W-S5 Spacecraft Primrose AAS 15-547 Nermin 15:50 - 16:10 Feedback Tracking Control Based On A Trajectory-Specific Finite-Time Causal Inverse GNC - 3 W-S7 Trajectory Larkspur AAS 15-800 Georges Krier 15:50 - 16:10 Fast and robust optimization of high fidelity low thrust transfer orbits with constraints Design and Optimization - 6 W-S8 Asteroid and Rocky C/D AAS 15-721 Samuel 16:10 - 16:30 Inflatable Sail for Asteroid Capture Non Earth Orbiting Ximenes Missions W-S6 Orbital Debris Rocky A/B AAS 15-631 Hyun Chul Ko 16:10 - 16:30 Maneuver Detection with Event Representation using Thrust-Fourier-Coefficients and Conjunction Analysis W-S5 Spacecraft Primrose AAS 15-548 Zhaohui Wang 16:10 - 16:30 Vector Control of Upper Stage with Uncertainty of the Centroid GNC - 3 W-S8 Asteroid and C/D AAS 15-739 Michele 16:30 - 16:50 The European Asteroid Impact Mission: phase A design and Mission Analysis Non Orbiting Lavagna Missions W-S6 Orbital Debris Rocky A/B AAS 15-635 Francois 16:30 - 16:50 QUANTIFICATION IN OPTICAL OBSERVATIONS OF RESIDENT SPACE and Conjunction Sanson OBJECTS FOR PROBABILITY OF DETECTION AND LIKELIHOOD Analysis W-S5 Spacecraft Primrose AAS 15-554 Jianjun Luo 16:30 - 16:50 MULTI-CONSTRAINT HANDLING AND A MIXED INTEGER PREDICTIVE GNC - 3 CONTROLLER FOR SPACE ROBOTS WITH OBSTACLE AVOIDANCE W-S7 Trajectory Larkspur AAS 15-682 Yanning Guo 16:30 - 16:50 Fuel-efficient Planetary Landing Guidance with Hazard Avoidance Design and Optimization - 6 W-S8 Asteroid and Rocky C/D AAS 15-786 Reza Raymond 16:50 - 17:10 PREDICTION OF ASTEROID TRAJECTORY DEFLECTION DUE TO ALBEDO Non Orbiting Karimi CHANGE: An APPLICATION TO APOPHIS DEFLECTION Missions W-S6 Orbital Debris Rocky A/B AAS 15-697 Jacco Geul 16:50 - 17:10 REGULARISED METHODS FOR HIGH-EFFICIENCY PROPAGATION and Conjunction Analysis
W-S5 Spacecraft GNC - 3 Primrose AAS 15-547 Nermin 15:50 - 16:10 Feedback Tracking Control Based On A Trajectory-Specific Finite-Time Causal Inverse W-S7 Trajectory Design and Optimization - 6 Larkspur AAS 15-800 Georges Krier 15:50 - 16:10 Fast and robust optimization of high fidelity low thrust transfer orbits with constraints W-S8 Asteroid and Non Earth Orbiting Missions Rocky C/D AAS 15-721 Samuel Ximenes 16:10 - 16:30 Inflatable Sail for Asteroid Capture W-S6 Orbital Debris and Conjunction Analysis Rocky A/B AAS 15-631 Hyun Chul Ko 16:10 - 16:30 Maneuver Detection with Event Representation using Thrust-Fourier-Coefficients W-S5 Spacecraft GNC - 3 Primrose AAS 15-548 Zhaohui Wang 16:10 - 16:30 Vector Control of Upper Stage with Uncertainty of the Centroid W-S8 Asteroid and Non Orbiting Missions C/D AAS 15-739 Michele Lavagna 16:30 - 16:50 The European Asteroid Impact Mission: phase A design and Mission Analysis W-S6 Orbital Debris and Conjunction Analysis Rocky A/B AAS 15-635 Francois Sanson 16:30 - 16:50 QUANTIFICATION IN OPTICAL OBSERVATIONS OF RESIDENT SPACE OBJECTS FOR PROBABILITY OF DETECTION AND LIKELIHOOD W-S5 Spacecraft GNC - 3 Primrose AAS 15-554 Jianjun Luo 16:30 - 16:50 MULTI-CONSTRAINT HANDLING AND A MIXED INTEGER PREDICTIVE CONTROLLER FOR SPACE ROBOTS WITH OBSTACLE AVOIDANCE W-S7 Trajectory Design and Optimization - 6 Larkspur AAS 15-682 Yanning Guo 16:30 - 16:50 Fuel-efficient Planetary Landing Guidance with Hazard Avoidance W-S8 Asteroid and Non Orbiting Missions Rocky C/D AAS 15-786 Reza Raymond Karimi 16:50 - 17:10 PREDICTION OF ASTEROID TRAJECTORY DEFLECTION DUE TO ALBEDO CHANGE: An APPLICATION TO APOPHIS DEFLECTION W-S6 Orbital Debris and Conjunction Analysis Rocky A/B AAS 15-697 Jacco Geul 16:50 - 17:10 REGULARISED METHODS FOR HIGH-EFFICIENCY PROPAGATION
ASC2015_Schedule_at_a_Glance_31Jul2015.docx