Gravity-assist Trajectory Design and Analysis - SNOPT
Cite As
David Eagle (2024). Gravity-assist Trajectory Design and Analysis - SNOPT (https://www.mathworks.com/matlabcentral/fileexchange/39462-gravity-assist-trajectory-design-and-analysis-snopt), MATLAB Central File Exchange. Retrieved .
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Version | Published | Release Notes | |
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2.1.0.0 | Updated source code and PDF documentation |
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2.0.0.0 | Script is now "data file driven". Added asteroid or comet as arrival body. Updated PDF document and added several new example missions. |
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1.6.0.0 | MATLAB source code updates (new keywords, etc.) |
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1.5.0.0 | Fixed bug in code that calculated the heliocentric orbital elements and state vector of the departure planet. (emu replaced with smu in the calling argument). |
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1.4.0.0 | UPDATED LINKS SNOPT ccom.ucsd.edu/~optimizers/ Binary Ephemeris Files https://www.dropbox.com/sh/hul0g7ia6nhspwo/AAATqfVXb5ClZODfGGvEbRZEa?dl=0 |
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1.3.0.0 | Bug fixes. Added three-dimensional graphics for the flyby trajectory. Updated PDF document. |
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1.2.0.0 | Added main script (flyby_matlab_64bit.m) that uses the March 17, 2014 version of SNOPT. |
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1.1.0.0 | MICE version included in flyby_mice.zip archive. |
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1.0.0.0 |