def _define_params(self):
lwing = self.comps['lwing'].props
lwing['pos'].params[''] = PGMparameter(1, 3)
lwing['pos'].params['lin'] = PGMparameter(3, 3, order_u=2)
lwing['scl'].params[''] = PGMparameter(3, 1, pos_u=[0, 0.52, 1])
lwing['shY', 'upp'].params[''] = PGMparameter(10,
6,
order_u=4,
order_v=4)
lwing['shY', 'low'].params[''] = PGMparameter(10,
6,
order_u=4,
order_v=4)
lstrut = self.comps['lstrut'].props
lstrut['pos'].params[''] = PGMparameter(1, 3)
lstrut['pos'].params['lin'] = PGMparameter(2, 3)
lstrut['scl'].params[''] = PGMparameter(1, 1)
lstrut['scl'].params['2'] = PGMparameter(2, 3)
lstrut['nor'].params[''] = PGMparameter(2, 1)
lstrut['rot'].params[''] = PGMparameter(3, 3, pos_u=[0, 0.15, 1])
lstrut['shY', 'upp'].params[''] = PGMparameter(10,
3,
order_u=4,
order_v=3)
lstrut['shY', 'low'].params[''] = PGMparameter(10,
3,
order_u=4,
order_v=3)
lv = self.comps['lv'].props
lv['pos'].params[''] = PGMparameter(1, 3)
lv['pos'].params['lin'] = PGMparameter(2, 3)
lv['scl'].params[''] = PGMparameter(2, 1)
lv['nor'].params[''] = PGMparameter(3, 1)
lv['rot'].params[''] = PGMparameter(2, 3, pos_u=[0, 1])
lv['shY', 'upp'].params[''] = PGMparameter(10, 2, order_u=4, order_v=2)
lv['shY', 'low'].params[''] = PGMparameter(10, 2, order_u=4, order_v=2)
lstrut_lwing = self.comps['lstrut_lwing'].props
lstrut_lwing['shN', ''].params[''] = PGMparameter(7, 7)
def _define_params(this):
fuse = this.comps['fuse'].props #1st parameter: streamwise
fuse['pos'].params[''] = PGMparameter(
2, 3) #Specify the cylinder front and end
fuse['nor'].params[''] = PGMparameter(1, 3) #Normal of each section
fuse['scl'].params[''] = PGMparameter(1, 1)
fuse['flt'].params[''] = PGMparameter(3, 4, pos_u=[0.0, 0.2, 1.0])
fuse['pos'].params['nose'] = PGMparameter(3,
3,
pos_u=[0, 0.15, 0.3],
order_u=3)
fuse['scl'].params['nose_y'] = PGMparameter(3,
3,
pos_u=[0, 0.15, 0.3],
order_u=3)
fuse['scl'].params['nose_z'] = PGMparameter(3,
3,
pos_u=[0, 0.1, 0.2],
order_u=3)
fuse['pos'].params['bottom'] = PGMparameter(3,
3,
pos_u=[0.2, 0.88, 1.0],
order_u=2)
fuse['scl'].params['bottom'] = PGMparameter(3,
3,
pos_u=[0.2, 0.88, 1.0],
order_u=2)
fuse['rot'].params['bottom'] = PGMparameter(3,
3,
pos_u=[0.2, 0.88, 1.0],
order_u=2)
lwing = this.comps['lwing'].props
lwing['pos'].params[''] = PGMparameter(1, 3)
lwing['pos'].params['lin'] = PGMparameter(3, 3, order_u=2)
lwing['scl'].params[''] = PGMparameter(3, 3, order_u=2)
rwing = this.comps['rwing'].props
rwing['pos'].params[''] = PGMparameter(1, 3)
rwing['pos'].params['lin'] = PGMparameter(3, 3, order_u=2)
rwing['scl'].params[''] = PGMparameter(3, 3, order_u=2)
if this.tail:
ctail = this.comps['ctail'].props
ctail['pos'].params[''] = PGMparameter(1, 3)
ctail['pos'].params['lin'] = PGMparameter(2, 3)
ctail['scl'].params[''] = PGMparameter(2, 3)
ctail['nor'].params[''] = PGMparameter(1, 3)
flap = this.comps['flap'].props
