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-Title: Astrodynamics 2005 - Part III.
-Authors:
Bobby G. Williams; Louis A. D'Amario; Kathleen C. Howell; Felix R. Hoots (Edits.).
-Publisher:
Univelt, Inc.
-Pages:
24 + 1859-2854
-Illustrations:
B/W graphics and photos.
-Language:
English.
-Publication Date:
2006.
-Collection:
Advances in the Astronautical Sciences, Volume 123 Part II.
-ISBN:
087703527X

Front Cover

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EDITORIAL INFORMATION

This volume in three parts presents the proceedings of the 2005 Astrodynamics Conference held in South Lake Tahoe, California, August 7-11, 2005. It includes a CD-ROM.

(Extracted from the Foreword).

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GENERAL TABLE OF CONTENTS

-Part III.
-TRAJECTORY DESIGN AND OPTIMIZATION II
-An Algorithm for Computing Near-Optimal, Many-Revolution Earth-Orbit
Transfers (AAS 05-371) Y. Gao and C. A. Kluever.
-Indirect Optimization of Spiral Trajectories (AAS 05-372) Christopher L. Ranieri and Cesar A. Ocampo.
-Minimum Impulse Transfers to Rotate the Line of Apsides (AAS 05-373)
Connie Phong and Theodore H. Sweetser.
-Low-Thrust Gravity Assist Trajectory Optimization Using Evolutionary
Neurocontrollers (AAS 05-374) Ian Carnelli, Bernd Dachwald, Massimiliano Vasile, Wolfgang Seboldt and Amalia Ercoli Finzi.
-Optimization of Low-Thrust Gravity-Assist Trajectories With a Reduced
Parameterization of the Thrust Vector (AAS 05-375) Chit Hong Yam and James M. Longuski.
-Six-Degree-of-Freedom Trajectory Optimization Utilizing a Two-Timescale Collocation Architecture (AAS 05-376) Prasun N. Desai and Bruce A. Conway.
-Numerical Investigation of Mapping Orbits About Jupiter’s Icy Moons
(AAS 05-377) John Aiello.
-DYNAMICAL SYSTEMS THEORY AND APPLICATIONS
-Stability Maps, Global Dynamics and Transfers (AAS 05-378) Benjamin Villac and Martín Lara.
-Surface Structure of an Invariant Manifold of a Halo Orbit (AAS 05-379)
Anil N. Hirani and Martin W. Lo.
-Chaining Simple Periodic Three Body Orbits (AAS 05-380) Martin W. Lo and Jeffrey S. Parker.
-Lyapunov Stability of Hovering Spacecraft in Time-Invariant Systems (AAS 05-381) S. B. Broschart and D. J. Scheeres.
-A Low Energy Lunar Transportation System Using Chaotic Dynamics
(AAS 05-382) Edward Belbruno.
-Shoot the Moon 3D (AAS 05-383) Jeffrey S. Parker and Martin W. Lo.
-On Parking Solutions Around Europa (AAS 05-384) Martin Lara, Ryan Russell and Benjamin Villac.
-ATMOSPHERIC ENTRY / REENTRY BREAKUP ANALYSIS
-Vehicle Breakup Analysis for Applications in Aerospace Nuclear Safety
(AAS 05-385) Lisa Ling, Dan Tuckness, Ahmed Salama and Angus McRonald.
-A Methodology of MSL Breakup Analysis for Earth Accidental Reentry and its Application to Breakup Analysis for Mars Off-Nominal Entry (AAS 05-386) Ahmed Salama and Lisa Ling.
-A Genesis Breakup and Burnup Analysis in Off-Nominal Earth Return and
Atmospheric Entry (AAS 05-387) Ahmed Salama, Lisa Ling and Angus McRonald.
-Development of Hypersonic Aerodynamic Coefficients for Arbitrary-Shaped Body Obtained from Newtonian Theory Using Triangular Panels (AAS 05-388) Lisa Ling and Dan Tuckness.
-Development of Non-Arbitrary Atmospheric Entry Points for Impact Footprint Determination in an Inadvertent Earth Reentry During Launch Contingency (AAS 05-389) Lisa Ling and Dan Tuckness.
-Modeling of Local Winds and Real-Time Application in Impact Point Prediction for Inadvertent Earth Reentry During Launch Contingency (AAS 05-390) Lisa Ling and Dan Tuckness.
-LOW THRUST MISSION AND TRAJECTORY DESIGN
-Genetic Algorithms for Interplanetary Continuous Thrust Trajectory Design
(AAS 05-391) Glenn E. Peterson, Eric T. Campbell, John P. McVey and Ryan M. Guice.
-Optimisation of Low-Thrust Orbit Transfers Using the Q-Law for the Initial Guess (AAS 05-392) Anastassios E. Petropoulos and Seungwon Lee.
-Low-Thrust Orbit Transfer Optimization with Refined Q-Law and Multi-Objective Genetic Algorithm (AAS 05-393) Seungwon Lee, Anastassios E. Petropoulos and Paul von Allmen.
-Maximum Deliverable Mass for Low-Thrust Geosynchronous Transfers Under Realistic Mission Constraints (AAS 05-394) Alan B. Jenkin.
-Low-Thrust Roundtrip Trajectories to Mars With One-Synodic-Period Repeat Time (AAS 05-395) Masataka Okutsu, Damon F. Landau and James M. Longuski.
-Analysis of Chemical, REP, and SEP Missions to the Trojan Asteroids
(AAS 05-396) Eugene P. Bonfiglio, David Oh and Chen-Wan Yen.
