RCAIDE.Library.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.initialize_conditions#
- initialize_conditions(segment)[source]#
Sets the specified conditions which are given for the segment type.
Assumptions: Constant throttle estting, with a constant true airspeed
Source: N/A
Inputs: segment.air_speed [meters/second] segment.altitude_start [meters] segment.altitude_end [meters] segment.state.numerics.dimensionless.control_points [Unitless] conditions.freestream.density [kilograms/meter^3]
Outputs: conditions.frames.inertial.velocity_vector [meters/second]
Properties Used: N/A