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Releases: IO-Aerospace-software-engineering/Astrodynamics

Release v8.0 Preview - Atmospheric model

30 Dec 14:16
c9ef46f

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Full Changelog: v7.1.0...v8.0.0-preview

Release v7.1.0 - upgrade to .Net 10

08 Dec 17:30
dd37404

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Full Changelog: v7.0.4...v7.1.0

Release v7.0.4 - Fix RID parameters

05 Dec 15:19
54730d2

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Full Changelog: v7.0.3...v7.0.4

Release v7.0.3 - Create TLE from osculating elements

31 Oct 13:38
672c6e3

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Full Changelog: v6.5.1...v7.0.3

Release v7.0.2-Preview2 - Create TLE from orbital parameters

01 Oct 12:20

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Full Changelog: v7.0.1-preview...v7.0.2-preview

Release v7.0.1-Preview1 - Create TLE from orbital parameters

04 Aug 20:59

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What's new

TLE has been upgraded, you can now convert orbital params to TLE

Release v7.0.0-Preview1 - Create TLE from orbital parameters

04 Aug 20:38
da18122

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Full Changelog: v6.5.1...v7.0.0-preview1

Release v6.5.1 - Fix Time frame

20 Jul 15:18
4d67196

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When you use ReadEpehemeris in low level API, the function returns statevector in TDB Frame instead of time frame used in time window

How to install : https://www.nuget.org/packages/IO.Astrodynamics

Release 6.5.0 - Add Lambert solver

10 Jul 12:25
c9304a4

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What's Changed

Lambert solver :

  • Direct transfert
  • N revolutions transfert
  • Left and right branch solutions

Full Changelog: v6.4.0...v6.5.0

Release 6.4.0 - Compute time when a given radius or sphere of influence is reached

05 Jun 14:27
641ee24

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Compute time when a given radius or sphere of influence is reached
Download the latest version here: https://www.nuget.org/packages/IO.Astrodynamics