A radio-controlled model airplane has a momentum given by [(β0.75ππ β π π 3 β )π‘ 2 + (3.0ππ β πβπ )]πΜ+ (0.25ππ β π π 2 β )π‘πΜ. What are the π₯-, π¦-, and π§-components of the net force on the airplane?
"\\vec p=(-0.75t^2+3)\\cdot\\vec i+0.25t\\cdot\\vec j"
"\\vec F=d\\vec p\/dt=-1.5t\\cdot \\vec i+0.25\\cdot\\vec j"
"F_x=-1.5t" , "F_y=0.25" , "F_z=0"
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