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A Two-Level Differential Corrections Algorithm for Low-Thrust Spacecraft Trajectory Targeting
By: Collin E. York and Kathleen C. Howell.
Pub. 2019, 20pgs.
PDF File. AAS 19-356.
Price: $29.00

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

Science Orbits for the Lunar CubeSat Equuleus and for the Phobos Sample Return Mission
By: Takuya Chikazawa, Nicola Baresi,† Naoya Ozaki, Stefano Campagnola and Yasuhiro Kawakatsu.
Pub. 2019, 15pgs.
PDF File. AAS 19-389.
Price: $29.00

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

Multi-Objective Optimization of Low Thrust Trajectories for Propellant Mass, Time of Flight, and Radiation Dose
By: Christopher G. Lorenz, Lake A. Singh and Jose J. Guzman.
Pub. 2019, 12pgs.
PDF File. AAS 19-398.
Price: $29.00

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

A Relaxation Approach for Hybrid Multi-Objective Optimal Control: Application to Multiple Debris Removal Missions
By: Lorenzo A. Ricciardi and Massimiliano Vasile.
Pub. 2019, 20pgs.
PDF File. AAS 19-406.
Price: $29.00

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

Low Energy Escape Using Tube Dynamics Associated with Quasi-Halo Orbit
By: Kazutoshi Takemura, Nicola Baresi, Yasuhiro Kawakatsu and Hiroaki Yoshimura.
Pub. 2019, 11pgs.
PDF File. AAS 19-408.
Price: $29.00

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

Quasi-Satellite Orbit Transfers via Multi-Revolutional Periodic Orbits
By: Kento Ichinomiya, Nicola Baresi, Yasuhiro Kawakatsu and Tomohiro Yanao.
Pub. 2019, 20pgs.
PDF File. AAS 19-422.
Price: $29.00

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

Integrated Optimization of Ascent Trajectory and SRM Desing of Multistage Launch Vehicles
By: Lorenzo Federici, Alessandro Zavoli, Guido Colasurdo, Lucandrea Mancini and Agostino Neri.
Pub. 2019, 20pgs.
PDF File. AAS 19-424.
Price: $29.00

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

Using the Paramat System in Mission Analysis and Design
By: Darrel J. Conway and Darren D. Garber.
Pub. 2019, 11pgs.
PDF File. AAS 19-442.
Price: $29.00

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

Series Solution for Motion in an Arbitrary Potential Field
By: Nathan Strange.
Pub. 2019, 16pgs.
PDF File. AAS 19-443.
Price: $29.00

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

Q-Law Aided Direct Trajectory Optimization for the High-Fidelity, Many-Revolution Low-Thrust Orbit Transfer Problem
By: Jackson L. Shannon, Martin T. Ozimek, Justin A. Atchison and Christine M. Hartzell.
Pub. 2019, 20pgs.
PDF File. AAS 19-448.
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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