So I am simulating plane flight. The plane flies certain distance (path variable) and then the simulation stops. The solver is trying to minimize the fuel consumption (m.Maximize(mass*tf*final), by maximizing the mass value. The solver controls the accelerator pedal position (Tcontr). I need it to try and keep Velocity value V above certain threshold(for example >=100). What kind of equation I need to add for that to happen?
My code:
import numpy as np
import matplotlib.pyplot as plt
from gekko import GEKKO
import math
#Gekko model
m = GEKKO(remote=False)
#Time points
nt = 11
tm = np.linspace(0,100,nt)
m.time = tm
# Variables
Ro = m.Const(value=1.1)#
g = m.Const(value=9.80665)
pressure = m.Var(value=101325)#
T = m.Var()
T0 = m.Const(value=273)
S = m.Const(value=122.6)
Cd = m.Const(value=0.1)
FuelFlow = m.Var()
D = m.Var()
Thrmax = m.Const(value=200000)
Thr = m.Var()
V = m.Var(value=100,lb=0,ub=240)
Vmin = m.Var(value=100)
nu = m.Var(value=0)
nuu = nu.value
x = m.Var(value=0,lb=0)
h = m.Var(value=1000)
mass = m.Var(value=60000)
path = m.Const(value=5000000) #intended distance travelled
L = m.Var()
p = np.zeros(nt)
p[-1] = 1.0
final = m.Param(value=p)
m.options.MAX_ITER=50000 # iteration number
#Fixed Variable
tf = m.FV(value=1,lb=0.0001,ub=1000.0)#
tf.STATUS = 1
# Parameters
Tcontr = m.MV(value=0.2,lb=0.2,ub=1)
Tcontr.STATUS = 1
Tcontr.DCOST = 0
# Equations
m.Equation(x.dt()==tf*(V*(math.cos(nuu.value))))#
m.Equation(Thr==Tcontr*Thrmax)
m.Equation(V.dt()==tf*((Thr-D)/mass))#
m.Equation(mass.dt()==tf*(-Thr*(FuelFlow/60000)))#
m.Equation(D==0.5*Ro*(V**2)*Cd*S)
m.Equation(FuelFlow==0.75882*(1+(V/2938.5)))
m.Equation(x*final<=path)
m.Equation(T==T0-(0.0065*h))
# Objective Function
m.Minimize(final*(x-path)**2)
m.Maximize(mass*tf*final)
m.options.IMODE = 6
m.options.NODES = 2 # it was 3 before
m.options.MV_TYPE = 1
m.options.SOLVER = 3
#m.open_folder() # to search for infeasibilities
m.solve()
tm = tm * tf.value[0]
print('Final Time: ' + str((tf.value[-1])*100))
print('Final Speed: ' + str(V.value[-1]))
print('Final X: ' + str(x.value[-1]))
print('Final Mass: ' + str(mass.value[-1]))
fig, axs = plt.subplots(5)
fig.suptitle('Results')
axs[0].plot(tm,Tcontr,'r-',LineWidth=2,label=r'$Tcontr$')
axs[0].legend(loc='best')
axs[1].plot(tm,V.value,'b-',LineWidth=2,label=r'$V$')
axs[1].legend(loc='best')
axs[2].plot(tm,x.value,'r--',LineWidth=2,label=r'$x$')
axs[2].legend(loc='best')
axs[3].plot(tm,D.value,'g-',LineWidth=2,label=r'$D$')
axs[3].legend(loc='best')
axs[4].plot(tm,mass.value,'g:',LineWidth=2,label=r'$mass$')
axs[4].legend(loc='best')
plt.xlabel('Time')
#plt.ylabel('Value')
plt.show()