flexible Bodies Using Lyapunov's Stability Theory</b></a> <dt>Misra, A. K. <dd><a href="abstracts/95-317.html"><b>Near-Minimum-Time Maneuvering of Flexible Space Manipulators Along a Prescribed Path</b></a> <dt>Misra, A. K. <dd><a href="abstracts/95-322.html"><b>Dynamics and Control of Mobile Flexible Manipulators with Slewing and Deployable Links</b></a> <dt>Mock, S. A. <dd><a href="abstracts/95-350.html"><b>Orbit Determination of a Tethered Satellite</b></a> <dt>Modi, V. J. <dd><a href="abstracts/95-322.html"><b>Dynamics and Control of Mobile Flexible Manipulators with Slewing and Deployable Links</b></a> <dt>Modi, V. J. <dd><a href="abstracts/95-395.html"><b>System Modes Based Dynamics and Control of Multibody Systems:Analysis and Applications</b></a> <dt>Moore, J. L. <dd><a href="abstracts/95-303.html"><b>In-Flight Calibration of the Field of View Distortion for Spacecraft Attitude Sensors</b></a> <dt>Morgan, S.R. <dd><a href="abstracts/95-351.html"><b>Attitude and Orbit Estimation of a Tether Satellite System</b></a> <dt>Muellerschoen, R. J. <dd><a href="abstracts/95-368.html"><b>TOPEX/Poseidon Precision Orbit Determination: 'Quick-Look' Operations with GPS and SLR Data</b></a> <dt>Neal, H. L. <dd><a href="abstracts/95-426.html"><b>An Analytic Orbit Propagation Program for Satellite Catalog Maintenance</b></a> <dt>Necsulescu, D. <dd><a href="abstracts/95-358.html"><b>Single and Dual Arm Robot Control for Free and Contact Motion</b></a> <dt>Nelson, K. <dd><a href="abstracts/95-326.html"><b>Relay Satellite Orbit Selection Considerations for Future Robotics Missions to Explore Venus</b></a> <dt>Nerem, R. S. <dd><a href="abstracts/95-310.html"><b>Preliminary Results from the Joint GSFC/DMA Gravity Model Project</b></a> <dt>Neta, B. <dd><a href="abstracts/95-431.html"><b>Comparison of Orbit Propagators in the Research and Development Goddard Trajectory Determination System (R & D GTDS). Part I: Simulated Data</b></a> <dt>Neumann, G. A. <dd><a href="abstracts/95-313.html"><b>Results from the Clementine Lunar Geodesy Investigation</b></a> <dt>Newman, L. K. <dd><a href="abstracts/95-325.html"><b>Evaluation of Spacecraft End-of-Life Disposal to Meet NASA Management Instruction (NMI) Guidelines</b></a> <dt>Newman, L. K. <dd><a href="abstracts/95-444.html"><b>Flight Dynamics Support for the Clementine Deep Space Program Science Experiment (DSPSE)</b></a> <dt>Nicholson, F. T. <dd><a href="abstracts/95-381.html"><b>Navigation Strategy for the Galileo Jupiter Encounter and Orbital Tour</b></a> <dt>Oh, P. <dd><a href="abstracts/95-376.html"><b>The Use of the Euler Operator in Learning and Repetitive Control</b></a> <dt>Ortiz, V. M. <dd><a href="abstracts/95-336.html"><b>An Evaluation of Energy-Sink Stability Criteria for Dual-Spin Spacecraft</b></a> <dt>Palmerini, G. B. <dd><a href="abstracts/95-332.html"><b>Optimal Design and Orbital Control of Satellite Constellations for Global Coverage</b></a> <dt>Pardini, C. <dd><a href="abstracts/95-348.html"><b>The Contribution of Past Fragmentation Events to the Uncatalogued Orbital Debris Population</b></a> <dt>Pardis, C. J. <dd><a href="abstracts/95-452.html"><b>Optimal Rendezvous of a Spacecraft with Multiple Power-Limited Thrusters Having Upper and Lower Bounds</b></a> <dt>Pastrone, D. <dd><a href="abstracts/95-305.html"><b>Indirect Optimization Method for Round-Trip Mars Trajectories</b></a> <dt>Pastrone, D. <dd><a href="abstracts/95-450.html"><b>Optimal Aeroassisted GEO-to-LEO Transfer by an Indirect Method</b></a> <dt>Patel, R. V. <dd><a href="abstracts/95-361.html"><b>A Trajectory Planning and Object Avoidance System for Kinematically Redundant Manipulators: An Experimental Evaluation</b></a> <dt>Paynter, S. J. <dd><a href="abstracts/95-418.html"><b>Indirect Adaptive Nonlinear Attitude Control and Momentum Management of Spacecraft Using Feedback Linearization</b></a> <dt>Penzo, P. A. <dd><a href="abstracts/95-380.html"><b>Multiple Encounter Missions with the Trojan and Main Belt Asteroids</b></a> <dt>Penzo, P. A. <dd><a href="abstracts/95-405.html"><b>LAMDA: A Software Tool for Lunar-Assist Escape Missions</b></a> <dt>Pernicka, H. J. <dd><a href="abstracts/95-400.html"><b>Low DV Earth-to-Moon Trajectories</b></a> <dt>Perrotta, G. <dd><a href="abstracts/95-331331.html"><b>Properties of a Class of Elliptical Sunsynchronous Orbits For Regional Communications and Remote Sensing</b></a> <dt>Piedboeuf, J. C. <dd><a href="abstracts/95-357.html"><b>Symbolic Modelling of Flexible Manipulators</b></a> <dt>Piedboeuf, J. C. <dd><a href="abstracts/95-359.html"><b>SYMOFROS: Symbolic Modelling of Flexible Robots and Simulation</b></a> <dt>Pierson, B. L. <dd><a href="abstracts/95-399.html"><b>Optimal Earth-Moon Trajectories Using Nuclear Electric Propulsion</b></a> <dt>Pierson, B. L. <dd><a href="abstracts/95-448.html"><b>Combined Launch Trajectory and Vehicle Design Optimization</b></a> <dt>Powell, G. E. <dd><a href="abstracts/95-445.html"><b>Autonomous Visible-Band Tracking for the Midcourse Space Experiment (MSX)</b></a> <dt>Powell, J. D. <dd><a href="abstracts/95-356.html"><b>Use of Passive Damping for a Tethered Artificial Gravity Spacecraft</b></a> <dt>Powers, P. P. <dd><a href="abstracts/95-441.html"><b>Goddard Space Flight Center Flight Dynamics Division Ascent Acquisition Support of Space Shuttle Rendezvous Missions</b></a> <dt>Proulx, R. J. <dd><a href="abstracts/95-428.html"><b>Parallel Orbit Propagation and the Analysis of Satellite Constellations</b></a> <dt>Puig-Suari, J. <dd><a href="abstracts/95-353.html"><b>A General Approach to Aerobraking Tether Design</b></a> <dt>Rampalli, R. <dd><a href="abstracts/95-455.html"><b>A Simulation Method for Multibody Dynamics</b></a> <dt>Randall, L. A. <dd><a href="abstracts/95-373.html"><b>Complex Analytic Solutions for a Spinning Rigid Body Under Constant Transverse Torques</b></a> <dt>Richardson, D.L. <dd><a href="abstracts/95-409.html"><b>A General Purpose Family of Numerical Integration Procedures for Astrodynamics Applications</b></a> <dt>Richardson, D. L. <dd><a href="abstracts/95-407.html"><b>Chaos in Artificial Satellite Motion Due to Third-Body Effects</b></a> <dt>Richon, K. <dd><a href="abstracts/95-323.html"><b>Operational Use of Swingby-an Interactive Trajectory Design and Maneuver Planning Tool - for Mission to the Moon and Beyond</b></a> <dt>Richon, K. V. <dd><a href="abstracts/95-444.html"><b>Flight Dynamics Support for the Clementine Deep Space Program Science Experiment (DSPSE)</b></a> <dt>Riedel, J. E. <dd><a href="abstracts/95-387.html"><b>Demonstration of Autonomous Orbit Determination Around Small Bodies</b></a> <dt>Ries, J. C. <dd><a href="abstracts/95-386.html"><b>Application of Precision Orbit Determination Techniques to Tracking and Prediction of Multiple Space Objects</b></a> <dt>Rim, H. J. <dd><a href="abstracts/95-370.html"><b>Dynamic Orbit Determination for the EOS Laser Altimeter Satellite (EOS ALT/GLAS) using GPS Measurements</b></a> <dt>Robinett, R. D. <dd><a href="abstracts/95-417.html"><b>Globally Stable Feedback Laws for Near-Minimum-Fuel and Near-Minimum-Time Pointing Maneuvers for a Landmark-Tracking Spacecraft</b></a> <dt>Robins, A. <dd><a href="abstracts/95-361.html"><b>A Trajectory Planning and Object Avoidance System for Kinematically Redundant Manipulators: An Experimental Evaluation</b></a> <dt>Rodriguez-Canabal, J. <dd><a href="abstracts/95-404.html"><b>Use of Earth-Moon Libration Points for Future Missions</b></a> <dt>Ross, I. M. <dd><a href="abstracts/95-336.html"><b>An Evaluation of Energy-Sink Stability Criteria for Dual-Spin Spacecraft</b></a> <dt>Rossi, A. <dd><a href="abstracts/95-348.html"><b>The Contribution of Past Fragmentation Events to the Uncatalogued Orbital Debris Population</b></a> <dt>Rowlands, D. D. <dd><a href="abstracts/95-313.html"><b>Results from the Clementine Lunar Geodesy Investigation</b></a> <dt>Rubenstein, D. S. <dd><a href="abstracts/95-415.html"><b>Multiple Rigid Body Reorientation Using Relative Motion With Constrained Final System Configuration</b></a> <dt>Ryan, R.R. <dd><a href="abstracts/95-455.html"><b>A Simulation Method for Multibody Dynamics</b></a> <dt>Sabol, C. <dd><a href="abstracts/95-340.html"><b>Refinement of a Sun-Synchronous, Critically Inclined Orbit for a Global Personal Communications System</b></a> <dt>Sadigh, M. J. <dd><a href="abstracts/95-317.html"><b>Near-Minimum-Time Maneuvering of Flexible Space Manipulators Along a Prescribed Path</b></a> <dt>Saeed, S. . <dd><a href="abstracts/95-356.html"><b>Use of Passive Damping for a Tethered Artificial Gravity Spacecraft</b></a> <dt>Saggin, B. <dd><a href="abstracts/95-355.html"><b>Non-Linear Dissipative Effects in Tethered Multilayer Systems for Space Missions</b></a> <dt>Salama, A. H. <dd><a href="abstracts/95-367.html"><b>Statistical Performance of TOPEX/POSEIDON Prime Mission Ground and On-Board Ephemerides and Consequences for the Extended Mission</b></a> <dt>Salama, A. H. <dd><a href="abstracts/95-411.html"><b>Semi-Autonomous Spacecraft On-Board Ephemeris Propagation</b></a> <dt>Scarberry, D. P. <dd><a href="abstracts/95-400.html"><b>Low DV Earth-to-Moon Trajectories</b></a> <dt>Schaub, H. <dd><a href="abstracts/95-417.html"><b>Globally Stable Feedback Laws for Near-Minimum-Fuel and Near-Minimum-Time Pointing Maneuvers for a Landmark-Tracking Spacecraft</b></a> <dt>Schinnerer, R.G. <dd><a href="abstracts/95-.html"><b>A