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updated 16 days ago

Optimal Finite-burn Interplanetary Injection from Earth Orbit by David Eagle

A MATLAB script for optimizing finite-burn interplanetary injection trajectories. (aerospace, mathematics, simulation)

[fid, ic_type, itarget, read_fname, write_fname, nsegment...

asympt (cbmu, rsc, vsc)

atan3 (a, b)

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updated 16 days ago

Two-dimensional, Low-thrust Earth-to-Mars Trajectory Analysis with MATLAB by David Eagle

Determines optimal, two-dimensional low-thrust Earth-to-Mars interplanetary trajectories. (aerospace, interplanetary missio...)

[fid, iopt, nsegments, mass0, thrmag, xisp, time_g, time_...

departure(jd_guess, transfer_time, transfer_angle)

gdate (jdate)

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updated 16 days ago

Solar Sail Trajectory Analysis with MATLAB by David Eagle

Two-dimensional trajectory analysis of solar sail Earth-to-Venus and Earth-to-Mars missions. (aerospace, mathematics, simulation)

[fid, nsegments, achar, b1, b2, b3, iplanet, time_g, time...

rkf78 (deq, neq, ti, tf, h, tetol, x)

ss2d_eqm_opt (t, y)

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updated 18 days ago

Gravity-assist Trajectory Design and Analysis by David Eagle

A MATLAB Script for Interplanetary Gravity-Assist Trajectory Design and Optimization (aerospace, mathematics, simulation)

atan3 (a, b)

bplane(r, v)

eci2orb1 (mu, r, v)

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updated 18 days ago

Ballistic Interplanetary Trajectory Design and Optimization by David Eagle

A MATLAB Script for Ballistic Interplanetary Trajectory Design and Optimization (aerospace, mathematics, simulation)

atan3 (a, b)

becl2000(ntarg, jdate)

eci2orb1 (mu, r, v)

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updated 7 months ago

Impulsive Hyperbolic Injection from a Circular Earth Park Orbit by David Eagle

Delta-v required for impulsive hyperbolic orbit transfer (aerospace, optimization, interplanetary missio...)

atan3 (a, b)

eci2orb1 (mu, r, v)

oeprint1(mu, oev, ittype)

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updated 12 months ago

Interplanetary Pork Chop Plots by David Eagle

A MATLAB Script for Creating Pork Chop Plots of Ballistic Earth-to-Mars Trajectories (aerospace, mathematics, simulation)

atan3 (a, b)

gdate (jdate)

getdate

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updated 1 year ago

A MATLAB Script for Propagating Interplanetary Trajectories from Earth to Mars by David Eagle

Numerically integrate the orbital equations of motion of an Earth to Mars interplanetary trajectory. (aerospace, mathematics, interplanetary missio...)

atan3 (a, b)

display1(jdtdb, cbmu, r, v)

eci2orb1 (mu, r, v)

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