def test_Ex10_cross_track_distance():
# Position A1 and A2 and B are given as n_EA1_E, n_EA2_E, and n_EB_E:
# Enter elements as lat/long in deg:
n_EA1_E = lat_lon2n_E(rad(0), rad(0))
n_EA2_E = lat_lon2n_E(rad(10), rad(0))
n_EB_E = lat_lon2n_E(rad(1), rad(0.1))
radius = 6371e3 # m, mean Earth radius
# Find the cross track distance from path A to position B.
# SOLUTION:
# Find the unit normal to the great circle:
c_E = unit(np.cross(n_EA1_E, n_EA2_E, axis=0))
# Find the great circle cross track distance:
s_xt = -np.arcsin(np.dot(c_E.T, n_EB_E)) * radius
# Find the Euclidean cross track distance:
d_xt = -np.dot(c_E.T, n_EB_E) * radius
msg = 'Ex10, Cross track distance = {} m, Euclidean = {} m'
print(msg.format(s_xt, d_xt))
assert_array_almost_equal(s_xt, 11117.79911015)
assert_array_almost_equal(d_xt, 11117.79346741)
def test_Ex9_intersection():
# Two paths A and B are given by two pairs of positions:
# Enter elements as lat/long in deg:
n_EA1_E = lat_lon2n_E(rad(10), rad(20))
n_EA2_E = lat_lon2n_E(rad(30), rad(40))
n_EB1_E = lat_lon2n_E(rad(50), rad(60))
n_EB2_E = lat_lon2n_E(rad(70), rad(80))
# Find the intersection between the two paths, n_EC_E:
n_EC_E_tmp = unit(np.cross(np.cross(n_EA1_E, n_EA2_E, axis=0),
np.cross(n_EB1_E, n_EB2_E, axis=0), axis=0))
# n_EC_E_tmp is one of two solutions, the other is -n_EC_E_tmp. Select
# the one that is closet to n_EA1_E, by selecting sign from the dot
# product between n_EC_E_tmp and n_EA1_E:
n_EC_E = np.sign(np.dot(n_EC_E_tmp.T, n_EA1_E)) * n_EC_E_tmp
# When displaying the resulting position for humans, it is more
# convenient to see lat, long:
lat_EC, long_EC = n_E2lat_lon(n_EC_E)
msg = 'Ex9, Intersection: lat, long = {} {} deg'
print(msg.format(deg(lat_EC), deg(long_EC)))
assert_array_almost_equal(deg(lat_EC), 40.31864307)
assert_array_almost_equal(deg(long_EC), 55.90186788)
def test_Ex9_intersect():
# Two paths A and B are given by two pairs of positions:
# Enter elements as lat/long in deg:
n_EA1_E = lat_lon2n_E(rad(10), rad(20))
n_EA2_E = lat_lon2n_E(rad(30), rad(40))
n_EB1_E = lat_lon2n_E(rad(50), rad(60))
n_EB2_E = lat_lon2n_E(rad(70), rad(80))
# Find the intersection between the two paths, n_EC_E:
n_EC_E_tmp = unit(
np.cross(np.cross(n_EA1_E, n_EA2_E, axis=0),
np.cross(n_EB1_E, n_EB2_E, axis=0),
axis=0))
# n_EC_E_tmp is one of two solutions, the other is -n_EC_E_tmp. Select
# the one that is closet to n_EA1_E, by selecting sign from the dot
# product between n_EC_E_tmp and n_EA1_E:
n_EC_E = np.sign(np.dot(n_EC_E_tmp.T, n_EA1_E)) * n_EC_E_tmp
# When displaying the resulting position for humans, it is more
# convenient to see lat, long:
lat_EC, long_EC = n_E2lat_lon(n_EC_E)
