Jsbsim Tutorial (2026)
After three hours of tweaking coefficients and re‑running simulations, the X‑1 flies straight and level at 80 knots.
<aerodynamics> <axis name="LIFT"> <coefficient name="CL"> <function> <table> <independentVar lookup="row">aero/alpha-rad</independentVar> <independentVar lookup="column">fcs/camber-command</independentVar> <!-- data from wind tunnel: rows alpha (-0.2 to 0.4 rad), cols camber (0 to 0.05) --> <tableData> -0.2 -0.4 -0.35 ... 0.0 0.2 0.25 ... 0.4 1.2 1.3 ... </tableData> </table> </function> </coefficient> </axis> </aerodynamics> He does the same for drag and pitch moment. For sideforce, yaw, roll, he uses simpler stability derivatives. jsbsim tutorial
<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. After three hours of tweaking coefficients and re‑running
The X‑1 lifts off at 45 knots, climbs, then slowly rolls left due to an asymmetric thrust he forgot to model. Alex corrects by adding a trim tab definition under <flight_control><channel name="roll"> . metrics unit="KG" unit_area="M2" unit_length="M">
“But how do I even fly it?” Alex asks.