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Near Optimal Finite-Time Feedback Control Synthesis Using the SDRE-Based Approach Extended for Nonlinear Terminal Hypersurfaces
By: Rajnish Sharma and George W. P. York.
Pub. 2017, 20pgs.
PDF File. AAS 17-243.
Price: $29.00

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Low-Thrust Many-revolution Trajectory Optimization via Differential Dynamic Programming and a Sundman Transformation
By: Jonathan D. Aziz, Jeffrey S. Parker, Daniel J. Scheeres and Jacob A. Englander.
Pub. 2017, 20pgs.
PDF File. AAS 17-253.
Price: $29.00

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Atmospheric Modeling Using Accelerometer Data During Mars Atmosphere and Volatile Evolution (MAVEN) Flight Operations
By: Robert H. Tolson, Rafael A. Lugo, Darren T. Baird, Alicia D. Cianciolo, Stephen W. Bougher and Richard M. Zurek.
Pub. 2017, 16pgs.
PDF File. AAS 17-273.
Price: $29.00

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Asteroid Deflection with Safe Harbors Found via Numerical Optimization
By: Bruce A. Conway, Siegfried Eggl and Daniel Hestroffer.
Pub. 2017, 11pgs.
PDF File. AAS 17-281.
Price: $29.00

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Global Search for Low-Energy Transfers to the Moon with Long Transfer Time
By: Kenta Oshima, Francesco Topputo and Tomohiro Yanao.
Pub. 2017, 18pgs.
PDF File. AAS 17-299.
Price: $29.00

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Combining Non-Linear Programming and Hyperheuristic Algorithms for Low-Thrust Trajectory Optimization
By: Lake A. Singh, Jose J, Guzman, Christopher L. Ranieri, Demyan V. Lantukh and Gregory Fruth.
Pub. 2017, 11pgs.
PDF File. AAS 17-303.
Price: $29.00

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Teo-Impulse Evolutionary Optimization of Satellite Formation Trajectories Over Multiple Revolutions with Topological Contstraints
By: David W. Hinckley Jr. and Darren L. Hitt.
Pub. 2017, 13pgs.
PDF File. AAS 17-309.
Price: $29.00

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Using Particle Swarm Optimization for Earth-Return Trajectories from Libration Point Orbits
By: Mollik Nayyar and David B. Spencer.
Pub. 2017, 19pgs.
PDF File. AAS 17-410.
Price: $29.00

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Multi-Tiered Approach to Constellation Maneuver Optimization for Low-Thrust Station-Keeping
By: Andris D. Jaunzemis, Christopher W. T. Roscoe and Marcus J. Holzinger.
Pub. 2017, 20pgs.
PDF File. AAS 17-416.
Price: $29.00

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A Time-Regularized, Multiple Gravity-Assist Low-Thrust, Bounded-Impulse Model for Trajectory Optimization
By: Donald H. Ellison, Jacob A. Englander and Bruce A. Conway.
Pub. 2017, 14pgs.
PDF File. AAS 17-429.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

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