msg = 'Ex9, Intersection: lat, long = {} {} deg'
print(msg.format(deg(lat_EC), deg(long_EC)))
assert_array_almost_equal(deg(lat_EC), 40.31864307)
assert_array_almost_equal(deg(long_EC), 55.90186788)
def test_Ex6_interpolated_position():
# Position B at time t0 and t2 is given as n_EB_E_t0 and n_EB_E_t1:
# Enter elements as lat/long in deg:
n_EB_E_t0 = lat_lon2n_E(rad(89), rad(0))
n_EB_E_t1 = lat_lon2n_E(rad(89), rad(180))
# The times are given as:
t0 = 10
t1 = 20
ti = 16 # time of interpolation
# Find the interpolated position at time ti, n_EB_E_ti
# SOLUTION:
# Using standard interpolation:
n_EB_E_ti = unit(n_EB_E_t0 + (ti - t0) * (n_EB_E_t1 - n_EB_E_t0) /
(t1 - t0))
# When displaying the resulting position for humans, it is more
# convenient to see lat, long:
lat_EB_ti, long_EB_ti = n_E2lat_lon(n_EB_E_ti)
msg = 'Ex6, Interpolated position: lat, long = {} {} deg'
print(msg.format(deg(lat_EB_ti), deg(long_EB_ti)))
assert_array_almost_equal(deg(lat_EB_ti), 89.7999805)
assert_array_almost_equal(deg(long_EB_ti), 180.)
def test_Ex10_cross_track_distance():
# Position A1 and A2 and B are given as n_EA1_E, n_EA2_E, and n_EB_E:
# Enter elements as lat/long in deg:
n_EA1_E = lat_lon2n_E(rad(0), rad(0))
n_EA2_E = lat_lon2n_E(rad(10), rad(0))
n_EB_E = lat_lon2n_E(rad(1), rad(0.1))
r_Earth = 6371e3 # m, mean Earth radius
# Find the cross track distance from path A to position B.
# SOLUTION:
# Find the unit normal to the great circle:
c_E = unit(np.cross(n_EA1_E, n_EA2_E, axis=0))
# Find the great circle cross track distance:
s_xt = (np.arccos(np.dot(c_E.T, n_EB_E)) - np.pi / 2) * r_Earth
# Find the Euclidean cross track distance:
d_xt = -np.dot(c_E.T, n_EB_E) * r_Earth
msg = 'Ex10, Cross track distance = {} m, Euclidean = {} m'
print(msg.format(s_xt, d_xt))
assert_array_almost_equal(s_xt, 11117.79911015)
assert_array_almost_equal(d_xt, 11117.79346741)
def test_Ex6_interpolated_position():
# Position B at time t0 and t2 is given as n_EB_E_t0 and n_EB_E_t1:
# Enter elements as lat/long in deg:
n_EB_E_t0 = lat_lon2n_E(rad(89), rad(0))
n_EB_E_t1 = lat_lon2n_E(rad(89), rad(180))
# The times are given as:
t0 = 10
t1 = 20
ti = 16 # time of interpolation
# Find the interpolated position at time ti, n_EB_E_ti
# SOLUTION:
# Using standard interpolation:
n_EB_E_ti = unit(n_EB_E_t0 +
(ti - t0) * (n_EB_E_t1 - n_EB_E_t0) / (t1 - t0))
# When displaying the resulting position for humans, it is more
# convenient to see lat, long:
lat_EB_ti, long_EB_ti = n_E2lat_lon(n_EB_E_ti)
msg = 'Ex6, Interpolated position: lat, long = {} {} deg'
print(msg.format(deg(lat_EB_ti), deg(long_EB_ti)))
assert_array_almost_equal(deg(lat_EB_ti), 89.7999805)
assert_array_almost_equal(deg(long_EB_ti), 180.)
