A hybrid VTOL fixed-wing drone comprising: a cabin; a left main wing and a right main wing coupled to the cabin; a left linear alignment of propellers having a first propeller, a second propeller, and a third propeller all of which are disposed on a top side of a left linear support; a right linear alignment of propellers having a fourth propeller, a fifth propeller, and a sixth propeller all of which are disposed on a top side of a right linear support; wherein the left linear support is parallel to the right linear support; a left forewing disposed on a front end of the left linear support; a right forewing disposed on a front end of the right linear support; characterized in that: the left forewing is directly connected to the right forewing; the left forewing and the right forewing are not directly connected to the cabin, the left main wing and the right main wing form a dihedral configuration, the left main wing and the right main wing each has a proximal portion disposed entirely within a space between the left and the right linear supports (220, 221), wherein the proximal portions of the left and the right main wings (213, 214) form the dihedral configuration such that a location where they connect to the left respectively right linear support is higher than where it connects to the cabin. a cabin; a left main wing and a right main wing coupled to the cabin; a left linear alignment of propellers having a first propeller, a second propeller, and a third propeller all of which are disposed on a top side of a left linear support; a right linear alignment of propellers having a fourth propeller, a fifth propeller, and a sixth propeller all of which are disposed on a top side of a right linear support; wherein the left linear support is parallel to the right linear support; a left forewing disposed on a front end of the left linear support; a right forewing disposed on a front end of the right linear support; characterized in that: the left forewing is directly connected to the right forewing; the left forewing and the right forewing are not directly connected to the cabin, the left main wing and the right main wing form a dihedral configuration, the left main wing and the right main wing each has a proximal portion disposed entirely within a space between the left and the right linear supports (220, 221), wherein the proximal portions of the left and the right main wings (213, 214) form the dihedral configuration such that a location where they connect to the left respectively right linear support is higher than where it connects to the cabin. the left forewing is directly connected to the right forewing; the left forewing and the right forewing are not directly connected to the cabin, the left main wing and the right main wing form a dihedral configuration, the left main wing and the right main wing each has a proximal portion disposed entirely within a space between the left and the right linear supports (220, 221), wherein the proximal portions of the left and the right main wings (213, 214) form the dihedral configuration such that a location where they connect to the left respectively right linear support is higher than where it connects to the cabin.