Doin Time,
No one said anything about being smarter than the system. The typical reason VDPs are actually published on approaches is for obstacle clearance reasons, and when published, are mandatory.
What we're talking about on this thread is calculating a point from which a stabilized, 3-degree glidepath to the runway can be made when transitioning from the MDA to the visual portion of a non-precision approach. You mentioned if you can't see the vasi or papi and don't have the depth perception to make a normal approach, you should think twice about leaving MDA. If I were at or past what I had calculated as the VDP, and the conditions you describe exist, I wouldn't at all think twice about leaving MDA. I would leave MDA and execute the missed approach procedure. This is a far better option than continuing along at the MDA for some distance past my calculated VDP, then attempting a de-stabilized, excessive rate of descent dive for the runway.
A botched VDP calculation or not having a good way of measuring it is simply poor planning. With very few exceptions, any non-precision approach will have a final approach fix and a missed approach point, and a method for calculating either by time or distance.
The FAA is advocating, and many companies are adopting, the "constant path angle" method of flying non-precision approaches, instead of the old "dive and drive" method, as a way to reduce exposure to CFIT risks. With this constant path angle type of non-precision approach, you descend from the FAF at a constant 3-degree (or whatever is published on the plate, if different) glide path, either by calculating what descent rate will give you the desired glidepath, or by dialing in the desired flight path angle in the autoflight system on aircraft that are so equipped, such as the A-320 or B-717, for example. You then treat the MDA as a "psudo" decision altitude, where you either have the required visual references to continue the approach in your already stabilized configuration, or if not, execute the missed approach. This method insures the aircraft is configured and stablized, and remains so throughout the final approach segment. It also makes the calculations of VDPs unnecessary. The MDA becomes the VDP.
Obviously, this applies only to straight in approaches, and not for circling maneuvers.