A collection of technical papers // AIAA/AAS Astrodynamics Specialist Conference : Keystone, Colorado, 21 - 24 August 2006 ; Vol. 2 (English)
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2006
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Title:A collection of technical papers // AIAA/AAS Astrodynamics Specialist Conference : Keystone, Colorado, 21 - 24 August 2006 ; Vol. 2
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Contributors:
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Conference:AIAA/AAS Astrodynamics Specialist Conference and Exhibit ; 2006 ; Keystone, Colo.
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Publisher:
- New search for: American Institute of Aeronautics and Astronautics
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Place of publication:Reston, Va.
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Publication date:2006
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Size:XV S., S. 753 - 1492, 3 S
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ISBN:
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Type of media:Conference Proceedings
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Type of material:Print
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Language:English
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Contract number:AIAA-2006-6299/AIAA-2006-6309, AIAA-2006-6382/AIAA-2006-6412, AIAA-2006-6513/AIAA-2006-6539, AIAA-2006-6650/AIAA-2006-6656
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Table of contents conference proceedings
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1
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Satellite Formation Design with a Multi-Objective Optimization Technique AIAA Paper 2006-6013Hoskins, A. / Atkins, E. et al. | 2006
- 13
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Digitial LQR Control Scheme to Maintain the Separation Distance of the NASA Benchmark Tetrahedron Constellation AIAA Paper 2006-6014Capo-Lugo, P. / Bainum, P. et al. | 2006
- 25
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Constellation Design with Parallel Multi-Objective Evolutionary Computation AIAA Paper 2006-6015Ferringer, M. / Clifton, R. / Thompson, T. et al. | 2006
- 44
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Dynamics of Drag-Free Formations for Earth Imaging Applications AIAA Paper 2006-6016Ploen, S. / Quadrelli, M. / Scharf, D. / Hadaegh, F. et al. | 2006
- 63
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Formation Flight Control for Modeling Interferometric Aperture Planes AIAA Paper 2006-6017O Malley, J. / Spencer, D. et al. | 2006
- 86
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Differential Perturbations and Semimajor Axis Estimation for Satellite Formation Orbits AIAA Paper 2006-6018Wnuk, E. / Golebiewska, J. et al. | 2006
- 99
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Continuous Mars Habitation with a Limited Number of Cycler Vehicles AIAA Paper 2006-6020Landau, D. / Longuski, J. / Aldrin, B. et al. | 2006
- 112
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Low-Thrust Aldrin Cycler with Reduced Encounter Velocities AIAA Paper 2006-6021Chen, K. / Okutsu, M. / Landau, D. / Longuski, J. et al. | 2006
- 122
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Mars Entry, Descent, and Landing Parametric Sizing and Design Space Visualization Trades AIAA Paper 2006-6022Alemany, K. / Wells, G. / Theisinger, J. / Clark, I. / Braun, R. et al. | 2006
- 134
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Entry Trajectory Simulation Using ESA Mars Climate Database Version 4.1 AIAA Paper 2006-6023Mooij, E. / Huot, J. / Ortega, G. et al. | 2006
- 147
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Analytic Solutions for Aerocapture, Descent, and Landing Trajectories for Dual-Use Ballute Systems AIAA Paper 2006-6026Medlock, K. / Ayoubi, M. / Longuski, J. / Lyons, D. et al. | 2006
- 172
