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.
Author:C. Deagle, Jr.
Downloaded file size:209,196 bytes
Size on calculator:19 KB
User rating:Not yet rated (you must be logged in to vote)
Primary category:Science
File date:2022-11-14 13:13:30
Creation date:2022-11-14
Source code:Included
Download count:57
Version history:2023-05-28: Added to site
Archive contents:
  Length      Date    Time    Name
---------  ---------- -----   ----
   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
---------                     -------
   256777                     4 files
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