574
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Aero input and outputs: Difference between revisions
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→Function outputs: deleted stuff I wrote when I had misunderstood how it worked.
(→Lift coefficients:: Updated CL to be L, instead of CL) |
(→Function outputs: deleted stuff I wrote when I had misunderstood how it worked.) |
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| Line 100: | Line 100: | ||
/fdm/jsbsim/metrics/bw-ft | /fdm/jsbsim/metrics/bw-ft | ||
== | === Stall hysteresis, normalized: === | ||
/fdm/jsbsim/aero/stall-hyst-norm | |||
/fdm/jsbsim/aero/ | === Time rate of change in alpha and sideslip in deg/sec and rad/sec: === | ||
/fdm/jsbsim/aero/ | |||
/fdm/jsbsim/aero/alphadot-rad_sec | |||
/fdm/jsbsim/aero/betadot-rad_sec | |||
/fdm/jsbsim/aero/alphadot-deg_sec | |||
/fdm/jsbsim/aero/betadot-deg_sec | |||
== Function outputs == | |||
Runtime-created aerodynamic force and moment components from definitions in | Runtime-created aerodynamic force and moment components from definitions in | ||
the <aerodynamics> section of the configuration file (varies per-aircraft): | the <aerodynamics> section of the configuration file (varies per-aircraft): | ||
Alan wrote about lift: | Alan wrote about lift: | ||
| Line 152: | Line 148: | ||
One thing to be careful about is not including a component twice. e.g. the CL that you are given may already include the tail and fuselage effects, and this case they should not be added in again. | One thing to be careful about is not including a component twice. e.g. the CL that you are given may already include the tail and fuselage effects, and this case they should not be added in again. | ||
{{JSBSim}} | {{JSBSim}} | ||