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Pso Algorithm For Planetary Atmosphere Entry Vehicles Multidisciplinary Guidance Design AIAA Paper 2006-6027Lavagna, M. / Parigini, C. / Armellin, R. et al. | 2006
- 188
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Trajectory Design of the Lunar Impactor Mission Concept AIAA Paper 2006-6031Chung, M. / McElrath, T. / Roncoli, R. et al. | 2006
- 197
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Comparison of Implicit Integration Methods for Solving Aerospace Trajectory Optimization Problems AIAA Paper 2006-6033Riehl, J. / Paris, S. / Sjauw, W. et al. | 2006
- 223
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Stationkeeping on Libration Point Orbits in the Elliptic Restricted Three-Body Problem AIAA Paper 2006-6035Gurfil, P. / Meltzer, D. et al. | 2006
- 255
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Aero-Gravity Assist Maneuvers: Coupled Trajectory and Vehicle Shape Optimization AIAA Paper 2006-6036Armellin, R. / Lavagna, M. / Starkey, R. / Lewis, M. et al. | 2006
- 270
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Attitude Determination through Image Registration Model and Test-case for Novel Attitude System in Low Earth Orbit AIAA Paper 2006-6157Bamber, D. / Palmer, P. / Mackin, S. et al. | 2006
- 284
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An Empirical Comparison between Two Recursive Filters for Attitude and Rate Estimation of Spinning Spacecraft AIAA Paper 2006-6158Harman, R. et al. | 2006
- 306
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Nonlinear Symplectic Attitude Estimation for Small Satellites AIAA Paper 2006-6159Valpiani, J. / Palmer, P. et al. | 2006
- 322
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An Object-Oriented Operator-Overloaded Quaternion Toolbox AIAA Paper 2006-6160Turner, J. et al. | 2006
- 346
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Accommodating Sensor Uncertainty in the Cones Method: Polycones and Fuzzycones AIAA Paper 2006-6162Hashmall, J. et al. | 2006
- 356
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Gyroless Attitude Control of Multi-Body Satellites Using an Unscented Kalman Filter AIAA Paper 2006-6163Fisher, J. / Vadali, S. et al. | 2006
- 373
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Quaternion Estimation and Norm Constrained Kalman Filtering AIAA Paper 2006-6164Zanetti, R. / Bishop, R. et al. | 2006
- 388
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The Development of New Solar Indices for Use in Thermospheric Density Modeling AIAA Paper 2006-6165Tobiska, W. / Bouwer, S. / Bowman, B. et al. | 2006
- 401
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A New Empirical Thermospheric Density Model JB2006 Using New Solar Indices AIAA Paper 2006-6166Bowman, B. / Tobiska, W. / Marcos, F. et al. | 2006
- 422
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Accuracy of Earth's Thermospheric Neutral Density Models AIAA Paper 2006-6167Marcos, F. / Bowman, B. / Sheehan, R. et al. | 2006
- 442
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Improvements in Density Modeling Using the Air Force Dynamic Calibration Atmosphere Model AIAA Paper 2006-6168Casali, S. / Barker, W. / Bowman, B. et al. | 2006
- 456
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Comparison of TIMED Satellite Drag with Solar EUV Experiment (SEE) Measurements AIAA Paper 2006-6169Woodraska, D. / Woods, T. / Eparvier, F. et al. | 2006
- 463
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Atmospheric Wind Measurements Deduced from Accelerometer Data AIAA Paper 2006-6170Sutton, E. / Forbes, J. / Nerem, R. et al. | 2006
- 484
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Neutral Density Measurements from the GRACE Accelerometers AIAA Paper 2006-6171Tapley, B. / Ries, J. / Bettadpur, S. / Cheng, M. et al. | 2006
- 495
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Storm-Time Density Enhancements Observed by CHAMP and GRACE AIAA Paper 2006-6172Bruinsma, S. / Forbes, J. / Zhang, X. et al. | 2006
