Configuration for vertical take-off and landing system for aerial vehicles

A vehicle, comprising:

• a main body having a fore portion, a tail portion, a starboard side, a port side and a cockpit formed therein to accommodate a human pilot;
• a first fluid generator coupled to the main body and producing a first fluid stream;
• at least one tail conduit fluidly coupled to the first generator,
• first and second fore ejectors coupled to the fore portion and respectively coupled to the starboard side and port side, the fore ejectors respectively comprising an outlet structure out of which fluid flows at a predetermined adjustable velocity;
• at least one tail ejector fluidly coupled to the at least one tail conduit and coupled to the tail portion, the at least one tail ejector comprising an outlet structure out of which fluid from the at least one tail conduit flows at a predetermined adjustable velocity;
• a primary airfoil element having a leading edge and a trailing edge;
• first and second control airfoils respectively coupled to the starboard and port sides and positioned between the fore portion and the primary airfoil element;
• and
• a third control airfoil coupled to the tail portion.