You are tracking the velocity and position of a rocket-propelled object near the surface of Mars. The velocity is v(t) and the position is s(t), where t is measured in seconds, s in meters, and v in m
You are tracking the quickness and posture of a rocket-propelled design nigh the demeanor of Mars. The quickness is v(t) and the posture is s(t), where t is measured in remedys, s in meters, and v in meters per remedy. It is notorious that the v(t) = ds/dt = 4.94 – 3.72t and s(0) = 5.
Explain why solving the rocket’s demolition in meters aggravate the duration interim from t = 1 to t = 3 is an application of the evaluation theorem.