def lla2enu(init_lla,point_lla):
n_EA_E = nv.lat_lon2n_E(init_lla[0], init_lla[1])
n_EB_E = nv.lat_lon2n_E(point_lla[0], point_lla[1])
p_AB_E = nv.n_EA_E_and_n_EB_E2p_AB_E(n_EA_E, n_EB_E, init_lla[2], point_lla[2])
R_EN = nv.n_E2R_EN(n_EA_E)
p_AB_N = np.dot(R_EN.T, p_AB_E).ravel()
p_AB_N[0],p_AB_N[1] = p_AB_N[1],p_AB_N[0]
return p_AB_N
def test_Ex8_position_A_and_azimuth_and_distance_to_B():
# Position A is given as n_EA_E:
# Enter elements as lat/long in deg:
lat, lon = rad(80), rad(-90)
n_EA_E = lat_lon2n_E(lat, lon)
# The initial azimuth and great circle distance (s_AB), and Earth
# radius (r_Earth) are also given:
azimuth = rad(200)
s_AB = 1000 # m
r_Earth = 6371e3 # m, mean Earth radius
# Find the destination point B, as n_EB_E ("The direct/first geodetic
# problem" for a sphere)
# SOLUTION:
# Step1: Convert distance in meter into distance in [rad]:
distance_rad = s_AB / r_Earth
# Step2: Find n_EB_E:
n_EB_E = n_EA_E_distance_and_azimuth2n_EB_E(n_EA_E, distance_rad,
azimuth)
# When displaying the resulting position for humans, it is more
# convenient to see lat, long:
lat_EB, long_EB = n_E2lat_lon(n_EB_E)
print('Ex8, Destination: lat, long = {0} {1} deg'.format(
deg(lat_EB), deg(long_EB)))
assert_array_almost_equal(deg(lat_EB), 79.99154867)
assert_array_almost_equal(deg(long_EB), -90.01769837)
azimuth1 = n_EA_E_and_n_EB_E2azimuth(n_EA_E, n_EB_E, a=r_Earth, f=0)
assert_array_almost_equal(azimuth, azimuth1 + 2 * np.pi)
def plot_mean_position():
positions = np.array([(90, 0),
(60, 10),
(50, -20),
])
lats, lons = positions.T
nvecs = lat_lon2n_E(rad(lats), rad(lons))
# Find the horizontal mean position:
n_EM_E = unit(np.sum(nvecs, axis=1).reshape((3, 1)))
lat, lon = n_E2lat_lon(n_EM_E)
lat, lon = deg(lat), deg(lon)
print('Ex7, Average lat={0}, lon={1}'.format(lat, lon))
map1 = Basemap(projection='ortho', lat_0=int(lat), lon_0=int(lon),
resolution='l')
plot_world(map1)
x, y = map1(lon, lat)
map1.scatter(x, y, linewidth=5, marker='o', color='r')
x1, y1 = map1(lons, lats)
print(len(lons), x1, y1)
map1.scatter(x1, y1, linewidth=5, marker='o', color='k')
plt.title('Figure of mean position (red dot) compared to positions '
'A, B, and C (black dots).')
def plot_mean_position():
"""
Example
-------
>>> plot_mean_position()
Ex7, Average lat=67.2, lon=-6.9
>>> plt.show() # doctest: +SKIP
>>> plt.close()
"""
positions = np.array([
(90, 0),
(60, 10),
(50, -20),
])
lats, lons = np.transpose(positions)
nvecs = lat_lon2n_E(rad(lats), rad(lons))
# Find the horizontal mean position:
n_EM_E = unit(np.sum(nvecs, axis=1).reshape((3, 1)))
lat, lon = n_E2lat_lon(n_EM_E)
lat, lon = deg(lat), deg(lon)
print('Ex7, Average lat={0:2.1f}, lon={1:2.1f}'.format(lat[0], lon[0]))
plotter = _init_plotter(lat, lon)
plotter(lon, lat, linewidth=5, marker='o', color='r')
plotter(lons, lats, linewidth=5, marker='o', color='k')
plt.title('Figure of mean position (red dot) compared to \npositions '
'A, B, and C (black dots).')
