public interface ControlAero3DOF
Modified by: Joseph A. Huwaldt
Modifier and Type | Method and Description |
---|---|
float |
getDCA()
Method that returns the body axis axial force coefficient increment due to control deflection.
|
float |
getDCD()
Method that returns the wind axis drag coefficient increment due to control deflection.
|
float |
getDCL()
Returns the wind axis lift coefficient increment due to control deflection.
|
float |
getDCM()
Method that returns the wind axis pitching moment coefficient increment due to control deflection.
|
float |
getDCMb()
Method that returns the body axis pitching moment coefficient increment due to control deflection.
|
float |
getDCN()
Returns the body axis normal force coefficient increment due to control deflection.
|
void |
setAOA(float AOA)
Method that sets the angle of attack in degrees.
|
void |
setDef(float def)
Sets the control deflection angle in degrees
|
void |
setHOB(float hob)
Sets the height above ground level (for ground effect modeling).
|
void |
setMach(float Mach)
Method that sets the Mach number.
|
void setAOA(float AOA)
AOA
- Angle of attack in degrees.void setMach(float Mach)
Mach
- The Mach number.void setDef(float def)
def
- Deflection angle in degrees.void setHOB(float hob)
hob
- The height to the aero reference point
divided by the reference span "bref".float getDCL()
float getDCD()
float getDCM()
float getDCN()
float getDCA()
float getDCMb()