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Is there a high precision orbit propagator considering multiple perturbation forces in SatelliteToolBox.jl? The perturbation forces maight include non-spherical geopotential gravity, third body attraction, atmospheric drag, solar radiation pressure, earth albedo, ocean tides, empirical accelerations and general relativity. Or is there a high precision orbit propagator in other julia package?
The text was updated successfully, but these errors were encountered:
In the current state of SatelliteToolbox.jl there is not. We already have almost all the functionality to implement a HPOP, but we depend on the ODE solver in DifferentialEquations.jl. If I add this package as a dependency, then the load time of SatelliteToolbox.jl will be very slow. Thus, I need to break this package into smaller components so that the HPOP can be in an external package.
Yes, indeed this should be the next big thing in SatelliteToolbox. However, there is some pathway to travel. I need to split the package into smaller parts (maybe the time to do this has finally arrived :D, see #1). Then, create a package focusing only on numerical propagators. I think we have everything we need, we just need to glue the code.
Is there a high precision orbit propagator considering multiple perturbation forces in SatelliteToolBox.jl? The perturbation forces maight include non-spherical geopotential gravity, third body attraction, atmospheric drag, solar radiation pressure, earth albedo, ocean tides, empirical accelerations and general relativity. Or is there a high precision orbit propagator in other julia package?
The text was updated successfully, but these errors were encountered: