blob: 5067a16e350c74494a25939190d1e5da3db7dbf6 [file] [log] [blame]
#!/usr/bin/python
from frc971.control_loops.python import control_loop
from y2020.control_loops.python import flywheel
import numpy
import sys
import gflags
import glog
FLAGS = gflags.FLAGS
gflags.DEFINE_bool('plot', False, 'If true, plot the loop response.')
# Inertia for a single 4" diameter, 2" wide neopreme wheel.
J_wheel = 0.000319 * 2.0
# Gear ratio to the final wheel.
# 40 tooth on the flywheel
# 48 for the falcon.
# 60 tooth on the outer wheel.
G = 48.0 / 40.0
# Overall flywheel inertia.
J = J_wheel * (1.0 + (40.0 / 60.0)**2.0)
# The position and velocity are measured for the final wheel.
kFinisher = flywheel.FlywheelParams(
name='Finisher',
motor=control_loop.Falcon(),
G=G,
J=J,
q_pos=0.08,
q_vel=4.00,
q_voltage=0.4,
r_pos=0.05,
controller_poles=[.84])
def main(argv):
if FLAGS.plot:
R = numpy.matrix([[0.0], [500.0], [0.0]])
flywheel.PlotSpinup(params=kFinisher, goal=R, iterations=200)
return 0
if len(argv) != 5:
glog.fatal('Expected .h file name and .cc file name')
else:
namespaces = ['y2020', 'control_loops', 'superstructure', 'finisher']
flywheel.WriteFlywheel(kFinisher, argv[1:3], argv[3:5], namespaces)
if __name__ == '__main__':
argv = FLAGS(sys.argv)
sys.exit(main(argv))