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Deployment of Spacecraft Large Formations
By: Giovanni B. Palmerini.
Pub. 2003, 7pgs.
PDF File. AAS 03-111.
Price: $29.00

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

Control Strategies for Formation Flight in the Vicinity of the Libration Points
By: K. C. Howell and B. G. Marchand.
Pub. 2003, 24pgs.
PDF File. AAS 03-113.
Price: $29.00

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

Suppose A(t) Isn’t Constant
By: William E. Wiesel.
Pub. 2003, 7pgs.
PDF File. AAS 03-114.
Price: $29.00

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

Incorporating Secular Drifts into the Orbit Element Difference Description of Relative Orbits
By: Hanspeter Schaub.
Pub. 2003, 18pgs.
PDF File. AAS 03-115.
Price: $29.00

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

Probabilistic Optimization Applied to Spacecraft Rendezvous and Docking
By: Jeff M. Phillips, Lydia E. Kavraki and Nazareth Bedrossian.
Pub. 2003, 14pgs.
PDF File. AAS 03-116.
Price: $29.00

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

Minimum-Time Orbital Phasing Maneuvers
By: Christopher D. Hall and Victor Collazo Perez.
Pub. 2003, 18pgs.
PDF File. AAS 03-117.
Price: $29.00

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

Optimal Rephasing Problem
By: Dario Izzo and Chiara Valente.
Pub. 2003, 14pgs.
PDF File. AAS 03-118.
Price: $29.00

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

Trajectory Optimization of a Constrained Mission About a Libration Point
By: S. Infeld and W. Murray.
Pub. 2003, 10pgs.
PDF File. AAS 03-119.
Price: $29.00

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

Trajectory Optimization for a Mission to NEOS, Using Low-Thrust Propulsion and Gravity Assist
By: Mauro Massari, Franco Bernelli-Zazzera and Massimiliano Vasile.
Pub. 2003, 14pgs.
PDF File. AAS 03-120.
Price: $29.00

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

Computation of Optimal Mars Trajectories Via Combined Chemical/ Electrical Propulsion, Part 2: Minimum Time Solutions With Bounded Thrust Direction
By: A. Miele, T. Wang and P. N. Williams.
Pub. 2003, 30pgs.
PDF File. AAS 03-121.
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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