Cannot recreate demo in examples of VTOL aircraft #414

from __future__ import print_function

import os
import matplotlib.pyplot as plt  # MATLAB plotting functions
from control.matlab import *    # MATLAB-like functions
import numpy as np

# System parameters
m = 4               
J = 0.0475       
r = 0.25         
g = 9.8            
c = 0.05           

Pi = tf([r], [J, 0, 0])  # inner loop (roll)
Po = tf([1], [m, c, 0])  # outer loop (position)

# Use state space versions
Pi = tf2ss(Pi)
Po = tf2ss(Po)


#
# This is the controller for the pitch dynamics.  Goal is to have
# fast response for the pitch dynamics so that we can use this as a 
# control for the lateral dynamics
#

# Design a simple lead controller for the system
k, a, b = 200, 2, 50
Ci = k*tf([1, a], [1, b])  # lead compensator
Li = Pi*Ci

Si = feedback(1, Li)
Ti = Li*Si

Hi = parallel(feedback(Ci, Pi), -m*g*feedback(Ci*Pi, 1))

a, b, K = 0.02, 5, 2
Co = -K*tf([1, 0.3], [1, 10])  # another lead compensator
Lo = -m*g*Po*Co



# Finally compute the real outer-loop loop gain + responses
L = Co*Hi*Po
S = feedback(1, L)
T = feedback(L, 1)

plt.figure('time domain response')
y,t=step(T,T=np.linspace(0,10,100))
plt.plot(t,y)
plt.xlabel('time/s')
plt.ylabel('y(t)')
plt.grid()

plt.figure('bode graph')
bode(L, np.logspace(-4, 3))

plt.figure('nyquist')
print(L)
nyquist(L, (0.0001, 1000))
plt.axis([-4000, 300, -300000, 300000])

plt.figure('4 diags')
gangof4(Hi*Po, Co)
plt.show()