Description
Interface used to access the options for the FourPoint aerodynamic strategy in the missile.
Public Methods
 SetAOA | Gets or sets and validates the maximum, max range and max endurance AOA values for the aircraft. |
| ValidateDragDesignPoints | Validate the drag design points - ensure the choices do not result in a singular system of equations. |
| ValidateLiftDesignPoints | Validate the lift design points - ensure the choices do not result in a singular system of equations. |
Public Properties
 AOA_1 | Gets or sets the AOA for the first design point. |
| AOA_2 | Gets or sets the AOA for the second design point. |
| AOA_3 | Gets or sets the AOA for the third design point. |
| AOA_4 | Gets or sets the AOA for the fourth design point. |
| CD_1 | Gets or sets the drag coefficient for the first design point. |
| CD_2 | Gets or sets the drag coefficient for the second design point. |
| CD_3 | Gets or sets the drag coefficient for the third design point. |
| CD_4 | Gets or sets the drag coefficient for the fourth design point. |
| CL_1 | Gets or sets the lift coefficient for the first design point. |
| CL_2 | Gets or sets the lift coefficient for the second design point. |
| CL_3 | Gets or sets the lift coefficient for the third design point. |
| CL_4 | Gets or sets the lift coefficient for the fourth design point. |
| Mach_1 | Gets or sets the Mach for the first design point. |
| Mach_2 | Gets or sets the Mach for the second design point. |
| Mach_3 | Gets or sets the Mach for the third design point. |
| Mach_4 | Gets or sets the Mach for the fourth design point. |
| MaxAOA | Gets the maximum AOA for the aircraft. |
| MaxEnduranceAOA | Gets the maximum endurance AOA for the aircraft. |
| MaxRangeAOA | Gets the maximum range AOA for the aircraft. |
| SRef | Gets or sets the aerodynamic reference area for the aircraft. |