Univelt, Inc: Individual AAS Papers

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An Heuristic Aproach to the Problem of Initial Orbit Determination: A Test Case with Geo Observations
By: L. Ansalone and F. Curti.
Pub. 2015, 20pgs.
PDF File. 14-525.
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 Stabilization of a Charged Spacecraft Subject to Lorentz Force
By: Yehia A. Abdel-Aziz and Muhammad Shoaib.
Pub. 2015, 14pgs.
PDF File. 14-524.
Price: $29.00

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

Low-Orbital Transformable Nanosatellite: Research of the Dynamics and Possibilities of Navigational and Communication Problems Solving for Passive Aerodynamic Stabilization
By: I. V. Belokonov, A. V. Kramlikh and I. A. Timbai.
Pub. 2015, 15pgs.
PDF File. 14-523.
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 Evaluation of the Inverse Dynamics Method for Optimal Spacecraft Reorientation
By: Jacopo Ventura, Marcello Romano and Ulrich Walter.
Pub. 2015, 19pgs.
PDF File. 14-522.
Price: $29.00

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

B-DOT Moment Offset Control Algorithm for Geo-Magnetic Field Pointing IITMSAT
By: B. Praneeth Kumar. B. Sruteesh Kumar, C. Sujatha and Sandipan Bandyopadhyay.
Pub. 2015, 10pgs.
PDF File. 14-521.
Price: $29.00

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

Robust Three-Axis Attitude Stabilization for Inertial Pointing Spacecraft Using Magnetorquers
By: Fabio Celani.
Pub. 2015, 20pgs.
PDF File. 14-520.
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 Geometric Method for Analyzing the Orthogonal Responses and Eigenfrequencies of Gravity Gradient Stabilized Satellites
By: A. E. (Arthur) Overlack and J. M. (Hans) Kulper.
Pub. 2015, 19pgs.
PDF File. 14-519.
Price: $29.00

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

Intermediaries for Gravity-Gradient Attitude Dynamics I. Action-Angle Variables
By: Sebastián Ferrer and Francisco J. Molero.
Pub. 2015, 20pgs.
PDF File. 14-518.
Price: $29.00

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

Active Magnetic Attitude Control System Providing Three-Axis Inertial Attitude
By: M. Ovchinnikov, V. Penkov, D. Roldugin and A Guerman.
Pub. 2015, 13pgs.
PDF File. 14-516.
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 Dynamics of a Spacecraft with a Solar Stabilizer
By: Vladislav Sidorenko.
Pub. 2015, 6pgs.
PDF File. 14-515.
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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