-Earth Gravity-Assist Trajectories to Jupiter Using Nuclear Electric Propulsion (AAS 05-397) Daniel W. Parcher and Jon A. Sims.
-Gravity-Assist Trajectories to Jupiter Using Nuclear Electric Propulsion
(AAS 05-398) Daniel W. Parcher and Jon A. Sims.
-ORBIT DETERMINATION II
-Linked, Autonomous, Interplanetary Satellite Orbit Navigation (LiAISON)
(AAS 05-399) Keric Hill, Martin W. Lo and George H. Born.
-Linked, Autonomous, Interplanetary Satellite Orbit Navigation (LiAISON) in Lunar Halo Orbits (AAS 05-400) Keric Hill, George H. Born and Martin W. Lo.
-An Overview of the ANDE Risk Reduction Flight (AAS 05-401) A. C. Nicholas, S. E. Thonnard, I. Galysh, P. Kalmanson and B. Bruninga.
-Special Perturbations to General Perturbations Extrapolation Differential Correction in Satellite Catalog Maintenance (AAS 05-402) David A. Cappellucci.
-Astrodyanmics Environment (ADE): An Alternative Approach to Space Dynamics Software (AAS 05-403) William B. Simpson and Kenneth J. Ernandes.
-Nonlinear Mapping of Gaussian State Uncertainties: Theory and Applications to Spacecraft Control and Navigation (AAS 05-404) Ryan S. Park and Daniel J. Scheeres.
-Maneuver Estimation Model for Relative Orbit Determination (AAS 05-405) Tara R. Storch, William E. Wiesel, Chris Sabol, Kyle T. Alfriend and K.Kim Luu.
-Using EOP and Space Weather Data for Satellite Operations (AAS 05-406) David A. Vallado and T. S. Kelso.
-TRAJECTORY DESIGN AND OPTIMIZATION III
-Mission Design of the First Robotic Lunar Exploration Program Mission:
The Lunar Reconnaissance Orbiter (AAS 05-300) Mark Beckman and Dave Folta.
-Trajectory Analysis of the Terminal Rendezvous Phase of the TECSAS Mission (AAS 05-408) Mathieu A. Landry, Arun K. Misra, Fédéric J. Pelletier, Johanne C. Heald and Alfred Ng.
-Calculation of Impulsive Hovering Trajectories Via Relative Orbit Elements (AAS 05-409) T. Alan Lovell and Mark V. Tollefson.
-Robust Aero-Gravity Assisted Maneuvers for a Multi-Objective Interplanetary Trajectory Design Optimization (AAS 05-410) Michčle R. Lavagna, Davide Lo Pinto and Amalia Ercoli Finzi.
-Potential Effects of Optical Solar Sail Degradation on Trajectory Design
(AAS 05-413) Bernd Dachwald, Volodymyr Baturkin, Victoria L. Coverstone, Benjamin Diedrich, Gregory P. Garbe, Marianne Görlich, Manfred Leipold, Franz Lura, Malcolm Macdonald, Colin R. McInnes, Giovanni Mengali, Alessandro A. Quarta, Leonel Rios-Reyes, Daniel J. Scheeres, Wolfgang Seboldt and Bong Wie.
-An Ultra-High-Altitude Sun-Synchronous Orbit and the Perturbation Due to
the Earth Gravity (AAS 05-414) Keiko Kuroshima, Shuhei Nishimaki, Takanao Saiki and Jun’ichiro Kawaguchi.
-ATTITUDE DYNAMICS AND CONTROL III
-Error Propagation Model for Rhumb-Line Attitude Maneuvers (AAS 05-415) Jozef C. van der Ha.
-Attitude Control: Solar Photon Thruster vs. Plane Solar Sail (AAS 05-416)
Anna D. Guerman and Georgi Smirnov.
-Three-Axis Magnetic Attitude Control Using Pseudospectral Control Law
(AAS 05-417) Hui Yan, I. Michael Ross and Kyle T. Alfriend.
-Gimbal-Position Command Generation for a Cluster of Control Moment
Gyroscopes (AAS 05-418) Giulio Avanzini.
-Singularity-Free Optimal Steering of Control Moment Gyros (AAS 05-419)
Andrew Fleming and I. Michael Ross.
-Quaternion-Based Satellite Attitude Control Using Fuzzy Logic (AAS 05-420) Mélanie Bélanger and Jean de Lafontaine.
-Further Results in Reduced Order Compensators for Dynamic Systems Using LQG/LTR Methods, (AAS 05-422) Donald L. Mackison and Andrew Sivess.
-LIBRATION POINT TRAJECTORIES
-WMAP Solar Radiation Pressure Modeling During February 2005 Reaction Wheel Power Off Anomaly (AAS 05-423) Dale R. Fink.
-Study on the Station Keeping Maintenance for the TPF Mission (AAS 05-424) G. Gómez, M. W. Lo and J. J. Masdemont.
-A Control Configured Small Circular Halo Orbit Around L2 (AAS 05-425)
Kohta Tarao and Jun’ichiro Kawaguchi.
-Using Hill’s 3-Body Equations to Approximate the Genesis Libration Trajectory (AAS 05-426) Nicholas G. Smith, Vincent C. Herr and Brandon S. Smith.
-Libration Points of a Gyrostat in a Generalized Restricted Three-Body Problem: Linear Stability (AAS 05-427) J. A. Vera and A. Vigueras.
-Earth-Moon Triangular Libration Point Spacecraft Formations in the Circular Restricted Three-Body Problem (AAS 05-429) Kathryn A. Catlin and Craig A. McLaughlin.
-APPENDICES
-Publications of the American Astronautical Society.
-Advances in the Astronautical Sciences.
-Science and Technology Series.
-AAS History Series.
-INDICES
-Numerical Index.
-Author Index.

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