def plot_mean_position():
"""
Example
-------
>>> plot_mean_position()
Ex7, Average lat=[ 67.23615295], lon=[-6.91751117]
"""
positions = np.array([
(90, 0),
(60, 10),
(50, -20),
])
lats, lons = positions.T
nvecs = lat_lon2n_E(rad(lats), rad(lons))
# Find the horizontal mean position:
n_EM_E = unit(np.sum(nvecs, axis=1).reshape((3, 1)))
lat, lon = n_E2lat_lon(n_EM_E)
lat, lon = deg(lat), deg(lon)
print(('Ex7, Average lat={0}, lon={1}'.format(lat, lon)))
map1 = Basemap(projection='ortho',
lat_0=int(lat),
lon_0=int(lon),
resolution='l')
plot_world(map1)
x, y = map1(lon, lat)
map1.scatter(x, y, linewidth=5, marker='o', color='r')
x1, y1 = map1(lons, lats)
# print(len(lons), x1, y1)
map1.scatter(x1, y1, linewidth=5, marker='o', color='k')
plt.title('Figure of mean position (red dot) compared to positions '
'A, B, and C (black dots).')
def test_Ex8_position_A_and_azimuth_and_distance_to_B():
# Position A is given as n_EA_E:
# Enter elements as lat/long in deg:
lat, lon = rad(80), rad(-90)
n_EA_E = lat_lon2n_E(lat, lon)
# The initial azimuth and great circle distance (s_AB), and Earth
# radius (r_Earth) are also given:
azimuth = rad(200)
s_AB = 1000 # m
r_Earth = 6371e3 # m, mean Earth radius
# Find the destination point B, as n_EB_E ("The direct/first geodetic
# problem" for a sphere)
# SOLUTION:
# Step1: Convert distance in meter into distance in [rad]:
distance_rad = s_AB / r_Earth
# Step2: Find n_EB_E:
n_EB_E = n_EA_E_distance_and_azimuth2n_EB_E(n_EA_E, distance_rad,
azimuth)
# When displaying the resulting position for humans, it is more
# convenient to see lat, long:
lat_EB, long_EB = n_E2lat_lon(n_EB_E)
print('Ex8, Destination: lat, long = {0} {1} deg'.format(deg(lat_EB),
deg(long_EB)))
assert_array_almost_equal(deg(lat_EB), 79.99154867)
assert_array_almost_equal(deg(long_EB), -90.01769837)
azimuth1 = n_EA_E_and_n_EB_E2azimuth(n_EA_E, n_EB_E, a=r_Earth, f=0)
assert_array_almost_equal(azimuth, azimuth1+2*np.pi)
def to_nvector(self):
lat = self.get_latitude(as_rad=True)
lon = self.get_longitude(as_rad=True)
alt = self.get_altitude()
n_EB_E = nv.lat_lon2n_E(lat, lon)
x, y, z = n_EB_E.ravel()
return Nvector(x, y, z, -alt)
def test_Ex5_great_circle_distance():
# Position A and B are given as n_EA_E and n_EB_E:
# Enter elements as lat/long in deg:
n_EA_E = lat_lon2n_E(rad(88), rad(0))
n_EB_E = lat_lon2n_E(rad(89), rad(-170))
r_Earth = 6371e3 # m, mean Earth radius
# SOLUTION:
s_AB = great_circle_distance(n_EA_E, n_EB_E, radius=r_Earth)
d_AB = euclidean_distance(n_EA_E, n_EB_E, radius=r_Earth)
msg = 'Ex5, Great circle distance = {} km, Euclidean distance = {} km'
print(msg.format(s_AB / 1000, d_AB / 1000))
assert_array_almost_equal(s_AB / 1000, 332.45644411)
assert_array_almost_equal(d_AB / 1000, 332.41872486)
def test_Ex5_great_circle_distance():
# Position A and B are given as n_EA_E and n_EB_E:
# Enter elements as lat/long in deg:
n_EA_E = lat_lon2n_E(rad(88), rad(0))
n_EB_E = lat_lon2n_E(rad(89), rad(-170))
r_Earth = 6371e3 # m, mean Earth radius
# SOLUTION:
s_AB = great_circle_distance(n_EA_E, n_EB_E, radius=r_Earth)
d_AB = euclidean_distance(n_EA_E, n_EB_E, radius=r_Earth)
msg = 'Ex5, Great circle distance = {} km, Euclidean distance = {} km'
print(msg.format(s_AB / 1000, d_AB / 1000))
assert_array_almost_equal(s_AB / 1000, 332.45644411)
assert_array_almost_equal(d_AB / 1000, 332.41872486)
def test_Ex1_A_and_B_to_delta_in_frame_N():