flap['pos'].params[''] = PGMparameter(1, 3)
flap['pos'].params['lin'] = PGMparameter(2, 3)
flap['scl'].params[''] = PGMparameter(2, 3)
flap['rot'].params[''] = PGMparameter(2, 3)
def _define_params(self):
fuse = self.comps['fuse'].props
fuse['pos'].params[''] = PGMparameter(2, 3)
fuse['nor'].params[''] = PGMparameter(1, 1)
fuse['scl'].params[''] = PGMparameter(1, 1)
fuse['flt'].params[''] = PGMparameter(2, 4, pos_u=[0.28, 0.53])
fuse['pos'].params['nose'] = PGMparameter(3,
3,
pos_u=[0, 0.065, 0.13],
order_u=3)
fuse['scl'].params['nose'] = PGMparameter(3,
1,
pos_u=[0, 0.07, 0.14],
order_u=3)
fuse['scl'].params['tail'] = PGMparameter(2, 1, pos_u=[0.7, 1.0])
lwing = self.comps['lwing'].props
lwing['pos'].params[''] = PGMparameter(1, 3)
lwing['scl'].params[''] = PGMparameter(3, 1, pos_u=[0, 0.35, 1.0])
lwing['pos'].params['lin'] = PGMparameter(2, 3)
lpylon = self.comps['lpylon'].props
lpylon['pos'].params[''] = PGMparameter(1, 3)
lpylon['pos'].params['lin'] = PGMparameter(2, 3)
lpylon['scl'].params[''] = PGMparameter(2, 1)
lpylon['nor'].params[''] = PGMparameter(1, 3)
lnac = self.comps['lnac'].props
lnac['pos'].params[''] = PGMparameter(1, 3)
lnac['pos'].params['lin'] = PGMparameter(2, 3)
lnac['nor'].params[''] = PGMparameter(1, 1)
lnac['scl'].params[''] = PGMparameter(1, 1)
lnac['thk'].params[''] = PGMparameter(3, 1)
ltail = self.comps['ltail'].props
ltail['pos'].params[''] = PGMparameter(1, 3)
ltail['pos'].params['lin'] = PGMparameter(2, 3)
ltail['scl'].params[''] = PGMparameter(2, 1)
ltail['rot'].params[''] = PGMparameter(2, 3)
ltail['ogn'].params[''] = PGMparameter(1, 3)
vtail = self.comps['vtail'].props
vtail['pos'].params[''] = PGMparameter(1, 3)
vtail['pos'].params['lin'] = PGMparameter(2, 3)
vtail['nor'].params[''] = PGMparameter(1, 3)
vtail['scl'].params[''] = PGMparameter(2, 1)
vtail['rot'].params[''] = PGMparameter(2, 3)
vtail['ogn'].params[''] = PGMparameter(1, 3)
def _define_params(self):
fuse_props = self.comps[
'fuse'].props #Get the reference to the body properties
fuse_props['pos'].params[''] = PGMparameter(
4, 3, order_u=3
) #This command states that we will have 4 points (linearly spaced between u=0.0 and u=1.0) to specify the fuselage center-line control points. In addition, the interpolation between the sections will be parabolic due to the order_u=3 option.
fuse_props['nor'].params[''] = PGMparameter(
1, 1
) #This controls the normal of the faces with respect to the center-line
fuse_props['scl'].params[''] = PGMparameter(
4, 3
) #We will specify the radius along 4 linearly spaced sections and in 3 directions (x,y,z, although the z one is ignored) to make an ellipse. Linear interpolation will be used for the radius of intermediate sections.
fuse_props['flt'].params[''] = PGMparameter(
1, 1
) #This parameter steadily turns elliptical cross-sections into rectangular cross-sections.
