rtakatori49 / Application-of-Extended-Kalman-Filter-to-Orbit-Determiation

Applying extended Kalman filter to initial orbit determination.
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SEZ to ECI #1

Open MMM-L opened 1 year ago

MMM-L commented 1 year ago

Hi, I have a problem with"SEZ to ECI" in your om.m file. why is it not followed? Csez2eci = Cz(-deg2rad(theta))*Cy(-((pi/2)-deg2rad(lla(1)))); % SEZ to ECI it like shown in "Fundamentals of Astrodynamics and Applications": $$ \vec{r}{IJK}=ROT3(-\theta{LST})ROT2(-{90-\Phi{gd}})\vec{r}{SEZ} $$ Excepting your reply! Best wishes!

MMM-L commented 1 year ago

Hi, can you help me?