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Perturbations of Gravity Field on a Flight Formation for an Eccentric Reference Frame
By: Jordi Fontdecaba Baig, Gilles Métris, F. Deleflie and Pierre Exertier.
Pub. 2007,
13pgs.
PDF File.
AAS 07-297.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Development and Control Scheme Solution for the Perturbed Motion of a Constellation in an Elliptical Orbit
By: Pedro A. Capó-Lugo and Peter M. Bainum.
Pub. 2007,
20pgs.
PDF File.
AAS 07-298.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Fuel-Equivalent Relative Orbit Element Space
By: Jean-Francois Hamel and Jean de Lafontaine.
Pub. 2007,
16pgs.
PDF File.
AAS 07-300.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Linearized Dynamics of Formation Flying Spacecraft on a J2-Perturbed Elliptical Orbit
By: Jean-Francois Hamel and Jean de Lafontaine.
Pub. 2007,
23pgs.
PDF File.
AAS 07-301.
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 Interferometric Image Acquisition via Multi-Spacecraft Formation Maneuvering - Special Cases of Optimality
By: Haithem A. Al-Twaijry and David C. Hyland.
Pub. 2007,
16pgs.
PDF File.
AAS 07-302.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Efficient, Passively Orbiting Constellations for High Resolution Imaging of Geosynchronous Objects
By: David C. Hyland.
Pub. 2007,
17pgs.
PDF File.
AAS 07-303.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
3 -D Trajectory Optimization Satisfying Waypoints and No-Fly Zone Constraints
By: Timothy R. Jorris and Richard G. Cobb.
Pub. 2007,
28pgs.
PDF File.
AAS 07-304.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Six-Degree-of-Freedom Trajectory Optimization for Reusable Launch Vehicle Footprint Determination
By: Kevin P. Bollino, I. Michael Ross and David B. Doman.
Pub. 2007,
20pgs.
PDF File.
AAS 07-305.
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 Trajectories for Maneuvering Re-entry Vehicles
By: Aditya Undurti, Ronald J. Proulx, James A. Shearer and Roy H. Setturlund.
Pub. 2007,
22pgs.
PDF File.
AAS 07-306.
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 and Aerothermodynamic Analysis of Towed-Ballute Aerocapture Using Direct Simulation Monte Carlo
By: Kristin L. Gates Medlock, Alina A. Alexeenko and James M. Longuski.
Pub. 2007,
18pgs.
PDF File.
AAS 07-307.
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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