wing_l_props = self.comps[
'wing_l'].props #Get the reference to the left wing parameters
wing_l_props['pos'].params[''] = PGMparameter(
2, 3
) #We need to set 3 coordinates (x,y,z) for the root section and the tip section (root + tip, hence the 2)
wing_l_props['scl'].params[''] = PGMparameter(
2, 1
) #We will specify the chord of the root and the tip with the scaling parameter (1 because the same scaling is applied to x,y,z, though z is irrelevant)
wing_r_props = self.comps[
'wing_r'].props #Get the reference to the right wing parameters
wing_r_props['pos'].params[''] = PGMparameter(2, 3)
wing_r_props['scl'].params[''] = PGMparameter(2, 1)
htail_l_props = self.comps[
'htail_l'].props #Get the reference to the left tail parameters
htail_l_props['pos'].params[''] = PGMparameter(2, 3)
htail_l_props['scl'].params[''] = PGMparameter(2, 3)
htail_l_props['rot'].params[''] = PGMparameter(
2, 3
) #Now we use 3 parameters to set rotations around 3 axes (x,y,z) for the root and tip sections
htail_r_props = self.comps[
'htail_r'].props #Get the reference to the right tail parameters
htail_r_props['pos'].params[''] = PGMparameter(2, 3)
htail_r_props['scl'].params[''] = PGMparameter(2, 3)
htail_r_props['rot'].params[''] = PGMparameter(2, 3)
vtail_props = self.comps[
'vtail'].props #Get the reference to the vertical tail parameters
vtail_props['pos'].params[''] = PGMparameter(2, 3)
vtail_props['scl'].params[''] = PGMparameter(2, 3)
vtail_props['nor'].params[''] = PGMparameter(
2, 3
) #We will turn on the normal condition for the root and tip sections
vtail_props['rot'].params[''] = PGMparameter(2, 3)
def _define_params(self):
fuse = self.comps['fuse'].props
fuse['nor'].params[''] = PGMparameter(1, 3)
fuse['pos'].params[''] = PGMparameter(2, 3)
fuse['pos'].params['nose'] = PGMparameter(2, 3, pos_u=[0, 0.12])
fuse['pos'].params['tail'] = PGMparameter(2, 3, pos_u=[0.76, 1.0])
# fuse['scl'].params['rad'] = PGMparameter(4, 1, pos_u=[0,0.14,0.75,1.0])
fuse['scl'].params['rad1'] = PGMparameter(4,
1,
pos_u=[0, 0.01, 0.05, 0.12],
order_u=4)
fuse['scl'].params['rad2'] = PGMparameter(2, 1, pos_u=[0.12, 0.76])
fuse['scl'].params['rad3'] = PGMparameter(4,
1,
pos_u=[0.76, 0.83, 0.99, 1],
order_u=4)
fuse['scl'].params['tail'] = PGMparameter(2, 3, pos_u=[0.76, 1.0])
fuse['flt'].params['flt1a'] = PGMparameter(
4, 2, pos_u=[0.24, 0.27, 0.33, 0.36], pos_v=[0.5, 1], order_u=4)
fuse['flt'].params['flt1b'] = PGMparameter(2,
2,
pos_u=[0.36, 0.41],
pos_v=[0.5, 1])
fuse['flt'].params['flt1c'] = PGMparameter(
4, 2, pos_u=[0.41, 0.44, 0.49, 0.52], pos_v=[0.5, 1], order_u=4)
fuse['flt'].params['flt2a'] = PGMparameter(
4, 2, pos_u=[0.24, 0.27, 0.33, 0.36], pos_v=[0, 0.5], order_u=4)
fuse['flt'].params['flt2b'] = PGMparameter(2,
2,
pos_u=[0.36, 0.41],
