The links and wishbones are the easiest to DIY fab, welded steel tubes with appropriate joints on the ends.
The Vertical Links, especially for driven wheels, are the most difficult to DIY, castings, forgings, or weldments, and difficult to design parts that are strong, light, and robust, so take advantage of the OEM investment in R&D and re-purpose something.
Select the VL that meet your needs, by strength, weight, # of lugs and PCD, wheel sizes available.
Lay out the suspension geometry based on the VL joints, which gives you the chassis mounting points, and then design the chassis
to handle the loads and stiffness requirements (find a copy of 'Racing and Sports Car Chassis Design' by Costin and Phipps).
Welded steel space frames are the most practical for DIY, both in design and fabrication. Triangulation and mechanical engineering knowledge to calculate the stresses in each tube member of the truss, selection of the tubes size and wall thickness, and design of the welded joints. Helps to have metalworking and welding skills.
But monocoque and similar stressed skin structures are possible (find a copy of 'Aircraft Structures' by David Peery). The skin stresses of a torque box are somewhat simple; t=2qA where t= max torque stress, q = skin shear strength, A= enclosed box area. But the devil lies in the details of skin reinforcement to prevent buckling, corner and seam joints, torque box intersections, and fastener placement and fabrication. Helps to have some airframe construction/maintenance experience, and sheet metal tools & skills.
Composite chassis, carbon fiber/fiberglass is a different ballgame, both design and fabrication. There is plenty of knowledge out there now that you can take advantage of. Burt Rutan offers a lot of practical advice for kit plane constructors that can be used by anyone building a composite structure.
So good luck, and have fun.
Carter