- 505
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Mass Efficiency Trends for Nuclear Thermal Propulsion Systems AIAA Paper 2006-6174Rauwolf, G. / Borowski, S. et al. | 2006
- 514
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Mission Options for Rendezvous with Wild 2 in 2016 Using Electric Propulsion AIAA Paper 2006-6175Guzman, J. / Horsewood, J. et al. | 2006
- 532
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Solar Sail Trajectory Optimization for the Solar Polar Imager (SPI) Mission AIAA Paper 2006-6177Dachwald, B. / Ohndorf, A. / Wie, B. et al. | 2006
- 550
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Solar Sailing Kinetic Energy Impactor (KEI) Mission Design Tradeoffs for Impacting and Deflecting Asteroid 99942 Apophis AIAA Paper 2006-6178Dachwald, B. / Kahle, R. / Wie, B. et al. | 2006
- 570
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Advanced Satellite Bus Technology for Near-Term Solar Sail Missions AIAA Paper 2006-6179Lappas, V. / Wie, B. et al. | 2006
- 589
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Evolutionary Optimization for a Solar Sailing Solar Polar Mission AIAA Paper 2006-6180Mooij, E. / Noomen, R. / Candy, S. et al. | 2006
- 602
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The Partition of Unity Finite Element Approach to the Stationary Fokker-Planck Equation AIAA Paper 2006-6285Kumar, M. / Singla, P. / Chakravorty, S. / Junkins, J. et al. | 2006
- 617
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Dynamic Analysis and Control of a Stewart Platform Using A Novel Automatic Differentiation Method AIAA Paper 2006-6286Bai, X. / Turner, J. / Junkins, J. et al. | 2006
- 628
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Realistic Models for the Comet Dynamical Environment AIAA Paper 2006-6288Byram, S. / Scheeres, D. / Combi, M. et al. | 2006
- 644
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Polyhedral Potential and Variational Integrator Computation of the Full Two Body Problem AIAA Paper 2006-6289Fahnestock, E. / Lee, T. / Leok, M. / McClamroch, N. / Scheeres, D. et al. | 2006
- 661
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Establishment and Implementation of a Close Approach Evaluation and Avoidance Process for Earth Observing System Missions AIAA Paper 2006-6291Newman, L. / Duncan, M. et al. | 2006
- 673
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The Debris Environment Around the Earth Science Morning and Afternoon Constellations AIAA Paper 2006-6292Demarest, P. et al. | 2006
- 688
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Realistic Covariance Prediction for the Earth Science Constellation AIAA Paper 2006-6293Duncan, M. / Long, A. et al. | 2006
- 700
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Adapting Covariance Propagation to Account for the Presence of Modeled and Unmodeled Maneuvers AIAA Paper 2006-6294Schiff, C. et al. | 2006
- 711
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Development of a Nonlinear Probability of Collision Tool for the Earth Observing System AIAA Paper 2006-6295McKinley, D. et al. | 2006
- 727
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Satellite Breakup Risk Mitigation AIAA Paper 2006-6296Leleux, D. / Smith, J. et al. | 2006
- 735
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A Brief Study of Ground Controlled Orbital Rendezvous: When is Autonomy Required? AIAA Paper 2006-6298Geller, D. et al. | 2006
- 752
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Guidance Strategy for Hyperbolic Rendezvous AIAA Paper 2006-6299Landau, D. / Longuski, J. et al. | 2006
- 768
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Relative Angles-Only Navigation and Pose Estimation for Autonomous Orbital Rendezvous AIAA Paper 2006-6300Woffinden, D. / Geller, D. et al. | 2006
- 791
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On Discrete-Time Optimality Conditions for Pseudospectral Methods AIAA Paper 2006-6304Fahroo, F. / Ross, I. et al. | 2006
