unable to use Aerospace Blockset function eci2ecef
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Eduardo Rodrigues Silva Filho
2020 年 3 月 27 日
Hi, I need to a function to transform acceleration data from ECI to ECEF frame and I found this function on Aerospace Blockset which does exactly what I need (https://www.mathworks.com/help/aeroblks/eci2ecef.html). However, I was unable to use it within a normal matlab script. I tried one of the example codes from the help center:
r_eci = [-2981784 5207055 3161595];
utc = [2019 1 4 12 0 0];
mjd = mjuliandate(utc);
pm = polarMotion(mjd, 'action', 'none')*180/pi;
r_ecef = eci2ecef(utc, r_eci, 'pm', pm)
And I got the following error:
Unrecognized function or variable 'eci2ecef'.
Is it possible to use this function outiside of Simulink in a normal script? Does anyone knows a good replacement for this function?
Thanks
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採用された回答
Divya Yerraguntla
2020 年 3 月 30 日
Hi Eduardo,
The "eci2ecef" is part of the set of function in CubeSats hence the function requires the 'Aerospace Blockset CubeSat Simulation Library' Add-on support package. You could download this from the Add-ons manager.
Hope it helps!
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その他の回答 (1 件)
Seth Wagenman
2020 年 9 月 3 日
Try importing Python's pymap3d package and using it instead as described at:
Unfortunately, you have to convert your MATLAB datetime objects to datenum and then do some math on them before passing over to Python, as described here:
The Python astropy package is the basis for the coordinate transformations and it works quite well. It is a bit slow and I recommend installing the MATLAB API for Python and using a custom Python function which returns MATLAB data objects instead of numpy arrays, which will then require extra conversion within MATLAB anyway before you can use them; see this answer for a work-around if you do not have administrative privileges:
Hope it works! I would love a comparison between what MATLAB spits out for Null Island's ECI coordinates on January 1, 2000 at noon UTC (using the leap seconds option) to compare. The python code returns (1158174.7900579234, -6272101.938428859, -143.09802467421062).
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