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Aero input and outputs: Difference between revisions
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/fdm/jsbsim/aero/ci2vel | /fdm/jsbsim/aero/ci2vel | ||
Alpha of the wing in radians (includes the angle of incidence of the wing, | |||
if input): | |||
/fdm/jsbsim/aero/alpha-wing-rad | |||
Altitude of CG divided by wing span: | |||
/fdm/jsbsim/aero/h_b-cg-ft | |||
Altitude of MAC divided by wing span: | |||
/fdm/jsbsim/aero/h_b-mac-ft | |||
Aerodynamic rotational rates in rad/sec (includes wind effects, if any): | |||
/fdm/jsbsim/velocities/p-aero-rad_sec | |||
/fdm/jsbsim/velocities/q-aero-rad_sec | |||
/fdm/jsbsim/velocities/r-aero-rad_sec | |||
Aerodynamic velocities in ft/sec (includes wind effects, if any): | |||
/fdm/jsbsim/velocities/u-aero-fps | |||
/fdm/jsbsim/velocities/v-aero-fps | |||
/fdm/jsbsim/velocities/w-aero-fps | |||
The body axis aerodynamic force vector of the aircraft in lbs: | |||
/fdm/jsbsim/forces/fbx-aero-lbs | |||
/fdm/jsbsim/forces/fby-aero-lbs | |||
/fdm/jsbsim/forces/fbz-aero-lbs | |||
The stability axis aerodynamic force vector of the aircraft in lbs: | |||
/fdm/jsbsim/forces/fwx-aero-lbs | |||
/fdm/jsbsim/forces/fwy-aero-lbs | |||
/fdm/jsbsim/forces/fwz-aero-lbs | |||
The body axis aerodynamic moment vector of the aircraft in ft-lbs: | |||
/fdm/jsbsim/moments/l-aero-lbsft | |||
/fdm/jsbsim/moments/m-aero-lbsft | |||
/fdm/jsbsim/moments/n-aero-lbsft | |||
The lift coefficient squared: | |||
/fdm/jsbsim/aero/cl-squared | |||
Dynamic pressure times reference area: | |||
/fdm/jsbsim/aero/qbar-area | |||
Angles of attack and sideslip in radians and degrees (and the magnitudes): | |||
/fdm/jsbsim/aero/alpha-rad | |||
/fdm/jsbsim/aero/beta-rad | |||
/fdm/jsbsim/aero/mag-beta-rad | |||
/fdm/jsbsim/aero/alpha-deg | |||
/fdm/jsbsim/aero/beta-deg | |||
/fdm/jsbsim/aero/mag-beta-deg | |||
Dynamic pressure in psf: | |||
/fdm/jsbsim/aero/qbar-psf | |||
Dynamic pressure in the body axis XZ plane: | |||
/fdm/jsbsim/aero/qbarUW-psf | |||
Dynamic pressure in the body axis XY plane: | |||
/fdm/jsbsim/aero/qbarUV-psf | |||
Others: | |||
metrics/cbarw-ft | |||
metrics/bw-ft | |||
== Function outputs == | == Function outputs == | ||
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Lift coefficients: | Lift coefficients: | ||
/fdm/jsbsim/aero/coefficient/CL - Lift coefficient | |||
/fdm/jsbsim/aero/coefficient/CLwbh | /fdm/jsbsim/aero/coefficient/CLwbh | ||
/fdm/jsbsim/aero/coefficient/CLDf | /fdm/jsbsim/aero/coefficient/CLDf | ||
| Line 40: | Line 118: | ||
/fdm/jsbsim/aero/coefficient/CLadot | /fdm/jsbsim/aero/coefficient/CLadot | ||
/fdm/jsbsim/aero/coefficient/CLq | /fdm/jsbsim/aero/coefficient/CLq | ||
/fdm/jsbsim/aero/coefficient/CLDsb - Lift coefficient of airbrake | |||
/fdm/jsbsim/aero/coefficient/CLDflaps - Lift coefficient of flaps | |||
Drag coefficients: | Drag coefficients: | ||
/fdm/jsbsim/aero/coefficient/CD - Drag coefficient | |||
/fdm/jsbsim/aero/coefficient/CDo | /fdm/jsbsim/aero/coefficient/CDo | ||
/fdm/jsbsim/aero/coefficient/CDDf | /fdm/jsbsim/aero/coefficient/CDDf | ||
| Line 48: | Line 129: | ||
/fdm/jsbsim/aero/coefficient/CDDe | /fdm/jsbsim/aero/coefficient/CDDe | ||
/fdm/jsbsim/aero/coefficient/CDbeta | /fdm/jsbsim/aero/coefficient/CDbeta | ||
/fdm/jsbsim/aero/coefficient/CDDsb - Drag coefficient of airbrake | |||
/fdm/jsbsim/aero/coefficient/CDgear - Drag coefficient of gear | |||
/fdm/jsbsim/aero/coefficient/CDDflaps - Drag coefficient of flaps | |||
Side force coefficients: | Side force coefficients: | ||
/fdm/jsbsim/aero/coefficient/CYb | /fdm/jsbsim/aero/coefficient/CYb - Side Force coefficient due to Sideslip | ||
/fdm/jsbsim/aero/coefficient/CYda | /fdm/jsbsim/aero/coefficient/CYda | ||
/fdm/jsbsim/aero/coefficient/CYdr | /fdm/jsbsim/aero/coefficient/CYdr | ||
| Line 73: | Line 157: | ||
/fdm/jsbsim/aero/coefficient/Cmo | /fdm/jsbsim/aero/coefficient/Cmo | ||
/fdm/jsbsim/aero/coefficient/Cmde | /fdm/jsbsim/aero/coefficient/Cmde | ||
/fdm/jsbsim/aero/coefficient/CmDsb - | |||
Yaw moment coefficients: | Yaw moment coefficients: | ||
| Line 81: | Line 166: | ||
/fdm/jsbsim/aero/coefficient/Cnda | /fdm/jsbsim/aero/coefficient/Cnda | ||
/fdm/jsbsim/aero/coefficient/Cndr | /fdm/jsbsim/aero/coefficient/Cndr | ||
Stall hysteresis, normalized: | Stall hysteresis, normalized: | ||
/fdm/jsbsim/aero/stall-hyst-norm | /fdm/jsbsim/aero/stall-hyst-norm | ||
Time rate of change in alpha and sideslip in deg/sec and rad/sec: | Time rate of change in alpha and sideslip in deg/sec and rad/sec: | ||
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/fdm/jsbsim/aero/alphadot-deg_sec | /fdm/jsbsim/aero/alphadot-deg_sec | ||
/fdm/jsbsim/aero/betadot-deg_sec | /fdm/jsbsim/aero/betadot-deg_sec | ||
{{JSBSim}} | {{JSBSim}} | ||