# Positions A and B are given in (decimal) degrees and depths:
lat_EA, lon_EA, z_EA = rad(1), rad(2), 3
lat_EB, lon_EB, z_EB = rad(4), rad(5), 6
# Find the exact vector between the two positions, given in meters
# north, east, and down, i.e. find p_AB_N.
# SOLUTION:
# Step1: Convert to n-vectors (rad() converts to radians):
n_EA_E = lat_lon2n_E(lat_EA, lon_EA)
n_EB_E = lat_lon2n_E(lat_EB, lon_EB)
# Step2: Find p_AB_E (delta decomposed in E).
# WGS-84 ellipsoid is default:
p_AB_E = n_EA_E_and_n_EB_E2p_AB_E(n_EA_E, n_EB_E, z_EA, z_EB)
# Step3: Find R_EN for position A:
R_EN = n_E2R_EN(n_EA_E)
# Step4: Find p_AB_N
p_AB_N = np.dot(R_EN.T, p_AB_E)
# (Note the transpose of R_EN: The "closest-rule" says that when
# decomposing, the frame in the subscript of the rotation matrix that
# is closest to the vector, should equal the frame where the vector is
# decomposed. Thus the calculation np.dot(R_NE, p_AB_E) is correct,
# since the vector is decomposed in E, and E is closest to the vector.
# In the example we only had R_EN, and thus we must transpose it:
# R_EN'=R_NE)
# Step5: Also find the direction (azimuth) to B, relative to north:
azimuth = np.arctan2(p_AB_N[1], p_AB_N[0])
# positive angle about down-axis
print('Ex1, delta north, east, down = {0}, {1}, {2}'.format(p_AB_N[0],
p_AB_N[1],
p_AB_N[2]))
print('Ex1, azimuth = {0} deg'.format(deg(azimuth)))
assert_array_almost_equal(p_AB_N[0], 331730.23478089)
assert_array_almost_equal(p_AB_N[1], 332997.87498927)
assert_array_almost_equal(p_AB_N[2], 17404.27136194)
assert_array_almost_equal(deg(azimuth), 45.10926324)
def test_Ex1_A_and_B_to_delta_in_frame_N():
# Positions A and B are given in (decimal) degrees and depths:
lat_EA, lon_EA, z_EA = rad(1), rad(2), 3
lat_EB, lon_EB, z_EB = rad(4), rad(5), 6
# Find the exact vector between the two positions, given in meters
# north, east, and down, i.e. find p_AB_N.
# SOLUTION:
# Step1: Convert to n-vectors (rad() converts to radians):
n_EA_E = lat_lon2n_E(lat_EA, lon_EA)
n_EB_E = lat_lon2n_E(lat_EB, lon_EB)