Gemini Puzzle - Optical Imaging 30 Years Ago</b></a> <dt>Schumacher, P. W. <dd><a href="abstracts/95-427.html"><b>Analytic Orbit Model for U.S. Naval Space Surveillance: An Overview</b></a> <dt>Schumacher, P. W. <dd><a href="abstracts/95-430.html"><b>Testing of Naval Space Command New Analytic Orbit Model</b></a> <dt>Schutz B. E. <dd><a href="abstracts/95-370.html"><b>Dynamic Orbit Determination for the EOS Laser Altimeter Satellite (EOS ALT/GLAS) using GPS Measurements</b></a> <dt>Schwertassek, R. <dd><a href="abstracts/95-391.html"><b>On a Systematic Way to Compute Geometric Stiffening Terms For Multibody Simulation</b></a> <dt>Seal, D. <dd><a href="abstracts/95-382.html"><b>Exposure of the Cassini Spacecraft to Horseshoe and Tadpole Particle Zones</b></a> <dt>Segerman, A. M. <dd><a href="abstracts/95-426.html"><b>An Analytic Orbit Propagation Program for Satellite Catalog Maintenance</b></a> <dt>Shadpey, F. <dd><a href="abstracts/95-361.html"><b>A Trajectory Planning and Object Avoidance System for Kinematically Redundant Manipulators: An Experimental Evaluation</b></a> <dt>Shapiro, B. E. <dd><a href="abstracts/95-366.html"><b>An Analysis of the TOPEX/Poseidon Operational Orbit: Observed Variations and Why</b></a> <dt>Shum, C. 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N. <dd><a href="abstracts/95-311.html"><b>Earth Gravitational Model Error Budget for Space Control</b></a> <dt>Wallner, R. N. <dd><a href="abstracts/95-432.html"><b>The Accuracy of General Perturbations and Semianalytic Satellite Ephemeris Theories</b></a> <dt>Wallrapp, O. <dd><a href="abstracts/95-392.html"><b>Standardization and Preparation of Flexible Body Data In Multibody Formulations</b></a> <dt>Wang, Y. <dd><a href="abstracts/95-377.html"><b>Use of Non-Causal Digital Signal Processing in Learning and Repetitive Control</b></a> <dt>Warren, W. <dd><a href="abstracts/95-304.html"><b>The New SKYMAP Master Catalog (Version 4.0)</b></a> <dt>Wielicki, B. A. <dd><a href="abstracts/95-329.html"><b>Orbital Analysis of LidarSat for Synergistic Measurements With the Earth Observing System (EOS) Satellite</b></a> <dt>Williams, S. E. <dd><a href="abstracts/95-343.html"><b>A Prototype Onboard Processor for LEO Control Using a GPS Receiver</b></a> <dt>Williams, T. <dd><a href="abstracts/95-339.html"><b>SAFER Mass Properties Determination: Results from On-Orbit Data</b></a> <dt>Williams, T. <dd><a href="abstracts/95-375.html"><b>Direct Adaptive Control for SAFER/Astronaut System</b></a> <dt>Williamson, R. G. <dd><a href="abstracts/95-312.html"><b>Precision Orbit Determination and Gravity Field Improvement Derived From TDRSS Orbit Determination</b></a> <dt>Wilson, M.G. <dd><a href="abstracts/95-381.html"><b>Navigation Strategy for the Galileo Jupiter Encounter and Orbital Tour</b></a> <dt>Wolf , A. A. <dd><a href="abstracts/95-382.html"><b>Exposure of the Cassini Spacecraft to Horseshoe and Tadpole Particle Zones</b></a> <dt>Wolfe, S. M. <dd><a href="abstracts/95-416.html"><b>A Magnetic Attitude Control System for Sun Pointing Satellites</b></a> <dt>Wright, J. 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