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Further Exploration of Lamberts' Problem Using Relative Satellite Dynamics
By: William Anthony and Thomas Alan Lovell.
Pub. 2014, 15pgs.
PDF File. AAS 14-220.
Price: $29.00

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

Periodic Orbits in the Elliptical Relative Motion Problem with Space Surveillance Applications
By: Ashley D. Biria and Ryan P. Russell.
Pub. 2014, 20pgs.
PDF File. AAS 14-219.
Price: $29.00

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

Use of Cartesian-Coordinate Calibration for Satellite Relative-Motion Control
By: Andrew J. Sinclair, Ryan E. Sherrill and T. Alan Lovell.
Pub. 2014, 12pgs.
PDF File. AAS 14-218.
Price: $29.00

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

Realtive Position Control of a Two-Satellite Formation Using the SDRE Control Method
By: Mohammad Mehdi Gomroki and Ozan Tekinalp.
Pub. 2014, 20pgs.
PDF File. AAS 14-217.
Price: $29.00

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

Inverse Transformation of Relative State Transition Matrix Based on Relative Orbit Elements
By: Jianfeng Yin, Yinrul Rao and Chao Han.
Pub. 2014, 12pgs.
PDF File. AAS 14-216.
Price: $29.00

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

Relative Dynamics and Control of High Area-to-Mass Ratio Spacecraft Flying Around an Oblate Earth Exploiting Solar Radiation Pressure
By: G. Mingotti and C. McInnes.
Pub. 2014, 17pgs.
PDF File. AAS 14-215.
Price: $29.00

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

Formation Flying and Relative Dynamics Under the Circular Restricted Three-Body Problem Formulation
By: Fabio Ferrari and Michèle Lavagna .
Pub. 2014, 20pgs.
PDF File. AAS 14-214.
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 Non-Singular Keplerian Differential State Transition Matrix
By: Stefano Casotto.
Pub. 2014, 17pgs.
PDF File. AAS 14-213.
Price: $29.00

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

Initial Relative Orbit Determination Performance Analysis in Cylindrical Coordinates Using Angles-Only Measurements
By: David K. Geller and T. Alan Lovell.
Pub. 2014, 17pgs.
PDF File. AAS 14-212.
Price: $29.00

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

Relative Orbital Motion and Angles-Only Relative State Observability in Cylindrical Coordinates
By: David K. Geller and T. Alan Lovell.
Pub. 2014, 16pgs.
PDF File. AAS 14-211.
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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