Aircraft and method of use

An aircraft comprising:

• a fuselage having an interior cockpit configured to hold one or more seats, the fuselage is configured to remain in an upright position relative to the ground surface during flight;
• a counterweight platform secured within the interior cockpit, the counterweight platform having:
• a first support and a second support, the first support extending perpendicular to the second support;
• a plurality of batteries secured to the first support;
• one or more motors associated with one or more worm drives, the one or more motors and the one or more worm drives are configured to move the plurality of batteries along the first support and the second support;
• a canopy pivotally attached to the fuselage and configured to provide access to the interior cockpit;
• a plurality of wings extending away from the fuselage, each of the plurality of wings having:
• a motor positioned at a first end;
• the plurality of wings being four wings, the four wings extending away from the fuselage in an X configuration;
• a tilting bar extending through the fuselage and engaging with a pivot point associated with each of the plurality of wings, the tilting bar allowing for the fuselage to rotate about the pivot joint and thereby stay in an upright position, regardless of the positioning of each of the plurality of wings;
• one or more landing legs positioned aside the fuselage and configured to support the fuselage during landing, the one or more landing legs are secured to the plurality of wings;
• and
• a computing device configured to control each motor, wherein each motor can be controlled independently;
• wherein the cockpit is sized to hold one or more people;
• wherein the motor of each of the plurality of wings provides lifting force;
• wherein the fuselage remains in the upright position as the plurality of wings rotate relative to the fuselage;
• and
• wherein the plurality of wings do not obstruct access to the interior cockpit when the plurality of wings rotate relative to the fuselage.