RCAIDE.Library.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle.residual_altitude#
- residual_altitude(segment)[source]#
Computes the altitude residual
Assumptions: No higher order terms.
Source: N/A
Inputs: segment.state.conditions.frames.inertial.total_force_vector [Newtons] segment.state.conditions.frames.inertial.acceleration_vector [meter/second^2] segment.state.conditions.weights.total_mass [kilogram] segment.state.conditions.freestream.altitude [meter]
Outputs: segment.state.residuals.altitude [meters]
Properties Used: N/A