Interface used to access the Simple Aerodynamics options for the Basic Acceleration Model of an aircraft.
![]() | Gets or sets the coefficient of drag. |
![]() | Gets or sets the max coefficient of lift. |
![]() | Gets or sets the mode option to treat the aircraft as a helicopter or a fixed wing aircraft when calculating the aircraft's attitude. |
![]() | Gets or sets the reference surface area of the aircraft. |
Configure the basic acceleration performance model of an aircraft
[C#] | ||
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Configure the basic acceleration performance model of an aircraft
[Visual Basic .NET] | ||
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Configure the basic acceleration performance model of an aircraft
[MATLAB] | ||
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