View Issue Details
|ID||Project||Category||View Status||Date Submitted||Last Update|
|0000001||Memorandum Series||Memorandum #1: Keplerian Orbit Elements to Cartesian State Vectors||public||2013-04-30 10:11||2013-04-30 21:28|
|Priority||normal||Severity||minor||Reproducibility||have not tried|
|Summary||0000001: Step 6 - Error in the transformation formula 8 and 9|
As I was looking for Keplerian orbit elements, I found your memo. Great work, with nice présentation, références.
I thinks there is an error in the formulas 8 and 9, where o stands for Omega, the longitude of the ascending node Actual Formula is :
The correct formula is :
Frederic Baudrand email@example.com
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thank you very much for your bug report. Of course you are right --- there was a minus sign, were a plus sign had to be. The typo has now been corrected; you can find the corrected version in my download center.
I appreciate your efforts.
Kind regards, René
|2013-04-30 10:11||DigNative||New Issue|
|2013-04-30 21:28||DigNative||Note Added: 0000001|
|2013-04-30 21:28||DigNative||Assigned To||=> DigNative|
|2013-04-30 21:28||DigNative||Status||new => assigned|
|2013-04-30 21:28||DigNative||Status||assigned => resolved|
|2013-04-30 21:28||DigNative||Resolution||open => fixed|
|2013-04-30 21:28||DigNative||Status||resolved => closed|