| pointPerformanceConstraintsType Complex Type |
Constraints
Namespace: Empty
Schema: Empty
| Name | Occurrences | Description |
|---|---|---|
| | [0, 1] | Rate of velocity [m/s^2] |
| | [0, 1] | Constant altitude [m] |
| | [0, 1] | Angle of attack [deg] |
| | [0, 1] | Calibrated airspeed [m/s] |
| | [0, 1] | Climb angle [deg] |
| | [0, 1] | Duration [s] |
| | [0, 1] | Mach number [-] |
| | [0, 1] | Rate of climb [m/s] |
| | [0, 1] | Rate of turn [deg/s] |
| | [0, 1] | Thrust setting for derated engine as fraction of max. thrust (e.g.: for powered descents, deceleration not at IDLE, manoevres) |
| Name | Type | Required | Description |
|---|---|---|---|