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Hello team, you are GIANTS! 🚀🚀
Astrodynamics is not for everyone, thank you for opening the heavens for us.
Just finished a [**3D demo**](https://rpubs.com/echarty/satellites) using **asteRisk**.
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I found a breaking change in how `propagate!` and `propagate_to_epoch!` are used in v0.9.0 and wanted to make sure it was brought up!
The old usage was (pull from the docs):
```
o,r,v = propagate…
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Example usage for init_orbit_propagator not working for julia 1.4 (does work in 1.2):
```
julia> tle_scd1 = tle"""
SCD 1
1 22490U 93009B 18350.91204528 .00000219 00000-0 10201-…
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Thanks for the great job on the SatelliteToolbox, it is really useful for my work!
I was wondering if it has been already considered the possibility of using Geodesy.jl to generalize the ECEFLLA coor…
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**Describe the bug**
The orbital propagators have a frequency keyword specified in the load routines. However, this keyword does not pass through the system as expected.
**To Reproduce**
```
im…
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While training a tagging model using the provided Keyphrase dataset SEMEVAL2017, following error comes up:
Tokenization MISMATCH in sentence '...'
Last matched: 'Token: 272 Ì„'
Last sentence: 'Tok…
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**Is your feature request related to a problem? Please describe.**
From a coding perspective, the orbit propagators here and the test instruments in `pysat` share a number of similarities, such as th…
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We have a maven_install rule with 3.5k artifacts in it (this was autogenerated based on effective poms from a multimodule project - I'm in parallel working to understand how to reduce this list). When…
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(Not to be confused with #285)
It's already well known that some of our propagators have issues (see for example #475). Tricky stuff includes:
* Near parabolic orbits
* Very long propagation ti…
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Hi Dominic,
As I have already told you, I am currently working on implementing a GNC system for aerobraking in Tudat. I have two main questions right now:
- For the control system, I would need…