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**Solution**
Determine a gravity model and using Vallado Equations, implement into the Gauss-Jackson propagator.
**Additional context**
One of many perturbations that need to be written to fully …
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First: I'm excited about the idea of a machine-speed SGP4 implementation that can be called from Python! This will meet an important need for folks finding the pure-Python `sgp4` not fast enough for t…
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Hi!
I have a satellite on-orbit which has a GPS unit built in. I have a list of ECEF positions and velocities. There are 20 of these data points, spaced out by 10 seconds each. Is there a good way …
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the SGP4 Skyfield libs are really cool. Also they have more realistic models.
but they seem a bit slow by a magnitude.
So adding a faster state vector processing would be great! :)
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Global navigation satellite system (GNSS), inertial measurement unit (IMU) and light detection and ranging (LiDAR), as common sensors in navigation systems, are widely used in fusion simultaneous loca…
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Hello!
I faced the issue with tags propagation in "Fixed Length Packet Tagger" block. I tried to push to flowgraph some additional info via tags (using PDU) and saw that this tags are mixed or missed…
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I see the error message in sharepoint project.
``` log
Dynamic operations can only be performed in homogenous AppDomain.
```
look into about this. it seems that causes by dynamic type.
So Can I c…
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# High level description
Nyx currently does not support the Two-Line Element Set (TLE) format and Simplified Perturbations Model (SGP4), both of which are commonly used in satellite tracking and co…
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Hello Eric!
I'm currently struggling to understand how to correctly propagate the orbit dynamics in 42 and I'd like your help in solving some doubts.
I'll report here the results for a 6U satellite…
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Dear people:
I want to run through a TLE file and calculate the coordinates of each satellite for a period of time (right now, datetime will only allow 60 seconds, but would like to run it longer).…