| dampingDerivativesType Complex Type |
Damping derivatives
Namespace: Empty
Schema: Empty
Base Type
UsagesChildren| Name | Occurrences | Description |
|---|---|---|
 All | ||
 dcddpStar | [0, 1] | Change of cd by normalized roll rate |
| dcddqStar | [0, 1] | Change of cd by normalized pitch rate |
| dcddrStar | [0, 1] | Change of cd by normalized yaw rate |
| dcldpStar | [0, 1] | Change of cl by normalized roll rate |
| dcldqStar | [0, 1] | Change of cl by normalized pitch rate |
| dcldrStar | [0, 1] | Change of cl by normalized yaw rate |
| dcmddpStar | [0, 1] | Change of cmd by normalized roll rate |
| dcmddqStar | [0, 1] | Change of cmd by normalized pitch rate |
| dcmddrStar | [0, 1] | Change of cmd by normalized yaw rate |
| dcmldpStar | [0, 1] | Change of cml by normalized roll rate |
| dcmldqStar | [0, 1] | Change of cml by normalized pitch rate |
| dcmldrStar | [0, 1] | Change of cml by normalized yaw rate |
| dcmsdpStar | [0, 1] | Change of cms by normalized roll rate |
| dcmsdqStar | [0, 1] | Change of cms by normalized pitch rate |
| dcmsdrStar | [0, 1] | Change of cms by normalized yaw rate |
| dcsdpStar | [0, 1] | Change of cs by normalized roll rate |
| dcsdqStar | [0, 1] | Change of cs by normalized pitch rate |
| dcsdrStar | [0, 1] | Change of cs by normalized yaw rate |
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 externalDataDirectory |  string | ||
| externalDataNodePath | string | ||
| externalFileName | string |
RemarksThis type contains aerodynamic performance maps with
the damping derivatives. The derivatives are calculated using
rotational rates [rad/s], normalized by:
Rate*ReferenceLength/flow speed. The rotations are performed
around the global axis directions with the aircraft model's
global reference point as origin. The damping derivative
performance maps are vectors of the same length as the input
vectors of the baseline aerodynamic performance maps, consisting of
semicolon separated values.