- 808
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Identifying Optimal Interplanetary Trajectories through a Genetic Approach AIAA Paper 2006-6306Bessette, C. / Spencer, D. et al. | 2006
- 826
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VTVL Suborbital RLV Upper Stage's Range Maximization AIAA Paper 2006-6307Xu, Y. et al. | 2006
- 834
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Trajectory Options for Human Mars Missions AIAA Paper 2006-6308Wooster, P. / Braun, R. / Ahn, J. / Putnam, Z. et al. | 2006
- 851
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Enhanced Procedures for Direct Trajectory Optimization Using Nonlinear Programming and Implicit Integration AIAA Paper 2006-6309Paris, S. / Riehl, J. / Sjauw, W. et al. | 2006
- 870
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Attitude Estimation for Sounding Rockets using MEMS gyros AIAA Paper 2006-6382Bekkeng, J. / Psiaki, M. et al. | 2006
- 886
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Autonomous Star Tracker Performance for the New Horizons Mission AIAA Paper 2006-6383Rogers, G. / Schwinger, M. / Kaidy, J. / Strikwerda, T. / Casini, R. / Landi, A. / Bettarini, R. / Lorenzini, S. et al. | 2006
- 903
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Attitude Error From Phase Center Uncertainty in an Interferometric GPS Antenna Array AIAA Paper 2006-6384Treder, A. et al. | 2006
- 917
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Iterative Magnetometer Calibration AIAA Paper 2006-6386Sedlak, J. et al. | 2006
- 929
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Design of an Image Motion Compensation (IMC) Algorithm for the Communication, Ocean, and Meteorological Satellite (COMS) AIAA Paper 2006-6387Jung, T. / Lee, U. / Park, S. / Choi, Y. / Bang, H. / Ju, G. / Yang, K. et al. | 2006
- 940
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Calculation of Zonal Winds Using Accelerometer and Rate Data from Mars Global Surveyor AIAA Paper 2006-6390Baird, D. / Tolson, R. / Bougher, S. et al. | 2006
- 954
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Atmospheric density during the aerobraking of Mars Odyssey from radio tracking data AIAA Paper 2006-6391Mazarico, E. / Zuber, M. / Lemoine, F. / Smith, D. et al. | 2006
- 967
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Mars Thermospheric Winds from MGS and Odyssey Accelerometers AIAA Paper 2006-6392Crowley, G. / Tolson, R. et al. | 2006
- 978
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Variability of the Satellite Drag Environments of Earth, Mars and Venus due to Rotation of the Sun AIAA Paper 2006-6393Forbes, J. / Bruinsma, S. / Lemoine, F. / Bowman, B. / Konopliv, A. et al. | 2006
- 987
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Global Reference Atmospheric Models, Including Thermospheres, for Mars, Venus and Earth AIAA Paper 2006-6394Justh, H. / Justus, C. / Keller, V. et al. | 2006
- 992
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Thermospheric Studies with Mars Global Surveyor AIAA Paper 2006-6395Lemoine, F. / Bruinsma, S. / Chinn, D. / Forbes, J. et al. | 2006
- 1005
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Method for Deriving Densities and In-Track Winds During Storms AIAA Paper 2006-6396Moe, K. / Moe, M. et al. | 2006
- 1013
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Application of MGS and ODY Aerobraking Accelerometer Data to Atmospheric Modeling AIAA Paper 2006-6397Tolson, R. / Keating, G. / Zurek, R. / Bougher, S. / Justus, C. / Fritts, D. et al. | 2006
- 1024
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Covariance Analysis of Cassini Titan Flyby using SAR and Altimetry Data AIAA Paper 2006-6398Park, R. / Cangahuala, L. / Chodas, P. / Roundhill, I. et al. | 2006
- 1038
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Nonlinear Semi-Analytic Method for Spacecraft Navigation AIAA Paper 2006-6399Park, R. / Scheeres, D. et al. | 2006
