Univelt, Inc: Individual AAS Papers

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Attitude Determinination and Control for the Global Imaging System 2000
By: Doug Wiemer.
Pub. 1998, 21pgs.
PDF File. AAS 98-012.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

Applications of Neural Networks to the Satellite Attitude Control Problem
By: Gustavo Riestra Rodriguez and Jordi Puig-Suari.
Pub. 1997, 20pgs.
PDF File. AAS 97-662.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

An Analytic Approach to Optimal Rendezvous Using the Der-Danchick Equations
By: Gim J. Der and Roy Danchick.
Pub. 1997, 20pgs.
PDF File. AAS 97-647.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

Optimization of Satellite Constellations for Discontinuous Global Coverage via Genetic Algorithms
By: Eric R. George.
Pub. 1997, 14pgs.
PDF File. AAS 97-621.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

Some Consequences of Force Model Uncertainty on Probability of Collision with Orbital Debris
By: Maruthi R. Akella, John L. Junkins and Kyle T. Alfriend.
Pub. 1998, 11pgs.
PDF File. AAS 97-606.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

NEAR Guidance and Control System
By: T. E. Strikwerda, J. C. Ray, D. R. Haley, G. A. Hayler, H. L. Fisher, and R. T. N. Pham.
Pub. 1997, 21pgs.
PDF File. AAS 97-077.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

Mission Plan For Mars Global Surveyor
By: Wayne Lee and Wayne Sidney.
Pub. 1996, 20pgs.
PDF File. AAS 96-153.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

HIGH FIDELITY MATHEMATICAL MODELING OF REACTTON WHEEL PERFORMANCE
By: Bill Bialke.
Pub. 1998, 14pgs.
PDF File. AAS 96-033.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

Analysis of the CT-633 Star Tracker's Attitude Estimation Capability
By: Thomas Bank and Ian J. Gravseth.
Pub. 1996, 21pgs.
PDF File. AAS 96-007.
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 Optimization of Initial Inclination for a Desired Sun-Synchronous Orbit
By: C. C. Chao and R. G. Gist.
Pub. 1996, 12pgs.
PDF File. AAS 95-333.
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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