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Adaptive Control - A Departure from the Certainty-Equivalence Paradigm
By: Maruthi R. Akella.
Pub. 2003, 14pgs.
PDF File. AAS 03-279.
Price: $29.00

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

Variable Structure Control With Optimized Sliding Surface for Slew Maneuver
By: Youdan Kim, Sangbum Cho, Kiseok Kim, John L. Junkins and Hyochoong Bang.
Pub. 2003, 13pgs.
PDF File. AAS 03-280.
Price: $29.00

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

Automated Operational Orbit Determination for the ICESat Mission
By: Matthew C. Meek, George H. Born, Keith S. Morris and Penina Axelrad.
Pub. 2003, 17pgs.
PDF File. AAS 03-281.
Price: $29.00

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

Precision Orbit and Attitude Determination for ICESat
By: B. Schutz, S. Bae, L. Magruder, R. Ricklefs, H. Rim, E. Silverberg, C. Webb and S. Yoon.
Pub. 2003, 12pgs.
PDF File. AAS 03-282.
Price: $29.00

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

Hamel Coefficients for the Rotational Motion of a Rigid Body
By: John E. Hurtado.
Pub. 2003, 17pgs.
PDF File. AAS 03-283.
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 Accurate Element Method: A Novel Method for Integrating Ordinary Differential Equations
By: Maty Blumenfeld and Paul Cizmas.
Pub. 2003, 16pgs.
PDF File. AAS 03-284.
Price: $29.00

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

Overview of Star Tracker Technology and its Trends in Research and Development
By: Gwanghyeok Ju and John L. Junkins.
Pub. 2003, 17pgs.
PDF File. AAS 03-285.
Price: $29.00

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

How Nonlinear Is It? — A Tutorial on Nonlinearity of Orbit and Attitude Dynamics
By: John L. Junkins and Puneet Singla.
Pub. 2003, 46pgs.
PDF File. AAS 03-286.
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 Low Cost Solid State GPS/INS Attitude Determination System
By: Gwanghyeok Ju, Changsun Yoo, Junghyun Lim and Iee-Ki Ahn.
Pub. 2003, 14pgs.
PDF File. AAS 03-287.
Price: $29.00

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

An Efficient and Robust Singular Value Method for Star Pattern Recognition and Attitude Determination
By: Jer-Nan Juang, Hye-Young Kim and John L. Junkins.
Pub. 2003, 15pgs.
PDF File. AAS 03-288.
Price: $29.00

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

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