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Representations of Invariant Manifolds for Applications in Three-Body Systems
By: K. Howell, M. Beckman, C. Patterson and D. Folta.
Pub. 2005,
19pgs.
PDF File.
AAS 04-287.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
The Role of Invariant Manifolds in Low Thrust Trajectory Design
By: Martin W. Lo, Rodney L. Anderson, Gregory Whiffen and Larry Romans.
Pub. 2005,
20pgs.
PDF File.
AAS 04-288.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Application of Dynamical Systems Theory to a Very Low Energy Transfer
By: Shane D. Ross, Wang Sang Koon, Martin W. Lo and Jerrold E. Marsden.
Pub. 2005,
13pgs.
PDF File.
AAS 04-289.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Coupled Effects of Initial Orbit Plane on Orbit Lifetime in the Three-Body Problem
By: Christopher J. Scott and David B. Spencer.
Pub. 2005,
11pgs.
PDF File.
AAS 04-290.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
The Dynamics of Orbits in a Potential Field of a Solid Circular Ring
By: Roger A. Broucke and Antonio Elipe.
Pub. 2005,
20pgs.
PDF File.
AAS 04-291.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Orbits Around an Elongated 3D-Object
By: Roger A. Broucke and Antonio Fernando Bertachini de Almeida Prado.
Pub. 2005,
24pgs.
PDF File.
AAS 04-292.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Lambert’s Theorem - A Complete Series Solution
By: James D. Thorne.
Pub. 2005,
13pgs.
PDF File.
AAS 04-293.
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 Spacecraft Motion: A Hamiltonian Approach to Eccentricity Perturbations
By: Egemen Kolemen and N. Jeremy Kasdin.
Pub. 2005,
11pgs.
PDF File.
AAS 04-294.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Satellite Constellation Design for Mid-Course Ballistic Missile Intercept
By: Luke M. Sauter, Ronald J. Proulx and Howard Musoff.
Pub. 2005,
19pgs.
PDF File.
AAS 04-295.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Close Spacecraft Formation Keeping
By: Pierre Vignal and Henry Pernicka.
Pub. 2005,
18pgs.
PDF File.
AAS 04-296.
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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