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Want to start off by saying thanks for providing such an amazing astrodynamics library and your great YouTube videos!
**Eclipse Duration Calculator**
Implement functionality to calculate the avera…
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For 2-body problems, the satellite orbits can be represented as [conic sections](https://en.wikipedia.org/wiki/Conic_section#Conic_parameters) (circle, ellipse, parabola, hyperbola).
A function shoul…
avanc updated
7 years ago
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CC: @giordano
* [x] Get validation setup in place
* [X] `ERFA.jl` Overhaul
* [x] Move `SPICE.jl` to `JuliaAstro` and complete wrapper
* [x] Migrate those to BinDeps2
* [x] Move `JP…
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_Converted from https://gitlab.com/nyx-space/nyx/-/issues/128 by ChatGPT_
# High level description
The purpose of this new feature is to enable users of the astrodynamics toolkit to take a set o…
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**Is your feature request related to a problem? Please describe.**
I found that with the existing frames there is a residual error when calculating the ra/dec position of known satellites based on TL…
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One year ago, working on question 1e of the Numerical Astrodynamics assignment 1, I reported the following issue in the course forum: when I used runge_kutta_fixed_step_size for different step sizes f…
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Is there a Lambert problem solver in SatelliteToolbox.jl? I used poliastro in Python and wondering whether there is such function in Julia?
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When the user fills out the TLE form, a point should be generated at the Cartesian location which astrodynamics dictates. The first set of coordinates generated (x1, y1, z1) represent the ECI (Earth …
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The second chapter of the project is focused on a deep review of the geometry, solutions and singularities of the Lambert's problem. Main references for this chapter are:
* Introduction to the theo…
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Hi! I'm writing a conference paper on [poliastro](https://github.com/poliastro/poliastro/), an open-source Python library for interactive Astrodynamics (WIP draft [here](https://github.com/scipy-confe…