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| ID No : | 837 Edit | Title: | Theoretical Foundation of Copernicus: A Unified System for Trajectory Design and Optimization |
| Summary / Review : | "The fundamental methods are described for the general spacecraft trajectory design and optimization software system called Copernicus. The methods rely on a unified framework that is used to model, design, and optimize spacecraft trajectories that may operate in complex gravitational force fields, use multiple propulsion systems, and involve multiple spacecraft. The trajectory model, with its associated equations of motion and maneuver models, are discussed." (Author's abstract) |
| Author(s) : |
Ocampo, Cesar; Senent, Juan S.; Williams, Jacob, [Johnson Space Center] |
| Publication Date: | 2010 |
| Category(s) : |
Transportation / Interorbital / Trajectories |
| Progress Type: | A ( A=Analysis only, D=Design, T=Testing, C=Completed or Commercial product ) |
| Web URL : |
http://hdl.handle.net/2060/20100017708
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| PERMANENT code(s) : | L,U |
|
(Explanation of the last 3 rows above) |
In the row above, there are up to 4 possibilities: U = URL you can click on to get a copy instantly from another source on the internet, or request it from that source D = Downloadable from PERMANENT (such as because no other URL known...) L = LAN copy, PERMANENT has a digital copy but not downloadable from our website P = Paper copy in the PERMANENT office Typically, only 0 to 3 methods are available. |
| NTRS : | 20100017708 |
| Other Ref # : | JSC-CN-20552 |
| Submitted by : | MEP |
| Comments: |
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