| #!/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)) |