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Ballistic Interplanetary Trajectory Design and Optimization

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Ballistic Interplanetary Trajectory Design and Optimization

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12 Dec 2012 (Updated )

A MATLAB Script for Ballistic Interplanetary Trajectory Design and Optimization

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Description

PDF document and a MATLAB script called ipto_matlab that can be used to design and optimize “patched conic” ballistic interplanetary trajectories between any two planets of our solar system. It can also be used to find two-body trajectories between a planet and an asteroid or comet. A patched-conic trajectory ignores the gravitational effect of both the launch and arrivals planets on the heliocentric transfer trajectory. This technique involves the solution of Lambert's problem relative to the Sun. Patched-conic trajectories are suitable for preliminary mission design. This script uses the SNOPT nonlinear programming (NLP) algorithm to solve this classic astrodynamics problem.
The ipto_matlab MATLAB script also performs a graphical primer vector analysis of the solution. This program feature displays the behavior of the primer vector magnitude and primer derivative magnitude as a function of mission elapsed time in days from departure.

MATLAB release MATLAB 8.0 (R2012b)
Other requirements Requires platform-specific version of SNOPT available at scicomp.ucsd.edu/~peg/ and the DE424 binary ephemeris file available at www.cdeagle.com. MICE version requires mex and binary ephemeris files available from NAIF.
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Updates
14 Dec 2012

Minor script changes (ecliptic-to-equatorial transformation, etc.) along with updates to PDF document.

21 Dec 2012

MICE version included in ipto_matlab_mice.zip archive.

28 Jan 2013

Updated version includes the option to enforce user-defined mission constraints during the trajectory optimization. PDF document updated to reflect this change.

09 Aug 2013

Added additional features to the heliocentric graphic display. Updated PDF document with additional script example.

07 Jul 2014

Added version of main script (ipto_matlab_64bit.m) that uses the March 17, 2014 version of SNOPT.

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