- 1056
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MR SAT Orbit Determination Using the 0-D Filter AIAA Paper 2006-6401Dancer, M. / Searcy, J. / Pernicka, H. et al. | 2006
- 1068
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Towards the GEOSAT Follow-On Precise Orbit Determination Goals of High Accuracy and Near-Real-Time Processing AIAA Paper 2006-6402Lemoine, F. / Zelensky, N. / Chinn, D. / Beckley, B. / Lillibridge, J. et al. | 2006
- 1085
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Orbit Determination for Microscope satellite scientific purpose AIAA Paper 2006-6403Delavault, S. / Mercier, F. et al. | 2006
- 1096
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Maneuver Analysis and Targeting Strategy for the Stardust Re-Entry Capsule AIAA Paper 2006-6406Helfrich, C. / Bhat, R. / Kangas, J. / Wilson, R. / Wong, M. / Potts, C. / Williams, K. et al. | 2006
- 1106
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Modeling of Deadbanding Delta-V for the Stardust Earth Return: Calibration, Analysis, Prediction and Performance AIAA Paper 2006-6408Kennedy, B. / McElrath, T. / Nandi, S. et al. | 2006
- 1113
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On-Orbit Maneuver Calibrations for the Stardust Spacecraft AIAA Paper 2006-6409Nandi, S. / Kennedy, B. / Williams, K. / Bymes, D. et al. | 2006
- 1118
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Entry, Descent, and Landing Operations Analysis for the Stardust Re-Entry Capsule AIAA Paper 2006-6410Desai, P. / Lyons, D. / Tooley, J. / Kangas, J. et al. | 2006
- 1128
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Interfacing with USSTRATCOM and UTTR During Stardust Earth Return AIAA Paper 2006-6411Jefferson, D. / Baird, D. / Cangahuala, L. / Lewis, G. et al. | 2006
- 1136
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Stardust Entry: Landing and Population Hazards in Mission Planning and Operations AIAA Paper 2006-6412Tooley, J. / Lyons, D. / Desai, P. / Wawrzyniak, G. et al. | 2006
- 1153
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Space Event Detection Method AIAA Paper 2006-6513Patera, R. et al. | 2006
- 1166
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Analytical Investigation of GEO Debris with High Area-to-Mass Ratio AIAA Paper 2006-6514Chao, C. et al. | 2006
- 1175
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Modelling the Meteoroid Stream Flux onto Targets in Earth Orbits AIAA Paper 2006-6516Stabroth, S. / Oswald, M. / Wiedemann, C. / Vorsmann, P. / Klinkrad, H. et al. | 2006
- 1184
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A Model for the High Area-to-Mass Ratio Debris in GEO AIAA Paper 2006-6517Oswald, M. / Flegel, S. / Stabroth, S. / Wiedemann, C. / Vorsmann, P. / Klinkrad, H. et al. | 2006
- 1191
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Two Line Element Accuracy Assessment Based On A Mixture of Gaussian Laws AIAA Paper 2006-6518Legendre, P. / Deguine, B. / Garmier, R. / Revelin, B. et al. | 2006
- 1204
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Considerations on a Feedback Control System for a Space Robot Reorientation AIAA Paper 2006-6519Hokamoto, S. / Funasako, T. et al. | 2006
- 1213
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Autonomous Attitude Control Strategies for a Nanosatellite with a Momemtum Wheel AIAA Paper 2006-6520Ascani, L. / De Rosa, D. / Curti, F. et al. | 2006
- 1224
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Frequency Shaped Cost Functionals, Guaranteed Cost Control, Modal Weighting, Loop Transmission Recovery, and Reduced Order Compensators AIAA Paper 2006-6521Mackison, D. / Fulton, J. / Palo, S. et al. | 2006
- 1237
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Development of an FPGA Based Attitude Control System for a Micro-Satellite AIAA Paper 2006-6522Grillmayer, G. / Hirth, M. / Huber, F. / Wolter, V. et al. | 2006
- 1251
