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Implementation of regularized propagators: stabilized Cowell and Dromo(P).
Branch: https://github.com/MiguelAvillez/tudat/tree/feature/regularized_propagators
Relevant literature:
- "REGULARISE…
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_Original description:_ https://blueprints.launchpad.net/stellarium/+spec/improved-planet-rendering
The current rendering is very basic: planets are ellipsoids mapped with a rectangular texture, li…
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### Environment
- OS: Server running on a dedicated Windows 7 machine.
- Mono:
### Description
If players leave the server and then return, there are stacks of flights on the launch pad, flight…
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Hi,
I am trying to use GNSS-SDRLIB as GNSS transmitter and RTKNAVI as GNSS receiver. Data from GNSS-SDRLIB are sent to TCP Server and I am trying to read it with RTKNAVI. RTKNAVI connects to TCP Se…
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Here is a list of events that can be explored as part of the tutorials to be presented at SciPy. The idea is to have 6 events in all to present on - 3 in each category. The events have to have occurre…
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Simulating a 500km SSO satellite, I would expect the various subsystem telemetry to vary with the solar illumination/eclipse.
Instead, I have noticed that:
- All 3 temperature endpoints have const…
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FEDS needs a monitoring system for when the data and github actions go down.
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Hello
How can i draw satellite orbit from this orbital element(TLE) ?
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**Describe the bug**
hello professor,
when I use the read_SLC_int function of the PRM.py, it report the error, here is the error ` File "c:\Users\kjzha\.conda\envs\pygmt\Lib\runpy.py", line 198, in …
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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 …