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Optimal Impulsive Satellite Transfers using Second-Order Solutions of Relative Motion
By: Weijun Huang.
Pub. 2010,
19pgs.
PDF File.
AAS 10-264.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Passively Safe Relative Motion Trajectories for On-Orbit Inspection
By: Liam M. Healy and C. Glen Henshaw.
Pub. 2010,
20pgs.
PDF File.
AAS 10-265.
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 Variational Method for the Propagation of Spacecraft Relative Motion
By: Giulio Baù, Claudio Bombardelli, Jesús Peláez, Enrico Lorenzini and Alessandro Francesconi.
Pub. 2010,
16pgs.
PDF File.
AAS 10-266.
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 Control of Multiple Rigid Body Spacecraft with Flexible Hinge Joints
By: Burak Akbulut, Kemal Ozgoren and Ozan Tekinalp.
Pub. 2010,
18pgs.
PDF File.
AAS 10-267.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Impact of Nodal Attitude Motion on Two-Element Tethered Coulomb Structures
By: Carl R. Seubert and Hanspeter Schaub.
Pub. 2010,
20pgs.
PDF File.
AAS 10-268.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Performance Analysis of Bare Electrodynamic Tethers as MicroSat Deorbiting Systems
By: Claudio Bombardelli, Jose Manuel Nuñez-Ayllón and Jesús Peláez.
Pub. 2010,
8pgs.
PDF File.
AAS 10-269.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Space Debris Removal with Bare Electrodynamic Tethers
By: Claudio Bombardelli, Javier Herrera-Montojo, Ander Iturri-Torrea and Jesús Peláez.
Pub. 2010,
11pgs.
PDF File.
AAS 10-270.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Validation of Tethered Satellite System Computational Models
By: Joshua R. Ellis and Christopher D. Hall.
Pub. 2010,
17pgs.
PDF File.
AAS 10-271.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Relative Equilibria of a Moon - Tethered Spacecraft
By: Alexander A. Burov, Oleg I. Kononov and Anna D. Guerman.
Pub. 2010,
10pgs.
PDF File.
AAS 10-272.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Rigid Body Attitude Stabilization with Unknown Time-Varying Delay in Feedback
By: Apurva Chunodkar and Maruthi R. Akella.
Pub. 2010,
16pgs.
PDF File.
AAS 10-274.
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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