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"REGULARISED METHODS FOR HIGH-EFFICIENCY PROPAGATION", Geul et al. (2016)
"DROMO propagator revisited", Urrutxua et al. (2016)
"ACCURATE COMPUTATION OF HIGHLY ECCENTRIC SATELLITE ORBITS", Janin (1974)
"Regularization in Orbital Mechanics", Roa (2016)
Stabilized cowell implemented according to Janin (1974). Dromo(P) implemented according to Urrutxua et al. (2016); same propagator used by Geul et al. (2016).
Current overall status:
Setup of propagation using independent variable other than time implemented, though not really working. See stabilized cowell.
Stabilized cowell:
Implemented, but not working, even without perturbations. No idea why.
Implementation of the term dU/dr of the EOM is wrong (which doesn't explain why it isn't working without perturbations)
Dromo(P):
Unit conversions and EOM implemented
Conversion from Cartesian to Dromo(P) unit tested
Conversion from Keplerian to Dromo(P) unit tested
Conversion from Dromo(P) to Cartesian partially tested: Parabolic case (case 3) not finished. Recheck remaining cases.
Conversion from Dromo(P) to Keplerian not yet tested
The text was updated successfully, but these errors were encountered:
Thanks for posting this! It looks like it's already pretty well advanced. The next time I have a couple of hours to spend on debugging something, I'll see if I can look into the stabilized Cowell
Implementation of regularized propagators: stabilized Cowell and Dromo(P).
Branch: https://github.com/MiguelAvillez/tudat/tree/feature/regularized_propagators
Relevant literature:
Stabilized cowell implemented according to Janin (1974). Dromo(P) implemented according to Urrutxua et al. (2016); same propagator used by Geul et al. (2016).
Current overall status:
Stabilized cowell:
Dromo(P):
The text was updated successfully, but these errors were encountered: