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 = 'custom' |
Private Attributes | |
_input | |
_output | |
Class describing a custom conversion curve between the command input, usually the angular velocity, and the correspondent output thrust force. Here the inverse of the conversion function can be computed so that the command for the desired thrust force is retrieved. The input vector corresponds to sampled values for the command input, and the output vector corresponds to the sampled values for the correspondent thrust forces. This information is usually available in the datasheet of the thruster's manufacturer.
Definition at line 21 of file thruster_custom.py.
def uuv_thrusters.models.thruster_custom.ThrusterCustom.__init__ | ( | self, | |
args, | |||
kwargs | |||
) |
Class constructor.
Definition at line 34 of file thruster_custom.py.
def uuv_thrusters.models.thruster_custom.ThrusterCustom.get_command_value | ( | self, | |
thrust | |||
) |
Definition at line 45 of file thruster_custom.py.
def uuv_thrusters.models.thruster_custom.ThrusterCustom.get_thrust_value | ( | self, | |
command | |||
) |
Computes the thrust force for the given command.
Definition at line 49 of file thruster_custom.py.
|
private |
Definition at line 41 of file thruster_custom.py.
|
private |
Definition at line 43 of file thruster_custom.py.
|
static |
Definition at line 32 of file thruster_custom.py.