Earth-to-Mars Interplanetary Pork Chop Plots

Version 1.4.0.0 (17,3 Mo) par David Eagle
A MATLAB Script for Creating Pork Chop Plots of Ballistic Earth-to-Mars Trajectories
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Mise à jour 16 jan. 2022

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PDF document and MATLAB script that can be used to create and plot interplanetary “pork chop” plots for Type I and Type II Earth-to-Mars trajectories. These plots illustrate the behavior of launch energy (C3L), right ascension (RLA) and declination (DLA) of the departure hyperbola, time-of-flight, and arrival v-infinity, DLA and RLA for a range of user-defined launch and arrival calendar dates.
The data required for these contour plots is created by solving the heliocentric, two-body “patched-conic” Lambert problem. A patched-conic trajectory ignores the gravitational effect of both the launch and arrivals planets on the heliocentric trajectory. Pork chop plots are typically used for preliminary mission analysis.

Citation pour cette source

David Eagle (2024). Earth-to-Mars Interplanetary Pork Chop Plots (https://www.mathworks.com/matlabcentral/fileexchange/39248-earth-to-mars-interplanetary-pork-chop-plots), MATLAB Central File Exchange. Récupéré le .

Compatibilité avec les versions de MATLAB
Créé avec R2019b
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Version Publié le Notes de version
1.4.0.0

Updated to use MICE routines and the DE421.bsp ephemeris
1.3.0.0

Added contour plot of total heliocentric delta-v. Updated PDF document.
1.2.0.0

Includes MICE version in porkchop_mice.zip archive.
1.1.0.0

Updated to use the DE421 binary ephemeris file from JPL. PDF document also updated.
1.0.0.0