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Practical, Model-Free, Completely Robust Learning Control using Reversed Time Input Runs AIAA Paper 2006-6523Longman, R. / Kwon, T. / Wang, D. / Ye, Y. et al. | 2006
- 1261
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Better Holds Can Make Worse Intersample Error in Digital Learning Control AIAA Paper 2006-6524Li, Y. / Longman, R. et al. | 2006
- 1281
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On the Relationship Between Repetitive Control and Model Predictive Control AIAA Paper 2006-6525Chen, K. / Longman, R. / Phan, M. et al. | 2006
- 1307
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Formation Flying for Distributed InSAR AIAA Paper 2006-6526Scharf, D. / Murray, E. / Ploen, S. / Gromov, K. / Chen, C. et al. | 2006
- 1322
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Micro-Arcsecond Line-of-Sight Filtered Performance for Spacecraft Formation Flying AIAA Paper 2006-6530Banas, W. / Crassidis, J. et al. | 2006
- 1336
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Hayabusa, Summary of Guidance, Navigation and Control Achievement in its Proximity Phase AIAA Paper 2006-6533Kawaguchi, J. et al. | 2006
- 1344
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Attitude Control Challenges and Solutions for Hayabusa Spacecraft AIAA Paper 2006-6534Uo, M. / Shirakawa, K. / Hashimoto, T. / Kubota, T. / Kawaguchi, J. et al. | 2006
- 1354
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Optical Hybrid Navigation and Station Keeping around Itokawa AIAA Paper 2006-6535Kominato, T. / Matsuoka, M. / Uo, M. / Hashimoto, T. / Kawaguchi, J. et al. | 2006
- 1369
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Hayabusa, Detailed Guidance and Navigation Operations during Descents and Touchdowns AIAA Paper 2006-6536Kawaguchi, J. / Aida, S. / Morita, H. et al. | 2006
- 1386
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Hayabusa's Real-time Landmark Tracking Navigation for Descents and Touching-Downs AIAA Paper 2006-6537Morita, H. / Shirakawa, K. / Kubota, T. / Hashimoto, T. / Kawaguchi, J. et al. | 2006
- 1397
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Final Autonomous Descent Based on Target Marker Tracking AIAA Paper 2006-6538Hashimoto, T. / Kubota, T. / Sawai, S. / Kawaguchi, J. / Uo, M. et al. | 2006
- 1405
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Touchdown Dynamics for Sampling in Hayabusa Mission AIAA Paper 2006-6539Kubota, T. / Otsuki, M. / Hashimoto, T. / Bando, N. / Yano, H. / Uo, M. / Shirakawa, K. / Kawaguchi, J. et al. | 2006
- 1417
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Micro Glavity Experiment of Variable Speed Control Moment Gyro at MG-LAB AIAA Paper 2006-6650Omagari, K. / Matunaga, S. et al. | 2006
- 1427
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Robust CMG Steering Logic with Gimbal Angle Constraints AIAA Paper 2006-6651Lappas, V. / Wie, B. et al. | 2006
- 1441
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Exact steering law for pyramid-type four control moment gyro systems AIAA Paper 2006-6652Asghar, S. / Palmer, P. / Roberts, M. et al. | 2006
- 1451
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Attitude Dynamics of a Rigid Body around the Lagrangian Points AIAA Paper 2006-6653Wong, B. / Patil, R. / Misra, A. et al. | 2006
- 1462
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Stability of Fluid Motion in a Vehicle Subject to Harmonic Excitations AIAA Paper 2006-6654Kang, J. / Oh, H. et al. | 2006
- 1470
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Axial Velocity Solution for a Spinning-Up Rigid Body Subject to Constant Body-Fixed Forces and Moments AIAA Paper 2006-6655Ayoubi, M. / Longuski, J. et al. | 2006
- 1482
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Higher Accuracy Modelling of Gravity-Gradient Induced Forces and Torques AIAA Paper 2006-6656Pelivan, I. / Theil, S. et al. | 2006
- 1495
