RCAIDE.Library.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude.initialize_conditions#
- initialize_conditions(segment)[source]#
Sets the specified conditions which are given for the segment type.
Assumptions: Constant throttle and constant altitude, allows for acceleration
Source: N/A
Inputs: segment.altitude [meters] segment.air_speed_start [meters/second] segment.air_speed_end [meters/second] segment.state.numerics.number_of_control_points [int]
Outputs: conditions.frames.inertial.position_vector [meters] conditions.freestream.altitude [meters]
Properties Used: N/A