model an airplane with DATCOM software and code the transfer functions

Choose one airplane data and specifications from the appendixes of the uploaded book: “airplane flight dynamic and automatic flight control by Jan Roskam” and do the three parts of the following project: Part one: Model an airplane in “DATCOM software” and extract its aerodynamic Coefficients. I need a report including: 1. The airplane data and specifications. 2. How you entered the inputs and modeled the airplane by the software. 3. The diagram of the extracted coefficients. 4. A short analysis of the stability of the airplane considering the extracted Coefficients. Part two: Considering the extracted coefficients from the software, write the code of the airplane transfer functions. (you can find the functions in the book too) I need a report including: 1. How you coded the transfer functions considering the extracted coefficients and investigate the transfer functions answers to the aircraft inputs. Part three: Simulate the 6 degrees of freedom for the airplane. I need a report including: 1. How you did the simulation and draw the diagrams of the simulations.