Yarkovsky effect
The Yarkovky effect is implemented according to [VokrouhlickyFarinella99] and [VokrouhlickyMilaniChesley00] and is available in the schemes (we recommend scheme 1):
Use YarkovskySolar Constant: Solar Constant at 1 AU in W / \(\text{m}^2\)Asteroid eps: Emissivity factorAsteroid rho: density of the body in kg/ \(\text{m}^3\)Asteroid C: Specific Heat Capacity in \(\text{J} \, \text{kg}^{-1} \text{K}^{-1}\)Asteroid A: Bond albedoAsteroid K: Thermal conductivity in \(\text{W} \, \text{m}^{-1} \text{K}^{-1}\)
Note that the calculation of the Yarkovsky effect uses the Asteroid rho value for the calculation of the thermal inertia
\(\Gamma\) and not the individual particle densities.
Set the call interval
With the parameter Yarkovky Inteval the calling interval of the Yarkovsky function can be set. This means that
the function is called fewer times, and in increased drift rate \(dx = a * dt * YarkovskyInterval\).
With the time averaged Yarkovsky function (mode 2) it is possible to use quite large interval numbers.
The direct Yarkovsky effect (mode 1) is more sensitive to values greater than \(\approx 100\).
Strictly speaking ,this argument violets the symplectic nature of the integrator, but as long as the Yarkovky force is small it is OK.
Test of the Yarkovsky effet
In Fig. 13 is shown a test of the Yarkovsky effect following [FarinellaVokrouhlickyHartmann98] and [BRB00].
Use Yarkovsky = 1 (2)
Asteroid emissivity eps = 1.0
Asteroid density rho = 3500.0
Asteroid specific heat capacity C = 680.0
Asteroid albedo A = 0.0
Asteroid thermal conductivity K = 2.65
Solar Constant = 1367
Semi-major axis a = 2 AU
Eccentricity = 0
Inclination = 0
Argument of perihelion = 0 - 2 \(\pi\)
Longitude of ascending node = 0 - 2 \(\pi\)
Mean anomaly = 0 - 2 \(\pi\)
Density \(\rho\) = 3500.0 kg/m^3
Physical radius R = 0.1 - 100 m
Rotation frequency \(\omega\) = 5 h
Obliquity \(\gamma_{\text{Seasonal}}\) = \(90^\circ\)
Obliquity \(\gamma_{\text{Diurnal}}\) = 0
Fig. 13 Drift rate of the seasonal and diurnal Yarkovsky effect. Computed after 10000 years and averaged over 1 orbit.