Earth Orbit Lambert Problem |
| Description: | Solves the Earth orbit Lambert problem. The user provides classical orbital elements for an initial and final orbit, and the time required to transfer from the initial to final orbits. |
| Filename: | demo_lambert.zip |
| ID: | 9466 |
| Author: | C. Deagle, Jr. |
| Downloaded file size: | 499,655 bytes |
| Size on calculator: | 56 KB |
| Platforms: | Prime |
| User rating: | Not yet rated (you must be logged in to vote) |
| Primary category: | Science |
| Languages: | ENG |
| File date: | 2022-09-29 12:47:34 |
| Creation date: | 2022-09-29 |
| Source code: | Included |
| Download count: | 124 |
| Version history: | 2023-05-28: Added to site
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| Archive contents: | Length Date Time Name
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56458 2022-09-29 10:06 demo_lambert.hpprgm
4295 2022-09-29 12:47 demo_lambert.html
28056 2022-09-29 10:11 demo_lambert.txt
561048 2022-09-29 10:09 lambert.pdf
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649857 4 files |
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| User comments: | No comments at this time. |
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