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!
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!