During the test flight of a UDF powered aircraft, the pilot has set the engine thrust level at 40,000N, which causes the 20,000 kg aircraft to attain a cruise speed of 180 m/s. The engine throttles are then set to a power level of 60,000N, and the aircraft begins to accelerate. As the speed of the plane increases, the aerodynamic drag increases in proportion to the square of the air speed. Eventually, the aircraft reaches a new cruise speed, where the thrust of the UDF engines is just offset by the drag. The equations used to estimate the velocity and acceleration of the aircraft from the time the throttle is rest to the time the plane reaches new cruise speed (at approximately 120 s) are the following: velocity = 0.00001 time -0.00488 time^3 + 0.75795 time + 181.3566
acceleration = 3 - 0.000062 velocity?

Write a MATLAB program, using a script M-file, that calculates the velocity and acceleration of the aircraft at times from 0 to 120 seconds, and at increments of 10 seconds.