VTOL having retractable wings

A vertical take-off and landing aircraft including:

• a fuselage;
• a flight computer;
• a control system;
• at least one pair of retractable wings being retractable and extendable sideways with axes of rotation of the retractable wings being substantially vertical;
• an absolute angle between said axes or rotation and a yaw axis of the aircraft being limited to 5 degrees;
• the retraction and extension of the retractable wings performed while the aircraft is hovering;
• at least one actuator to extend and retract the retractable wings, with said retractable wings being supported by at least one hinge and said hinge being supported by the fuselage;
• the at least one pair of wings having at least one trailing edge mounted control surface (TEMCS);
• and
• at least one engine being supported by said TEMCS;
• wherein said engine being tilt-able together with said TEMCS thus creating vectored forces;
• said TEMCS having rotational range of motion of at least 80 degrees in order to tilt the said at least one engine fully upward to a substantially vertical position in order to create vertical lift for a hover mode and tilt the said at least one engine forward to a substantially horizontal position in order to create thrust for a cruise mode and having bidirectional range of motion of at least 1 degree in both substantially horizontal and substantially vertical positions in order to create controlled vectored forces in both positions.