Homework Help

Engineering
Mechanical Engineering
consider an airplane in constantaltitude straightline flight the velocity equation...

Question: consider an airplane in constantaltitude straightline flight the velocity equation...

Question details

Consider an airplane in constant-altitude, straight-line flight. The velocity equation is where the second term represents aerodynamic drag, and assume k= constant, and Tis the engine thrust acceleration. Treat T as the control (input Let V be a given constant cruise speed. Obtain the linearized differential equation for the velocity around V

Solution by an expert tutor

Blurred Solution

This question has been solved

Subscribe to see this solution