KRC for Exoplanets

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Where  
 
Where  
  
:e: Eccentricity
+
:e: Eccentricity (Default=0)
  
:a: Text
+
:a: Semi-Major Axis in AU (Default=1)
  
:i: text
+
:i: Inclination of mean orbit to ecliptic in degrees  (Default=0)
  
:node: text
+
:node: Longitude of the asceding node in degrees (Default=0)
  
:per:i text
+
:per: Argument of perihelion in degrees (Default=0)
  
:m: text
+
:m: Mean Anomaly at epoch in degrees (Default=0)
  
:rot_per: text
+
:rot_per: siderial rotation period in hours (Default=23.9345)
  
:polera: text
+
:polera: Right Ascension of the pole in degrees (Default=0)
  
:merid: text
+
:merid: Prime meridian at epoch in degrees (Default=0)
  
:poledec: text
+
:poledec: Declination of the pole in degrees (Default=0)
  
:period: text
+
:period: Sideral orbital period in Earth days (Default=365.256)
  
:name: text
+
:name: Body name (default ="None")
  
  
 +
 +
 +
printf("\nGenerate a generic PORB structure for use with the davinci porb function\n")
 +
printf("This is formatted in the minor body style for porb and permits the following values described below\n\n")
 +
printf("\tname = body name (Default=\"None\"\n")
 +
printf("\tepoch = epoch in Julian Date (Default = 2451545.0, year 2000)\n")
 +
printf("\ta = Semi-Major Axis in AU (Default=1)\n")
 +
printf("\te = Eccentricity (Default=0)\n")
 +
printf("\ti = Inclination of mean orbit to ecliptic in degrees  (Default=0)\n")
 +
printf("\tnode = Longitude of the asceding node in degrees (Default=0)\n")
 +
printf("\tperi = Argument of perihelion in degrees (Default=0)\n")
 +
printf("\tm = Mean Anomoly at epoch in degrees (Default=0)\n")
 +
printf("\tpolera = Right Ascention of the pole in degrees (Default=0)\n")
 +
printf("\tpoledec = Declination of the pole in degrees (Default=0)\n")
 +
printf("\tmerid = prime meridian at epoch in degrees (Default=0\n")
 +
printf("\trot_per = siderial rotation period in hours (Default=23.9345)\n")
 +
printf("\tperiod = siderial orbital period in days (Default=365.256)\n")
  
  

Revision as of 20:33, 15 January 2019

A user can define the orbital parameters of any body rotating around any star. PORB generates the rotation matrix accordingly.

Solar System-like

First, run porb to define the orbital parameters of the body in a structure:

tmp=generic_porb(e=0, a=1.,i=1.30439695, node=100.47390909, peri=293.923, m=79.668,rot_per=200., polera=273.85,poledec=poledec, merid=7.7, period=4332.589, name="IdealJupiterTrojan")

Where

e: Eccentricity (Default=0)
a: Semi-Major Axis in AU (Default=1)
i: Inclination of mean orbit to ecliptic in degrees (Default=0)
node: Longitude of the asceding node in degrees (Default=0)
per: Argument of perihelion in degrees (Default=0)
m: Mean Anomaly at epoch in degrees (Default=0)
rot_per: siderial rotation period in hours (Default=23.9345)
polera: Right Ascension of the pole in degrees (Default=0)
merid: Prime meridian at epoch in degrees (Default=0)
poledec: Declination of the pole in degrees (Default=0)
period: Sideral orbital period in Earth days (Default=365.256)
name: Body name (default ="None")



printf("\nGenerate a generic PORB structure for use with the davinci porb function\n") printf("This is formatted in the minor body style for porb and permits the following values described below\n\n") printf("\tname = body name (Default=\"None\"\n") printf("\tepoch = epoch in Julian Date (Default = 2451545.0, year 2000)\n") printf("\ta = Semi-Major Axis in AU (Default=1)\n") printf("\te = Eccentricity (Default=0)\n") printf("\ti = Inclination of mean orbit to ecliptic in degrees (Default=0)\n") printf("\tnode = Longitude of the asceding node in degrees (Default=0)\n") printf("\tperi = Argument of perihelion in degrees (Default=0)\n") printf("\tm = Mean Anomoly at epoch in degrees (Default=0)\n") printf("\tpolera = Right Ascention of the pole in degrees (Default=0)\n") printf("\tpoledec = Declination of the pole in degrees (Default=0)\n") printf("\tmerid = prime meridian at epoch in degrees (Default=0\n") printf("\trot_per = siderial rotation period in hours (Default=23.9345)\n") printf("\tperiod = siderial orbital period in days (Default=365.256)\n")



poledec=0; tmp=generic_porb(e=0, a=1.,i=1.30439695, node=100.47390909, peri=293.923, m=79.668,rot_per=200., polera=273.85,poledec=poledec, merid=7.7, period=4332.589, name="IdealJupiterTrojan")
out=krc(lat=0.,lon=0,INERTIA=20.,ALBEDO=.05,LKofT="F",body=tmp,bodytype="minor")          #

PLOTS AND EXPLANATION NEEDED HERE

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