A 4.0kg quadcopter hovers in still air when its rotors supply an upward thrust force. Suddenly a steady wind exerts a 6.0N force toward the east. To give the quadcopter an acceleration of 1.5m/s2 upward and 0.50m/s2 toward the west, what thrust magnitude must the rotors now provide? (Assume the thrust can be directed vertically upward.)
a) 39N
b) 46N
c) 45N
d) 49N