uuv_thrusters.models.thruster_proportional.ThrusterProportional Class Reference

Inheritance diagram for uuv_thrusters.models.thruster_proportional.ThrusterProportional:

Public Member Functions
def	__init__ (self, args, kwargs)
def	get_command_value (self, thrust)
def	get_thrust_value (self, command)

Static Public Attributes
string	LABEL = 'proportional'

Private Attributes
	_gain

Detailed Description

This model corresponds to the linear relation between a function
abs(command)*command of the command input (usually the command angular
velocity) to the thrust force. A constant gain has to be provided.

Definition at line 21 of file thruster_proportional.py.

Constructor & Destructor Documentation

def uuv_thrusters.models.thruster_proportional.ThrusterProportional.__init__	(		self,
			args,
			kwargs
	)

Definition at line 28 of file thruster_proportional.py.

Member Function Documentation

def uuv_thrusters.models.thruster_proportional.ThrusterProportional.get_command_value	(		self,
			thrust
	)

Definition at line 37 of file thruster_proportional.py.

def uuv_thrusters.models.thruster_proportional.ThrusterProportional.get_thrust_value	(		self,
			command
	)

Computes the thrust force for the given command.

Definition at line 41 of file thruster_proportional.py.

Member Data Documentation

uuv_thrusters.models.thruster_proportional.ThrusterProportional._gain

private

Definition at line 33 of file thruster_proportional.py.

string uuv_thrusters.models.thruster_proportional.ThrusterProportional.LABEL = 'proportional'

static

Definition at line 26 of file thruster_proportional.py.

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

• thruster_proportional.py