pos_v=[0, 0.5])
fuse['flt'].params['flt2c'] = PGMparameter(
4, 2, pos_u=[0.41, 0.44, 0.49, 0.52], pos_v=[0, 0.5], order_u=4)
lwing = self.comps['lwing'].props
lwing['pos'].params[''] = PGMparameter(1, 3)
lwing['scl'].params[''] = PGMparameter(2, 1)
lwing['pos'].params['lin'] = PGMparameter(3, 3, order_u=3)
lstrut = self.comps['lstrut'].props
lstrut['pos'].params[''] = PGMparameter(1, 3)
lstrut['pos'].params['lin'] = PGMparameter(2, 3)
# lstrut['pos'].params['curv'] = PGMparameter(3, 3, pos_u=[0.9,0.95,1.0], order_u=3)
lstrut['scl'].params[''] = PGMparameter(2, 1)
lstrut['nor'].params[''] = PGMparameter(1, 1)
# lstrut['rot'].params[''] = PGMparameter(2, 3, pos_u=[0.85,1.0])
# lstrut['rot'].params[''] = PGMparameter(2, 3, pos_u=[0,1.0])
lv = self.comps['lv'].props
lv['pos'].params[''] = PGMparameter(1, 3)
lv['pos'].params['lin'] = PGMparameter(2, 3)
lv['scl'].params[''] = PGMparameter(2, 1)
lv['nor'].params[''] = PGMparameter(1, 1)
lv['rot'].params[''] = PGMparameter(2, 3, pos_u=[0, 1])
ltail = self.comps['ltail'].props
ltail['pos'].params[''] = PGMparameter(1, 3)
ltail['pos'].params['lin'] = PGMparameter(2, 3)
ltail['scl'].params[''] = PGMparameter(2, 1)
vtail = self.comps['vtail'].props
vtail['pos'].params[''] = PGMparameter(1, 3)
vtail['pos'].params['lin'] = PGMparameter(2, 3)
vtail['scl'].params[''] = PGMparameter(2, 1)
vtail['nor'].params[''] = PGMparameter(1, 3)
def _define_params(self):
wing = self.comps['wing'].props
wing['pos'].params[''] = PGMparameter(3, 3, pos_u=[0,0.37,1.0])
wing['scl'].params[''] = PGMparameter(3, 1, pos_u=[0,0.37,1.0])
def _define_params(self):
fuse = self.comps['fuse'].props #1st parameter: streamwise
fuse['pos'].params[''] = PGMparameter(
2, 3) #Specify the cylinder front and end
fuse['nor'].params[''] = PGMparameter(1, 1) #Normal of each section
fuse['scl'].params[''] = PGMparameter(1, 1)
fuse['flt'].params[''] = PGMparameter(2, 4, pos_u=[0.28, 0.53])
fuse['pos'].params['nose'] = PGMparameter(3,
3,
pos_u=[0, 0.065, 0.13],
order_u=3)
fuse['scl'].params['nose'] = PGMparameter(3,
1,
pos_u=[0, 0.07, 0.14],
order_u=3)
fuse['scl'].params['tail'] = PGMparameter(2, 1, pos_u=[0.7, 1.0])
lwing = self.comps['lwing'].props
lwing['pos'].params[''] = PGMparameter(1, 3)
lwing['scl'].params[''] = PGMparameter(3, 1, pos_u=[0, 0.35, 1.0])
lwing['pos'].params['lin'] = PGMparameter(2, 3)
lwing['shY', 'upp'].params[''] = PGMparameter(10,
6,
order_u=4,
order_v=4)
lwing['shY', 'low'].params[''] = PGMparameter(10,
6,
order_u=4,
order_v=4)
rwing = self.comps['rwing'].props
rwing['pos'].params[''] = PGMparameter(1, 3)
rwing['scl'].params[''] = PGMparameter(3, 1, pos_u=[0, 0.65, 1.0])
rwing['pos'].params['lin'] = PGMparameter(2, 3)
rwing['shY', 'upp'].params[''] = PGMparameter(10,
6,
order_u=4,