# Step2: Find p_AB_E (delta decomposed in E).
# WGS-84 ellipsoid is default:
p_AB_E = n_EA_E_and_n_EB_E2p_AB_E(n_EA_E, n_EB_E, z_EA, z_EB)
# Step3: Find R_EN for position A:
R_EN = n_E2R_EN(n_EA_E)
# Step4: Find p_AB_N
p_AB_N = np.dot(R_EN.T, p_AB_E)
# (Note the transpose of R_EN: The "closest-rule" says that when
# decomposing, the frame in the subscript of the rotation matrix that
# is closest to the vector, should equal the frame where the vector is
# decomposed. Thus the calculation np.dot(R_NE, p_AB_E) is correct,
# since the vector is decomposed in E, and E is closest to the vector.
# In the example we only had R_EN, and thus we must transpose it:
# R_EN'=R_NE)
# Step5: Also find the direction (azimuth) to B, relative to north:
azimuth = np.arctan2(p_AB_N[1], p_AB_N[0])
# positive angle about down-axis
print('Ex1, delta north, east, down = {0}, {1}, {2}'.format(
p_AB_N[0], p_AB_N[1], p_AB_N[2]))
print('Ex1, azimuth = {0} deg'.format(deg(azimuth)))
assert_array_almost_equal(p_AB_N[0], 331730.23478089)
assert_array_almost_equal(p_AB_N[1], 332997.87498927)
assert_array_almost_equal(p_AB_N[2], 17404.27136194)
assert_array_almost_equal(deg(azimuth), 45.10926324)
def test_Ex7_mean_position():
# Three positions A, B and C are given:
# Enter elements as lat/long in deg:
n_EA_E = lat_lon2n_E(rad(90), rad(0))
n_EB_E = lat_lon2n_E(rad(60), rad(10))
n_EC_E = lat_lon2n_E(rad(50), rad(-20))
# Find the horizontal mean position:
n_EM_E = unit(n_EA_E + n_EB_E + n_EC_E)
# The result is best viewed with a figure that shows the n-vectors
# relative to an Earth-model:
print('Ex7, See figure')
# plot_Earth_figure(n_EA_E,n_EB_E,n_EC_E,n_EM_E)
assert_array_almost_equal(n_EM_E.ravel(),
[0.384117, -0.046602, 0.922107])
# Alternatively:
n_EM_E = mean_horizontal_position(np.hstack((n_EA_E, n_EB_E, n_EC_E)))
assert_array_almost_equal(n_EM_E.ravel(),
[0.384117, -0.046602, 0.922107])
def test_Ex7_mean_position():
# Three positions A, B and C are given:
# Enter elements as lat/long in deg:
n_EA_E = lat_lon2n_E(rad(90), rad(0))
n_EB_E = lat_lon2n_E(rad(60), rad(10))
n_EC_E = lat_lon2n_E(rad(50), rad(-20))
# Find the horizontal mean position:
n_EM_E = unit(n_EA_E + n_EB_E + n_EC_E)
# The result is best viewed with a figure that shows the n-vectors
# relative to an Earth-model:
print('Ex7, See figure')
# plot_Earth_figure(n_EA_E,n_EB_E,n_EC_E,n_EM_E)
assert_array_almost_equal(n_EM_E.ravel(),
[0.384117, -0.046602, 0.922107])
# Alternatively:
n_EM_E = mean_horizontal_position(np.hstack((n_EA_E, n_EB_E, n_EC_E)))
assert_array_almost_equal(n_EM_E.ravel(),
[0.384117, -0.046602, 0.922107])
def test_small_and_large_cross_track_distance(self):
radius = 6371e3 # m, mean Earth radius
n_EA1_E = lat_lon2n_E(rad(5), rad(10))
n_EA2_E = lat_lon2n_E(rad(10), rad(10))
n_EB0_E = lat_lon2n_E(rad(7), rad(10.1))
path = (n_EA1_E, n_EA2_E)
n_EB1_E = closest_point_on_great_circle(path, n_EB0_E)
for s_xt0 in [np.pi / 3 * radius, 10., 0.1, 1e-4, 1e-8]:
