I'm doing a project regarding orbital launches and i'm kinda confused about how to calculate orbital inclination from launch sites. I've simplified my model so I can ignore fuel and the rocket equation as I'm only interested in delta-v.
I'm a bit confused on how to account for earth rotational speed at different Latitudes for the orbital inclination with the lowest delta-v requirements. I know that the orbit with the lowest delta-v will have an orbital incliation the same as the latitudes of launch but am unsure how to prove it ?
I am aware that I'm going to have to use spherical trigonomet