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Added a description of the output files in the README
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README.md

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@@ -124,6 +124,22 @@ We suggest the user to run each simulation in a separate folder, that can be pla
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./orbit9.x
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**NOTE.** You may want to run the program in background for long-term integrations.
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### Output files
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The output files for the orbital integration of the asteroids are the same as the one provided by the
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original orbit9 code.
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In addition to the orbital integration, the modified orbit9 code provides the output files for the spin-axis
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dynamics when the flag *enable_out* is set to 1. The output files are called
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<astname>.yorp
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and it provides 4 columns, representing:
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1. the output time (in years)
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2. the rotation period (in hours)
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3. the obliquity (in degrees)
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4. the semi-major axis drift due to Yarkovsky (in au/My).
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### Run the test simulation
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The folder *tests/orbit9_yorp* contains the files to test a simulation that includes

tests/orbfit/epoch/410777.eq0

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

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