State Vector to C3, RLA and DLA |
| Description: | Calculates C3 (twice the specific (per unit mass) orbital energy), RLA (the right ascension) and DLA (declination) of the asymptote of a hyperbolic trajectory. This computer program assumes that the hyperbolic targets, state vector and classical orbital elements are all in the same Earth-centered-inertial (ECI) coordinate system. |
| Filename: | demo_rv2hyper.zip |
| ID: | 9469 |
| Author: | C. Deagle, Jr. |
| Downloaded file size: | 209,196 bytes |
| Size on calculator: | 19 KB |
| Platforms: | Prime |
| User rating: | Not yet rated (you must be logged in to vote) |
| Primary category: | Science |
| Languages: | ENG |
| File date: | 2022-11-14 13:13:30 |
| Creation date: | 2022-11-14 |
| Source code: | Included |
| Download count: | 79 |
| Version history: | 2023-05-28: Added to site
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| Archive contents: | Length Date Time Name
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226140 2022-11-14 10:38 demo_hyper.pdf
19084 2022-11-14 10:35 demo_rv2hyper.hpprgm
2609 2022-11-14 14:13 demo_rv2hyper.html
8944 2022-11-14 10:36 demo_rv2hyper.txt
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256777 4 files |
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