distance_rad = s_xt0 / radius
n_EB_E = n_EA_E_distance_and_azimuth2n_EB_E(
n_EB1_E, distance_rad, np.pi / 2)
n_EB2_E = closest_point_on_great_circle(path, n_EB_E)
s_xt = great_circle_distance(n_EB1_E, n_EB_E, radius)
c_E = unit(np.cross(n_EA1_E, n_EA2_E, axis=0))
s_xt2 = (np.arccos(np.dot(c_E.T, n_EB_E)) - np.pi / 2) * radius
s_xt3 = cross_track_distance(path,
n_EB_E,
method='greatcircle',
radius=radius)
s_xt4 = np.arctan2(
-np.dot(c_E.T, n_EB_E),
np.linalg.norm(np.cross(c_E, n_EB_E, axis=0), axis=0)) * radius
assert_array_almost_equal(n_EB2_E, n_EB1_E)
assert_array_almost_equal(s_xt, s_xt0)
assert_array_almost_equal(s_xt2, s_xt0)
assert_array_almost_equal(s_xt3, s_xt0)
assert_array_almost_equal(s_xt4, s_xt0)
rtol = 10**(-min(9 + np.log10(s_xt0), 15))
self.assertTrue(np.abs(s_xt - s_xt0) / s_xt0 < rtol, 's_xt fails')
self.assertTrue(
np.abs(s_xt2 - s_xt0) / s_xt0 < rtol, 's_xt2 fails')
self.assertTrue(
np.abs(s_xt3 - s_xt0) / s_xt0 < rtol, 's_xt3 fails')
self.assertTrue(
np.abs(s_xt4 - s_xt0) / s_xt0 < rtol, 's_xt4 fails')
def setNed(self, current, target):
lat_C, lon_C = rad(current.lat), rad(current.lon)
lat_T, lon_T = rad(target.lat), rad(target.lon)
# create an n-vector for current and target
nvecC = nv.lat_lon2n_E(lat_C, lon_C)
nvecT = nv.lat_lon2n_E(lat_T, lon_T)
# create a p-vec from C to T in the Earth's frame
# the zeros are for the depth (depth = -1 * altitude)
p_CT_E = nv.n_EA_E_and_n_EB_E2p_AB_E(nvecC, nvecT, 0, 0)
# create a rotation matrix
# this rotates points from the NED frame to the Earth's frame
R_EN = nv.n_E2R_EN(nvecC)
# rotate p_CT_E so it lines up with current's NED frame
# we use the transpose so we can go from the Earth's frame to the NED frame
n, e, d = np.dot(R_EN.T, p_CT_E).ravel()
#Scale Nedvalues
if n > e:
scaleFactor = abs(1.00000 / n)
else:
scaleFactor = abs(1.00000 / e)
return Nedvalues(n * scaleFactor, e * scaleFactor, d)
def test_Ex4_geodetic_latitude_to_ECEF_vector():
# Position B is given with lat, long and height:
lat_EB_deg = 1
long_EB_deg = 2
h_EB = 3
# Find the vector p_EB_E ("ECEF-vector")
# SOLUTION:
# Step1: Convert to n-vector:
n_EB_E = lat_lon2n_E(rad(lat_EB_deg), rad(long_EB_deg))
# Step2: Find the ECEF-vector p_EB_E:
p_EB_E = n_EB_E2p_EB_E(n_EB_E, -h_EB)
print('Ex4: p_EB_E = {0} m'.format(p_EB_E.ravel()))
assert_array_almost_equal(p_EB_E.ravel(),
[6373290.27721828, 222560.20067474,
110568.82718179])
def test_Ex4_geodetic_latitude_to_ECEF_vector():
# Position B is given with lat, long and height:
lat_EB_deg = 1
long_EB_deg = 2
h_EB = 3
# Find the vector p_EB_E ("ECEF-vector")
# SOLUTION:
# Step1: Convert to n-vector:
n_EB_E = lat_lon2n_E(rad(lat_EB_deg), rad(long_EB_deg))
# Step2: Find the ECEF-vector p_EB_E:
p_EB_E = n_EB_E2p_EB_E(n_EB_E, -h_EB)
print('Ex4: p_EB_E = {0} m'.format(p_EB_E.ravel()))
assert_array_almost_equal(
p_EB_E.ravel(),
[6373290.27721828, 222560.20067474, 110568.82718179])
def botPost():
positions = list()
try:
