use bisection to solve this problem in matlab "applied numerical methods with matlab" prob.5-22.

The upward velocity of a rocket can be computed by the following formula: moot u=11 In mo-q where u upward velocity, u the velocity at which fuel is expelled relative to the rocket, mo- the initial mass of the rocket at time t 0, q the fuel consumption rate, and g -the downward acceleration of gravity (assumed constant 9.81 m/s). If u 1800 m/s, mo 160,000 kg, and q - 2600 kg/s, compute the time at which u- 750 m/s. (Hint: tis somewhere between 10 and 50 s) Determine your result so that it is within 1% of the true value. Check your