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The Application of Quaternion Algebra to Gyroscopic Motion, Navigation, and Guidance AIAA Paper 2006-6657Davailus, G. / Newman, B. et al. | 2006
- 1517
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Astrodynamics Science About Itokawa, Gravity and Ephemeris AIAA Paper 2006-6658Yoshikawa, M. / Ikeda, H. / Yano, H. / Saito, J. / Kubota, T. / Hashimoto, T. / Fujiwara, A. / Kawaguchi, J. / Kominato, T. / Matsuoka, M. et al. | 2006
- 1524
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Navigation Shape and Surface Topography Model of Itokawa AIAA Paper 2006-6659Maruya, M. / Ohyama, H. / Uo, M. / Muranaka, N. / Morita, H. / Kubota, T. / Hashimoto, T. / Saito, J. / Kawaguchi, J. et al. | 2006
- 1543
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Landmark Navigation Studies and Target Characterization in the Hayabusa Encounter with Itokawa AIAA Paper 2006-6660Gaskell, R. / Barnouin-Jha, O. / Scheeres, D. / Mukai, T. / Hirata, N. / Abe, S. / Saito, J. / Ishiguro, M. / Kubota, T. / Hashimoto, T. et al. | 2006
- 1555
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The Actual Dynamical Environment About Itokawa AIAA Paper 2006-6661Scheeres, D. / Gaskell, R. / Abe, S. / Barnouin-Jha, O. / Hashimoto, T. / Kawaguchi, J. / Kubota, T. / Saito, J. / Yoshikawa, M. / Hirata, N. et al. | 2006
- 1577
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A Lunar L2 Navigation, Communication, and Gravity Mission AIAA Paper 2006-6662Hill, K. / Parker, J. / Born, G. / Demandante, N. et al. | 2006
- 1608
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Cassini-Huygens Maneuver Experience: Second Year of Saturn Tour AIAA Paper 2006-6663Wagner, S. / Gist, E. / Goodson, T. / Hahn, Y. / Stumpf, P. / Williams, P. et al. | 2006
- 1629
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Pseudo-Doppler Velocity Navigation for Lidar-Based Planetary Exploration AIAA Paper 2006-6664de Lafontaine, J. / Neveu, D. / Hamel, J. et al. | 2006
- 1644
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Radiation Pressure Modeling for ICESat Precision Orbit Determination AIAA Paper 2006-6666Rim, H. / Webb, C. / Yoon, S. / Schutz, B. et al. | 2006
- 1650
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Communication, Ocean, and Meteorological Satellite Orbit Determination Analysis Considering Maneuver Scheme AIAA Paper 2006-6668Hwang, Y. / Lee, B. / Kim, H. / Kim, J. / Shin, H. et al. | 2006
- 1663
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13 Years of TOPEX/Poseidon Precision Orbit Determination and the 10-fold improvement in expected orbit accuracy AIAA Paper 2006-6672Lemoine, F. / Zelensky, N. / Luthcke, S. / Rowlands, D. / Chinn, D. / Beckley, B. / Klosko, S. et al. | 2006
- 1679
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Sixth US/Russian Space Surveillance Workshop AIAA Paper 2006-6673Cefola, P. / Alfriend, K. et al. | 2006
- 1696
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Mars Entry Guidance with Improved Altitude Control AIAA Paper 2006-6674Benito, J. / Mease, K. et al. | 2006
- 1708
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Atmospheric Guidance for Aero-Gravity Assist Using Matched Asymptotic Expansions AIAA Paper 2006-6675Casoliva, J. / Mease, K. et al. | 2006
- 1726
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A Comparison of Powered Descent Guidance Laws for Mars Pinpoint Landing AIAA Paper 2006-6676Ploen, S. / Acikmese, B. / Wolf, A. et al. | 2006
- 1742
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Lunar Descent Using Sequential Engine Shutdown AIAA Paper 2006-6678Springmann, P. / Proulx, R. / Fill, T. et al. | 2006
- 1760
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A Non-Deterministic Planner for Planetary Rover Autonomy AIAA Paper 2006-6679Ceriotti, M. / Vasile, M. / Giardini, G. / Massari, M. et al. | 2006
- 1780
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Autonomous Optical Navigation at Jupiter: A Linear Covariance Analysis AIAA Paper 2006-6680Stastny, N. / Geller, D. et al. | 2006
