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Design of Lunar Gravity-Assist for the BepiColombo Mission to Mercury
By: Stefano Campagnola, Rüdiger Jehn and Carlos Corral Van Damme.
Pub. 2005,
15pgs.
PDF File.
AAS 04-130.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Nozomi Earth Swingby Orbit Determination
By: Mark Ryne and Sumita Nandi.
Pub. 2005,
19pgs.
PDF File.
AAS 04-131.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
End-to-End Mission Analysis for a Low-Cost, Two-Spacecraft Mission to Europa
By: Michael Khan, Stefano Campagnola and Michael Croon.
Pub. 2005,
11pgs.
PDF File.
AAS 04-132.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Evaluation of an Energy-Cutoff Algorithm for the Saturn Orbit Insertion Burn of the Cassini-Huygens Mission
By: Troy Goodson.
Pub. 2005,
17pgs.
PDF File.
AAS 04-133.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
1-AU Calibration Activities for Stardust Earth Return
By: Brian M. Kennedy, Eric Carranza and Kenneth E. Williams.
Pub. 2005,
18pgs.
PDF File.
AAS 04-134.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Geometric Analysis of Visibility of Mission Support Infrastructure for Phobos and Deimos
By: William J. Chadwick III, David B. Spencer, and Robert G. Melton.
Pub. 2005,
26pgs.
PDF File.
AAS 04-135.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
New Horizons Pluto Approach Navigation
By: James K. Miller, Dale R. Stanbridge and Bobby G. Williams.
Pub. 2005,
12pgs.
PDF File.
AAS 04-136.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Options for Optimal Trajectory Design of a Mission to NEOs Using Low-Thrust Propulsion
By: Mauro Massari and Franco Bernelli-Zazzera.
Pub. 2005,
12pgs.
PDF File.
AAS 04-137.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Time-Varying Potential Function Control for Constrained Attitude Tracking
By: Massimo Casasco and Gianmarco Radice.
Pub. 2005,
20pgs.
PDF File.
AAS 04-138.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Attitude and Position Estimation from Vector Observations
By: Daniele Mortari, J. Maurice Rojas and John L. Junkins.
Pub. 2005,
18pgs.
PDF File.
AAS 04-140.
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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