So I'm actually a student studying this sorta thing, and an assignment I have is to chase/rendezvous with an asteroid. I've done my reading on the C-W equations (what little I could understand) and from what I can gather, these are general equations who care not for what they are being used to chase.
Essentially my question is, am I correct in thinking that they can be used to calculate motion/delta V to close the distance on an asteroid, just as well as the ISS/any other Space Station?