Jsbsim Tutorial -

Maya hands Alex wind tunnel data: CL(alpha, camber) , CD(alpha) , Cm(alpha) .

<propulsion> <engine file="Rotax912"> <location> 0 0 0 </location> </engine> <propeller file="fixed_pitch"> <ixx> 0.2 </ixx> <diameter> 1.6 </diameter> <num_blades> 2 </num_blades> </propeller> </propulsion> He writes a taxi script: throttle 0.3, release brakes, wait 10 seconds, full rudder right. jsbsim tutorial

At 5 PM, Maya hands him a FlightGear configuration file that references x1.xml . “Now go see your aircraft fly for real.” Maya hands Alex wind tunnel data: CL(alpha, camber)

<flight_control name="FCS"> <channel name="pitch"> <pid name="elevator_pid"> <kp> 0.8 </kp> <ki> 0.05 </ki> <kd> 0.2 </kd> <input> aero/qbar-psf </input> <!-- dynamic pressure --> <output> fcs/elevator-cmd-norm </output> </pid> </channel> </flight_control> He runs a quick test using JSBSim’s command‑line tool: “Now go see your aircraft fly for real

“But how do I even fly it?” Alex asks.

<metrics unit="KG" unit_area="M2" unit_length="M"> <wingarea> 12.0 </wingarea> <wingspan> 10.0 </wingspan> <chord> 1.2 </chord> </metrics> All units are SI internally, but you can specify units per value. JSBSim converts. Part 3: The Aerodynamics Puzzle – Coefficient Tables Now the hardest part: the X‑1 has a variable‑camber wing (no flaps, but morphing trailing edge). No existing table works.