A fixed-wing drone comprising: a main body ; a left main wing and a right main wing ; a left forewing and a right forewing , which are shorter than the left main wing and the right main wing ; a left linear support , which physically connects.the left forewing to the left main wing and which is fixed near a left terminal end of the left forewing ; a rear terminal end of the left linear support extends rearward beyond a rear edge of the left main wing ; a right linear support , which physically connects the right forewing to the right main wing and which is fixed near a right terminal end of the right forewing ; a rear terminal end of the right linear support extends rearward beyond a rear edge of the right main wing ; a left linear alignment of propellers having a first propeller , a second propeller , and a third propeller ; a right linear alignment of propellers having a fourth propeller , a fifth propeller , and a sixth propeller ; wherein the left linear alignment is parallel to the right linear alignment, the first propeller , the second propeller , and the third propeller are directly disposed linearly in a straight line on the left linear support , wherein the straight line is parallel to a longitudinal axis of the main body , the first propeller is disposed at the front terminal end of the left linear support , the third propeller is disposed at the rear terminal end of the left linear support , the fourth propeller is disposed at the front terminal end of the right linear support , and the sixth propeller is disposed at the rear terminal end of the right linear support , characterized in that , the left linear support is fixed at a front terminal end near the left terminal end of the left forewing , the right linear support is fixed at a front terminal end near the right terminal end of the right forewing , and the first propeller and the second propeller are disposed on opposing sides of the left linear support . a main body ; a left main wing and a right main wing ; a left forewing and a right forewing , which are shorter than the left main wing and the right main wing ; a left linear support , which physically connects.the left forewing to the left main wing and which is fixed near a left terminal end of the left forewing ; a rear terminal end of the left linear support extends rearward beyond a rear edge of the left main wing ; a right linear support , which physically connects the right forewing to the right main wing and which is fixed near a right terminal end of the right forewing ; a rear terminal end of the right linear support extends rearward beyond a rear edge of the right main wing ; a left linear alignment of propellers having a first propeller , a second propeller , and a third propeller ; a right linear alignment of propellers having a fourth propeller , a fifth propeller , and a sixth propeller ; wherein the left linear alignment is parallel to the right linear alignment, the first propeller , the second propeller , and the third propeller are directly disposed linearly in a straight line on the left linear support , wherein the straight line is parallel to a longitudinal axis of the main body , the first propeller is disposed at the front terminal end of the left linear support , the third propeller is disposed at the rear terminal end of the left linear support , the fourth propeller is disposed at the front terminal end of the right linear support , and the sixth propeller is disposed at the rear terminal end of the right linear support , characterized in that , the left linear support is fixed at a front terminal end near the left terminal end of the left forewing , the right linear support is fixed at a front terminal end near the right terminal end of the right forewing , and the first propeller and the second propeller are disposed on opposing sides of the left linear support . <EOS>