[First Page] [Prev] Showing page 277 of 891 pages [Next] [Final Page]

Three-Axis Magnetic Attitude Control Using Pseudospectral Control Law
By: Hui Yan, I. Michael Ross and Kyle T. Alfriend.
Pub. 2006, 19pgs.
PDF File. AAS 05-417.
Price: $29.00

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

Gimbal-Position Command Generation for a Cluster of Control Moment Gyroscopes
By: Giulio Avanzini.
Pub. 2006, 12pgs.
PDF File. AAS 05-418.
Price: $29.00

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

Singularity-Free Optimal Steering of Control Moment Gyros
By: Andrew Fleming and I. Michael Ross.
Pub. 2006, 20pgs.
PDF File. AAS 05-419.
Price: $29.00

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

Quaternion-Based Satellite Attitude Control Using Fuzzy Logic
By: Mélanie Bélanger and Jean de Lafontaine.
Pub. 2006, 11pgs.
PDF File. AAS 05-420.
Price: $29.00

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

Further Results in Reduced Order Compensators for Dynamic Systems Using LQG/LTR Methods
By: Donald L. Mackison and Andrew Sivess.
Pub. 2006, 16pgs.
PDF File. AAS 05-422.
Price: $29.00

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

WMAP Solar Radiation Pressure Modeling During February 2005 Reaction Wheel Power Off Anomaly
By: Dale R. Fink.
Pub. 2006, 7pgs.
PDF File. AAS 05-423.
Price: $29.00

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

Study on the Station Keeping Maintenance for the TPF Mission
By: G. Gómez, M. W. Lo and J. J. Masdemont.
Pub. 2006, 14pgs.
PDF File. AAS 05-424.
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 Control Configured Small Circular Halo Orbit Around L2
By: Kohta Tarao and Jun’ichiro Kawaguchi.
Pub. 2006, 10pgs.
PDF File. AAS 05-425.
Price: $29.00

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

Using Hill’s 3-Body Equations to Approximate the Genesis Libration Trajectory
By: Nicholas G. Smith, Vincent C. Herr and Brandon S. Smith.
Pub. 2006, 13pgs.
PDF File. AAS 05-426.
Price: $29.00

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

Libration Points of a Gyrostat in a Generalized Restricted Three-Body Problem: Linear Stability
By: J. A. Vera and A. Vigueras.
Pub. 2006, 20pgs.
PDF File. AAS 05-427.
Price: $29.00

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

[First Page] [Prev] Showing page 277 of 891 pages [Next] [Final Page]