conversion.m

% conversion from full, empty to total
clc 
iMotor = 406;
settings.motor.expTime = motors(iMotor).t;
settings.motor.expThrust = motors(iMotor).T;
settings.motor.expM = motors(iMotor).m;
settings.mp = motors(iMotor).mp;                  % [kg]   Propellant Mass
settings.tb = motors(iMotor).t(end) ;             % [s]    Burning time
settings.mc = motors(iMotor).mc;
settings.mNoMot = 17.85;
settings.ms = settings.mNoMot + settings.mc;               % [kg]   Structural Mass
settings.m0 = settings.ms + settings.mp;          % [kg]   Total Mass
settings.mnc = 0;
settings.Lmot = motors(iMotor).L/1000;

mNoMot = settings.ms
mProp = settings.m0 - settings.mNoMot;

settings.xcg = [1.05, 0.98];   
xcgTot = 1.05;
xcgEmpty = 0.98;

settings.Lcenter = 2.270;
settings.boatL = 0.0;
LcenterNoMot = settings.Lcenter - settings.Lmot - settings.boatL

xcgProp = settings.Lmot/2;

% XcgNoMotor = (XcgTot*(MNoMot + Mfull) - mFull*XcgFull)/MNotMot
XcgNoMotor = (xcgTot*(mNoMot + mProp) - mProp*xcgProp)/mNoMot