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  • About
  • The Global ETD Search service is a free service for researchers to find electronic theses and dissertations. This service is provided by the Networked Digital Library of Theses and Dissertations.
    Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
1

Characteristic velocity requirements for rendezvous between non co-planar orbits

Fraser, Robert Bruce, 1939- January 1963 (has links)
No description available.
2

Analysis of relative motion and thrust requirements in the terminal phase of rendezvous

Daugherty, William Lester, 1928- January 1963 (has links)
No description available.
3

Characterization of the relative motion of rendezvous between vehicles in proximate, highly elliptic orbits /

Olsen, Carrie Dumas, January 2001 (has links)
Thesis (Ph. D.)--University of Texas at Austin, 2001. / Vita. Includes bibliographical references (leaves 183-185). Available also in a digital version from Dissertation Abstracts.
4

Model predictive control for spacecraft rendezvous

Hartley, Edward Nicholas January 2010 (has links)
No description available.
5

A homotopy approach to the solutions of minimum-fuel space-flight rendezvous problems

Vasudevan, Gopal January 1989 (has links)
A homotopy approach for solving constrained parameter optimization problems is examined. The first order necessary conditions, with the complementarity conditions represented using a technique due to Mangasarian, are solved. The equations are augmented to avoid singularities which occur when the active constraint set changes. The Chow-Yorke algorithm is used to track the homotopy path leading to the solution to the desired problem at the terminal point. Since the Chow-Yorke algorithm requires a fairly accurate computation of the Jacobian matrix, analytical representation of the system of equations is desired. Consequently, equations obtained using the true anomaly regularization of the governing equations were employed for the above purpose. A homotopy map suited for the space-flight rendezvous problem including a minimum radius constraint is developed, which can naturally deform any initial problem into some other valid desired problem. Several coplanar and non-coplanar solutions for circular and elliptic cases have been presented for the restricted time problem with a minimum radius constraint. / Ph. D.

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