- 1793
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Experiment of Autonomous Orbit Control on DEMETER: In-Flight Results and Perspectives AIAA Paper 2006-6681Lamy, A. / Charmeau, M. / Laurichesse, D. et al. | 2006
- 1806
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Mystic: Implementation of the Static Dynamic Optimal Control Algorithm for High-Fidelity, Low-Thrust Trajectory Design AIAA Paper 2006-6741Whiffen, G. et al. | 2006
- 1818
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Comparison of Performance Predictions for New Low-Thrust Trajectory Tools AIAA Paper 2006-6742Polsgrove, T. / Kos, L. / Hopkins, R. / Crane, T. et al. | 2006
- 1836
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Overview of the Development for a Suite of Low-Thrust Trajectory Analysis Tools AIAA Paper 2006-6743Kos, L. / Polsgrove, T. / Hopkins, R. / Thomas, D. / Sims, J. et al. | 2006
- 1844
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Reduced Parameterization for Optimization of Low-Thrust Gravity-Assist Trajectories: Case Studies AIAA Paper 2006-6744Yam, C. / Longuski, J. et al. | 2006
- 1860
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Low-Thrust Trajectories to Jupiter via Gravity Assists from Venus, Earth, and Mars AIAA Paper 2006-6745Okutsu, M. / Yam, C. / Longuski, J. et al. | 2006
- 1874
-
Implementation of a Low-Thrust Trajectory Optimization Algorithm for Preliminary Design AIAA Paper 2006-6746Sims, J. / Finlayson, P. / Rinderle, E. / Vavrina, M. / Kowalkowski, T. et al. | 2006
- 1884
-
Optimization of Low-Thrust Trajectories for Formation Flying with Parallel Multiple Shooting AIAA Paper 2006-6747Massari, M. / Bernelli-Zazzera, F. et al. | 2006
- 1900
-
Periodic Solutions and Their Parametric Evolution in the Planar Case of the (n+1) Ring Problem with Oblateness Aiaa Paper 2006-6748Elipe, A. / Arribas, M. / Kalvouridis, T. et al. | 2006
- 1917
-
Lunar Frozen Orbits AIAA Paper 2006-6749Folta, D. / Quinn, D. et al. | 2006
- 1935
-
Repeat Ground Track Lunar Orbits in the Full-Potential Plus Third-Body Problem AIAA Paper 2006-6750Russell, R. / Lara, M. et al. | 2006
- 1955
-
Earth Escape Trajectories Starting from L2 Point AIAA Paper 2006-6751Nakamiya, M. / Yamakawa, H. et al. | 2006
- 1975
-
Revisiting Spacetrack Report #3 AIAA Paper 2006-6753Vallado, D. / Crawford, P. / Hujsak, R. / Kelso, T. et al. | 2006
- 2063
-
Testing of the Java Astrodynamics Toolkit Propagator AIAA Paper 2006-6754Gaylor, D. / Page, R. / Bradley, K. et al. | 2006
- 2074
-
Feasibility Study and Fuel Optimal Control Techniques for Constrained Relative Satellite Orbit Geometries AIAA Paper 2006-6758Irvin, D. / Cobb, R. et al. | 2006
- 2083
-
Second Order Relative Motion Model for Spacecraft Under J2 Perturbations AIAA Paper 2006-6759Pluym, J. / Damaren, C. et al. | 2006
- 2090
-
Addressing Nonlinear Relative Motion For Spacecraft Collision Probability AIAA Paper 2006-6760Alfano, S. et al. | 2006
- 2100
-
An Analytic Relative Orbit Model Incorporating J3 AIAA Paper 2006-6761Halsall, M. / Palmer, P. et al. | 2006
- 2112
-
Visual Monitoring of Space Rendezvous: A Structure From Motion Problem AIAA Paper 2006-6762De Rosa, D. / Curti, F. et al. | 2006
- 2125
-
Retrieving Dynamics and Control of Tethered Sampling Method for Minorbody Exploration AIAA Paper 2006-6763Matunaga, S. / Masumoto, S. / Yamanaka, T. / Mori, O. / Nakaya, K. et al. | 2006
- 2135
-
Periodic Optimal Control of a Spinning Earth-Pointing Tethered Satellite Formation AIAA Paper 2006-6764Williams, P. et al. | 2006
- 2160
-
Periodic Solutions of Electrodynamic Tethers under Forced Current Variations AIAA Paper 2006-6765Williams, P. et al. | 2006
- 2193
-
Nonlinear Control of Electro-Dynamic Tether System AIAA Paper 2006-6766Kojima, H. / Sugimoto, T. et al. | 2006
- 2210
-
Explorations of Low Cost Connections Between Lissajous Orbits from the Sun-earth and Earth-moon Systems. AIAA Paper 2006-6836Canalias, E. / Masdemont, J. et al. | 2006