Applied-Orbital-master

Applied-Orbital-master\.DS_Store

Applied-Orbital-master\HW10

Applied-Orbital-master\HW10\.DS_Store

Applied-Orbital-master\HW10\HW10Script.m

Applied-Orbital-master\HW10\HW10Script.m~

Applied-Orbital-master\HW10\L4.jpg

Applied-Orbital-master\HW10\Transfer.jpg

Applied-Orbital-master\HW10\integrateThreeBodyEquation.m

Applied-Orbital-master\HW10\integrateThreeBodyEquation.m~

Applied-Orbital-master\HW11

Applied-Orbital-master\HW11\Homework11Script.m

Applied-Orbital-master\HW11\Homework11Script.m~

Applied-Orbital-master\HW11\RightAscnFrameToECI.m

Applied-Orbital-master\HW11\eph.m

Applied-Orbital-master\HW11\eph.m~

Applied-Orbital-master\HW11\integrateFourBodyEquation.m

Applied-Orbital-master\HW11\integrateFourBodyEquation.m~

Applied-Orbital-master\HW11\integrateTwoBodyEquation.m

Applied-Orbital-master\HW11\integrateTwoBodyEquation.m~

Applied-Orbital-master\HW11\keplerSolver.m

Applied-Orbital-master\HW11\lambertTransfer.m

Applied-Orbital-master\HW11\lambertTransfer.m~

Applied-Orbital-master\HW11\orbitalElementsToStateVectors.m

Applied-Orbital-master\HW12

Applied-Orbital-master\HW12\.DS_Store

Applied-Orbital-master\HW12\Assignment 12.docx

Applied-Orbital-master\HW12\EclipsedSat.m

Applied-Orbital-master\HW12\EclipsedSat.m~

Applied-Orbital-master\HW12\RightAscnFrameToECI.m

Applied-Orbital-master\HW4

Applied-Orbital-master\HW4\EclipsedSat.m

Applied-Orbital-master\HW4\EclipsedSat.m~

Applied-Orbital-master\HW4\Results updated.rtf

Applied-Orbital-master\HW4\Results.docx

Applied-Orbital-master\HW4\RightAscnFrameToECEF.m

Applied-Orbital-master\HW5

Applied-Orbital-master\HW5\ground_track.asv

Applied-Orbital-master\HW5\ground_track.m

Applied-Orbital-master\HW5\kepler_E.m

Applied-Orbital-master\HW5\ra_and_dec_from_r.m

Applied-Orbital-master\HW5\sv_from_coe.m

Applied-Orbital-master\HW6

Applied-Orbital-master\HW6\Homework 6.docx

Applied-Orbital-master\HW6\Homework6Script.m

Applied-Orbital-master\HW6\Homework6Script.m~

Applied-Orbital-master\HW6\RightAscnFrameToECEF.m

Applied-Orbital-master\HW6\RightAscnFrameToECEF.m~

Applied-Orbital-master\HW6\keplerSolver.m

Applied-Orbital-master\HW6\keplerSolver.m~

Applied-Orbital-master\HW6\orbitalElementsToStateVectors.m

Applied-Orbital-master\HW6\relativePositionVectorsToRTN.m

Applied-Orbital-master\HW7

Applied-Orbital-master\HW7\.DS_Store

Applied-Orbital-master\HW7\ECIToECEF.m

Applied-Orbital-master\HW7\GroundTrack.tif

Applied-Orbital-master\HW7\Homework 7.docx

Applied-Orbital-master\HW7\Homework7Script.m

Applied-Orbital-master\HW7\Homework7Script.m~

Applied-Orbital-master\HW7\RAandDecOverTime.tif

Applied-Orbital-master\HW7\RightAscnFrameToECEF.m

Applied-Orbital-master\HW7\RvsTime.tif

Applied-Orbital-master\HW7\integrateTwoBodyEquation.m

Applied-Orbital-master\HW7\integrateTwoBodyEquation.m~

Applied-Orbital-master\HW7\keplerSolver.m

Applied-Orbital-master\HW7\positionVecToRAandDec.m

Applied-Orbital-master\HW7\semimajorAxisForRepeatingGroundtrack.m

Applied-Orbital-master\HW8

Applied-Orbital-master\HW8\HW8.m

Applied-Orbital-master\HW8\Homework8Script.m

Applied-Orbital-master\HW8\Homework8Script.m~

Applied-Orbital-master\HW8\RightAscnFrameToECEF.m

Applied-Orbital-master\HW8\convertUTCAndDOYToSiderealTimeInDegreesAtGreenwich.m

Applied-Orbital-master\HW8\elevationAndAzimuthToRAandDec.m

Applied-Orbital-master\HW8\elevationAndAzimuthToRAandDec.m~

Applied-Orbital-master\HW8\keplerSolver.m

Applied-Orbital-master\HW8\stateVectorToPerifocalFrame.m

Applied-Orbital-master\HW9

Applied-Orbital-master\HW9\Problem3.asv

Applied-Orbital-master\HW9\Problem3.m

Applied-Orbital-master\HW9\Problem3b.asv

Applied-Orbital-master\HW9\Problem3b.m

Applied-Orbital-master\HW9\fDot_and_gDot.m

Applied-Orbital-master\HW9\f_and_g.m

Applied-Orbital-master\HW9\kepler_U.m

Applied-Orbital-master\HW9\rkf45.m

Applied-Orbital-master\HW9\rv_from_r0v0.m

Applied-Orbital-master\HW9\stumpC.m

Applied-Orbital-master\HW9\stumpS.m

Applied-Orbital-master\HW9\sv_from_coe.m

Applied-Orbital-master\Orbital-Mechanics

Applied-Orbital-master\README.md