order_v=4)
rwing['shY', 'low'].params[''] = PGMparameter(10,
6,
order_u=4,
order_v=4)
lpylon = self.comps['lpylon'].props
lpylon['pos'].params[''] = PGMparameter(1, 3)
lpylon['pos'].params['lin'] = PGMparameter(2, 3)
lpylon['scl'].params[''] = PGMparameter(2, 1)
lpylon['nor'].params[''] = PGMparameter(1, 3)
lnac = self.comps['lnac'].props
lnac['pos'].params[''] = PGMparameter(1, 3)
lnac['pos'].params['lin'] = PGMparameter(2, 3)
lnac['nor'].params[''] = PGMparameter(1, 1)
lnac['scl'].params[''] = PGMparameter(1, 1)
lnac['thk'].params[''] = PGMparameter(3, 1)
ltail = self.comps['ltail'].props
ltail['pos'].params[''] = PGMparameter(1, 3)
ltail['pos'].params['lin'] = PGMparameter(2, 3)
ltail['scl'].params[''] = PGMparameter(2, 1)
ltail['rot'].params[''] = PGMparameter(2, 3)
ltail['ogn'].params[''] = PGMparameter(1, 3)
rtail = self.comps['rtail'].props
rtail['pos'].params[''] = PGMparameter(1, 3)
rtail['pos'].params['lin'] = PGMparameter(2, 3)
rtail['scl'].params[''] = PGMparameter(2, 1)
rtail['rot'].params[''] = PGMparameter(2, 3)
rtail['ogn'].params[''] = PGMparameter(1, 3)
vtail = self.comps['vtail'].props
vtail['pos'].params[''] = PGMparameter(1, 3)
vtail['pos'].params['lin'] = PGMparameter(2, 3)
vtail['nor'].params[''] = PGMparameter(1, 3)
vtail['scl'].params[''] = PGMparameter(2, 1)
vtail['rot'].params[''] = PGMparameter(2, 3)
vtail['ogn'].params[''] = PGMparameter(1, 3)
lwing_fuse = self.comps['lwing_fuse'].props
lwing_fuse['shN', ''].params[''] = PGMparameter(7, 7)
def _define_params(self):
fuse = self.comps['fuse'].props
fuse['pos'].params[''] = PGMparameter(2, 3)
fuse['pos'].params['nose'] = PGMparameter(2, 3, pos_u=[0, 0.45])
fuse['pos'].params['tail'] = PGMparameter(2, 3, pos_u=[0.85, 1.0])
fuse['scl'].params['rad_nose'] = PGMparameter(
4, 1, pos_u=[0, 0.05, 0.41, 0.45], order_u=4)
fuse['scl'].params['rad_middle'] = PGMparameter(2,
1,
pos_u=[0.45, 0.85])
fuse['scl'].params['rad_tail'] = PGMparameter(
4, 1, pos_u=[0.85, 0.87, 0.98, 1.0], order_u=4)
fuse['nor'].params[''] = PGMparameter(1, 3)
lwing = self.comps['lwing'].props
lwing['pos'].params[''] = PGMparameter(1, 3)
lwing['pos'].params['lin'] = PGMparameter(3, 3, order_u=2)
lwing['scl'].params[''] = PGMparameter(2, 1)
lwing['rot'].params[''] = PGMparameter(2, 3)
pylon = self.comps['pylon'].props
pylon['pos'].params[''] = PGMparameter(1, 3)
pylon['pos'].params['lin'] = PGMparameter(2, 3)
pylon['scl'].params[''] = PGMparameter(2, 1)
pylon['nor'].params[''] = PGMparameter(1, 3)
nac = self.comps['nac'].props
nac['pos'].params[''] = PGMparameter(1, 3)
nac['pos'].params['lin'] = PGMparameter(2, 3)
nac['nor'].params[''] = PGMparameter(1, 1)
nac['scl'].params[''] = PGMparameter(3,
1,
pos_u=[0, 0.8, 1],
order_u=3)
nac['thk'].params[''] = PGMparameter(3, 1)