SUAVE  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
SUAVE.Components.Energy.Networks.Solar.Solar Class Reference
Inheritance diagram for SUAVE.Components.Energy.Networks.Solar.Solar:
SUAVE.Components.Energy.Networks.Network.Network SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component

Public Member Functions

def __defaults__ (self)
 
def evaluate_thrust (self, state)
 
def unpack_unknowns (self, segment)
 
def residuals (self, segment)
 
def add_unknowns_and_residuals_to_segment (self, segment, initial_power_coefficient=0.005)
 

Public Attributes

 solar_flux
 
 solar_panel
 
 motors
 
 propellers
 
 esc
 
 avionics
 
 payload
 
 solar_logic
 
 battery
 
 engine_length
 
 number_of_engines
 
 tag
 
 use_surrogate
 
 generative_design_minimum
 
 identical_propellers
 
- Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network
 tag
 
 generative_design_max_per_vehicle
 
 non_dimensional_origin
 
 number_of_engines
 
 engine_length
 
 wing_mounted
 
 areas
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 
 mass_properties
 
 origin
 
 symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
 tag
 
 origin
 
 generative_design_max_per_vehicle
 
 generative_design_characteristics
 
 generative_design_special_parent
 

Detailed Description

A solar powered system with batteries and maximum power point tracking.
    
    This network adds an extra unknowns to the mission, the torque matching between motor and propeller.

    Assumptions:
    None
    
    Source:
    None

Member Function Documentation

◆ __defaults__()

def SUAVE.Components.Energy.Networks.Solar.Solar.__defaults__ (   self)
This sets the default values for the network to function.
    
    Assumptions:
    None
    
    Source:
    N/A
    
    Inputs:
    None
    
    Outputs:
    None
    
    Properties Used:
    N/A

Reimplemented from SUAVE.Components.Energy.Networks.Network.Network.

◆ add_unknowns_and_residuals_to_segment()

def SUAVE.Components.Energy.Networks.Solar.Solar.add_unknowns_and_residuals_to_segment (   self,
  segment,
  initial_power_coefficient = 0.005 
)
This function sets up the information that the mission needs to run a mission segment using this network
    
    Assumptions:
    None
    
    Source:
    N/A
    
    Inputs:
    segment
    initial_voltage                   [v]
    initial_power_coefficient         [float]s
    
    Outputs:
    segment.state.unknowns.propeller_power_coefficient
    segment.state.conditions.propulsion.propeller_motor_torque
    segment.state.conditions.propulsion.propeller_torque   
    
    Properties Used:
    N/A

◆ evaluate_thrust()

def SUAVE.Components.Energy.Networks.Solar.Solar.evaluate_thrust (   self,
  state 
)
Calculate thrust given the current state of the vehicle
    
    Assumptions:
    Caps the throttle at 110% and linearly interpolates thrust off that
    
    Source:
    N/A
    
    Inputs:
    state [state()]
    
    Outputs:
    results.thrust_force_vector [newtons]
    results.vehicle_mass_rate   [kg/s]
    conditions.propulsion:
solar_flux           [watts/m^2] 
rpm                  [radians/sec]
current              [amps]
battery_power_draw   [watts]
battery_energy       [joules]
motor_torque         [N-M]
propeller_torque     [N-M]
    
    Properties Used:
    Defaulted values

◆ residuals()

def SUAVE.Components.Energy.Networks.Solar.Solar.residuals (   self,
  segment 
)
This packs the residuals to be send to the mission solver.
    
    Assumptions:
    None
    
    Source:
    N/A
    
    Inputs:
    state.conditions.propulsion:
motor_torque                          [N-m]
propeller_torque                      [N-m]
    
    Outputs:
    None
    
    Properties Used:
    None

◆ unpack_unknowns()

def SUAVE.Components.Energy.Networks.Solar.Solar.unpack_unknowns (   self,
  segment 
)
This is an extra set of unknowns which are unpacked from the mission solver and send to the network.
    
    Assumptions:
    None
    
    Source:
    N/A
    
    Inputs:
    state.unknowns.propeller_power_coefficient [None]
    
    Outputs:
    state.conditions.propulsion.propeller_power_coefficient [None]
    
    Properties Used:
    N/A

The documentation for this class was generated from the following file: