1995 AAS/AIAA Astrodynamics Specialists Conference Author Index

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