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I keep getting an error when attempting to query JPL horizons to get back only astromertic right ascension and declination. Here is the code I am using:
``` python
from astroquery.jplhorizons impo…
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### Expected Behaviour
The "Date and Time" column of the results for "Astronomical algorithms"->"Ephemeris" should show a regular progress according to the selected increment, from 10m up.
### Act…
wlaun updated
5 years ago
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Hi,
I would like to use code from the observation model packages, but without performing orbit determination / parameter estimation. For my application I only need the range observation/ relative d…
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Falscher unterschiedlicher Sprachcode bei verschiedenen Aufsätzen, die auf deutsch verfasst wurden
hier fre:
http://poj.peeters-leuven.be/content.php?url=article&id=3285206
hier eng:
http://poj.pe…
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In #4963, @StuartLittlefair implemented machinery to compute the location of the moon. This includes some standard algorithms for getting the location of an object given its standard orbital elements…
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Right now, the LS assumes that all of the ephemerides are equally spaced (with regards to time). The ephemerides we get off of ISIS cubes may or may not be equally spaced because of how ISIS reduces t…
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When trying to retrieve data for JPL, `measuresdata` requests the file download again and again endlessly:
```
oles@donar:/tmp/measuresdata$ ./measuresdata-update type=DE200
Calling measuresdata t…
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Hello,
I do not know if this can be considered appropriate here, in case not, feel free to close the issue.
I have tried to apply a parallelization scheme for the fitness computation using pagm…
Sceki updated
5 years ago
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Hi,
I want to analyse the stability of an asteroid over long periods of time. What I have noticed however, is that every time that I put the end epoch of the analysis past 1 Jan 2025, I get a messa…
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Hi Dominic,
I try to retrieve ephemeris data for long periods of time (20 years and longer) (to use it for accelerations during the propagation), and put it into bodysettings. I get the following e…