users_data = request.json['usersLocationList']
except:
return 'Ups, algo salió mal'
if (len(users_data) <= 1):
return 'Ups, parece que estás solo'
else:
for pos in users_data:
positions.append(
nv.lat_lon2n_E(radians(float(pos.get('lat'))),
radians(float(pos.get('lon')))))
lat, lon = getMiddlePointFromList(positions)
#location = getLocationName(lat,lon)
bars = getPatagoniaNearbyBars(lat, lon)
text = 'Encontrémonos en _{0}_ ({1}) a disfrutar una rica *Cerveza Patagonia*. ¡Nos queda cómodo a todos!'.format(
bars[0]['name'], bars[0]['url'])
logger.debug('botPost: %s', text)
geoJsonData = createJs(users_data, {'lat': lat, 'lon': lon}, bars[0])
db_cur.execute(
"INSERT INTO usrQuery(dateQuery,jsonQuery,jsonResp,groupSize,barName) VALUES (?,?,?,?,?)",
[
str(datetime.now()),
str(users_data),
str(geoJsonData),
len(users_data), bars[0]['name']
])
db_conn.commit()
return text
def nv(self):
if self._nv is None:
self._nv = lat_lon2n_E(deg2rad(self.lat), deg2rad(self.lng))
return self._nv
def pvec_b_to_lla(forward, right, down, roll, pitch, yaw, lat, lon, alt):
"""
returns the lat lon and alt corresponding to a p-vec in the UAV's body frame
Parameters
----------
forward: float
The number of meters forward of the UAV
right: float
The number of meters to the right of the UAV
down: float
The number of meters below the UAV
roll: float
The UAV's roll angle in degrees
pitch: float
The UAV's pitch angle in degrees
yaw: float
The UAV's yaw angle in degrees
lat: float
The UAV's latitude in degrees
lon: float
The UAV's longitude in degrees
alt: float
The UAV's altitude in meters
Returns
-------
list
This list holds three floats representing the latitude in degrees, longitude in degrees and altitude in meters (in that order).
"""
# create a p-vector with the forward, right and down values
p_B = np.array([forward, right, down])
# this matrix can transform a pvec in the body frame to a pvec in the NED frame
rot_NB = nv.zyx2R(radians(yaw), radians(pitch), radians(roll))
# calculate the pvec in the NED frame
p_N = rot_NB.dot(p_B)
# create an n-vector for the UAV
n_UAV = nv.lat_lon2n_E(radians(lat), radians(lon))
# this creates a matrix that rotates pvecs from NED to ECEF
rot_EN = nv.n_E2R_EN(n_UAV)
# find the offset vector from the UAV to the point of interest in the ECEF frame
p_delta_E = rot_EN.dot(p_N)
# find the p-vector for the UAV in the ECEF frame
p_EUAV_E = nv.n_EB_E2p_EB_E(n_UAV, -alt).reshape(1, 3)[0]
# find the p-vector for the point of interest. This is the UAV + the offset in the ECEF frame.
p_E = p_EUAV_E + p_delta_E
# find the n-vector for the point of interest given the p-vector in the ECEF frame.
n_result, z_result = nv.p_EB_E2n_EB_E(p_E.reshape(3, 1))
# convert the n-vector to a lat and lon
lat_result, lon_result = nv.n_E2lat_lon(n_result)
lat_result, lon_result = degrees(lat_result), degrees(lon_result)
# convert depth to alt
alt_result = -z_result[0]
return [lat_result, lon_result, alt_result]
