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Added a description of the output files in the README
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Fenu24 committed Aug 8, 2022
1 parent 8867d68 commit b54d6c5
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16 changes: 16 additions & 0 deletions README.md
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Expand Up @@ -124,6 +124,22 @@ We suggest the user to run each simulation in a separate folder, that can be pla
./orbit9.x
**NOTE.** You may want to run the program in background for long-term integrations.


### Output files
The output files for the orbital integration of the asteroids are the same as the one provided by the
original orbit9 code.

In addition to the orbital integration, the modified orbit9 code provides the output files for the spin-axis
dynamics when the flag *enable_out* is set to 1. The output files are called

<astname>.yorp

and it provides 4 columns, representing:
1. the output time (in years)
2. the rotation period (in hours)
3. the obliquity (in degrees)
4. the semi-major axis drift due to Yarkovsky (in au/My).

### Run the test simulation
The folder *tests/orbit9_yorp* contains the files to test a simulation that includes
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40 changes: 20 additions & 20 deletions tests/orbfit/epoch/410777.eq0
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Expand Up @@ -4,23 +4,23 @@ refsys = ECLM J2000 ! default reference system
END_OF_HEADER
410777
! Equinoctial elements: a, e*sin(LP), e*cos(LP), tan(i/2)*sin(LN), tan(i/2)*cos(LN), mean long.
EQU 1.16258579991419E+00 -0.460780587309722 0.174893426578777 0.004546873094735 0.027005357832081 130.2149433096533
MJD 56146.360960617 TDT
MAG 22.134 0.150
! RMS 1.96473E-09 2.98895E-08 5.56570E-08 6.52480E-09 4.94639E-08 5.61450E-06
! EIG 2.84046E-10 3.77115E-09 1.37549E-08 2.39388E-08 4.96551E-08 1.13333E-07
! WEA 0.00193 -0.23555 0.45263 -0.00008 0.04021 0.85908
COV 3.860161481946468E-18 -1.446165963073374E-17 4.656822845390550E-17
COV 1.821664976970862E-18 -5.907075447992529E-18 3.682275993571308E-17
COV 8.933795320401931E-16 -1.305841352943879E-15 3.588417695120097E-17
COV -2.535854001407887E-16 -1.476485819588337E-13 3.097701994976310E-15
COV 5.346289388090830E-17 2.106754334362823E-17 2.736504315540130E-13
COV 4.257297281472898E-17 1.513509627075819E-16 -1.526753453281804E-15
COV 2.446682165292112E-15 2.326849867690401E-14 3.152255413752462E-11
NOR 1.226873664370155E+19 7.665131030671191E+17 -7.691614761816942E+17
NOR 1.253841081615465E+17 1.043852799048019E+16 1.025147626692871E+16
NOR 5.620974881710584E+16 -4.607629446026310E+16 -6.410417471291135E+15
NOR 2.188687554135583E+15 6.604524414262104E+14 5.060145487149013E+16
NOR -1.577644806577004E+16 1.374226967551625E+14 -6.550602190972885E+14
NOR 6.677124890538547E+16 -5.440786433786167E+15 1.140347934489098E+14
NOR 9.190707863578328E+14 8.104493058181679E+12 8.799427002223816E+12
EQU 1.16267296532696E+00 -0.460663787149893 0.174881277291140 0.004551542480933 0.027004980226847 25.7135001289037
MJD 56013.440131620 TDT
MAG 22.130 0.150
! RMS 2.04185E-09 3.16794E-08 6.08065E-08 6.78702E-09 5.56062E-08 6.08870E-06
! EIG 3.19829E-10 3.77761E-09 1.30692E-08 2.33856E-08 5.58635E-08 1.23626E-07
! WEA 0.00272 -0.23241 0.46139 0.00157 0.03830 0.85535
COV 4.169162701043839E-18 -1.575613095247293E-17 5.410558529866873E-17
COV 2.152240948132489E-18 -9.031385169561095E-18 8.884898855419340E-16
COV 1.003581986244237E-15 -1.541881189719501E-15 3.003470624508290E-17
COV -3.099241892348508E-16 -1.738565027899039E-13 3.697434392752590E-15
COV 6.490030078113178E-17 -7.073003849329925E-18 3.340752601130692E-13
COV 4.606360963780009E-17 1.905728985028579E-16 -4.279273760580620E-16
COV 3.092046688674574E-15 2.664964672746937E-14 3.707226110912469E-11
NOR 9.651481524731505E+18 6.768856270706134E+17 -6.796850344075229E+17
NOR 1.097599830124688E+17 9.610409045856248E+15 9.062369656042902E+15
NOR 5.617325196682769E+16 -4.601854955571240E+16 -6.412826238343329E+15
NOR 2.206948159407462E+15 6.602451178273214E+14 5.035122539431070E+16
NOR -1.574921120663447E+16 1.206500486267548E+14 -6.535286385660412E+14
NOR 6.651283311730663E+16 -5.439260899254842E+15 1.138966593927292E+14
NOR 8.360785526839552E+14 8.368481587875975E+12 8.790657650278620E+12

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