Understanding the Effects of Spacecraft Trajectories through Solar Coronal Mass Ejection Flux Ropes Using 3DCOREweb
This study investigates the impact of spacecraft positioning and trajectory on in situ signatures of coronal mass ejections (CMEs).Employing the 3DCORE model, a 3D flux rope model that can generate in situ profiles for any given point in space and time, we conduct forward adifom q red modeling to analyze such signatures for various latitudinal and