<reponame>c-bruce/pysamss
# Date: 06/01/2019
# Author: <NAME>
# Math helper functions
import numpy as np
from pyquaternion import Quaternion

def referenceFrames2rotationMatrix(referenceFrame1, referenceFrame2):
    """
    Rotation matrix for converting from referenceFrame1 to referenceFrame2.

    Args:
        referenceFrame1 (object): referenceFrame1 object.
        referenceFrame2 (object): referenceFrame2 object.

    Returns:
        R (np.array): Rotation matrix to convert from referenceFrame1 to
                      referenceFrame2.
    """
    i, j, k = referenceFrame1.getIJK()

    i_d, j_d, k_d = referenceFrame2.getIJK()

    R = np.array([[np.dot(i,i_d), np.dot(j,i_d), np.dot(k,i_d)],
                  [np.dot(i,j_d), np.dot(j,j_d), np.dot(k,j_d)],
                  [np.dot(i,k_d), np.dot(j,k_d), np.dot(k,k_d)]])
    return R

def euler2rotationMatrix(euler):
    """
    Get rotation matrix defined by phi, theta, psi.

    Args:
        euler (list/np.array): Euler angles to convert.

    Returns:
        R (np.array): Rotation matrix representation of Euler angles.
    """
    phi = euler[0]
    theta = euler[1]
    psi = euler[2]
    Rx = np.array([[1, 0, 0],
                   [0, np.cos(phi), -np.sin(phi)],
                   [0, np.sin(phi), np.cos(phi)]])

    Ry = np.array([[np.cos(theta), 0, np.sin(theta)],
                   [0, 1, 0],
                   [-np.sin(theta), 0, np.cos(theta)]])

    Rz = np.array([[np.cos(psi), -np.sin(psi), 0],
                   [np.sin(psi), np.cos(psi), 0],
                   [0, 0, 1]])

    R = np.matmul(Rz, np.matmul(Ry, Rx))
    return R

def rotationMatrix2euler(R):
    """
    Get Euler angles representation of rotation matrix R.

    Args:
        R (np.array): Rotation matrix to convert.

    Returns:
        euler (np.array): Euler angles representation of rotation matrix.
    """
    quaternion = rotationMatrix2quaternion(R)
    euler = quaternion2euler(quaternion)
    return euler

def quaternion2rotationMatrix(quaternion):
    """
    Get rotation matrix representation of quaternion [w, x, y, z].

    Args:
        quaternion (list/np.array): Quaternion to convert.

    Returns:
        R (np.array): Rotation matrix representation of quaternion.
    """
    w = quaternion[0]
    x = quaternion[1]
    y = quaternion[2]
    z = quaternion[3]
    R = np.array([[w**2 + x**2 - y**2 - z**2, (2*x*y) - (2*w*z), (2*x*z) + (2*w*y)],
                  [(2*x*y) + (2*w*z), w**2 - x**2 + y**2 - z**2, (2*y*z) + (2*w*x)],
                  [(2*x*z) - (2*w*y), (2*y*z) + (2*w*x), w**2 - x**2 - y**2 + z**2]])
    return R

def rotationMatrix2quaternion(R):
    """
    Get quaternion representation of rotation matrix R.

    Args:
        R (np.array): Rotation matrix to convert.

    Returns:
        quaternion (np.array): Quaternion representation of R.
    """
    w = 0.5 * np.sqrt(R[0,0]**2 + R[1,1]**2 + R[2,2]**2 + 1)
    x = (R[1,2] - R[2,1]) / (4 * w)
    y = (R[2,0] - R[0,2]) / (4 * w)
    z = (R[0,1] - R[1,0]) / (4 * w)
    quaternion = np.array([w, x, y, z])
    quaternion = Quaternion(quaternion)
    return quaternion

def euler2quaternion(euler):
    """
    Get quaternion representation of Euler angles phi, theta, psi.

    Args:
        euler (list/np.array): Euler angles to convert.

    Returns:
        quaternion (np.array): Quaternion representation of Euler angles.
    """
    phi = euler[0]
    theta = euler[1]
    psi = euler[2]
    q1 = Quaternion(axis=[1, 0, 0], angle=phi)
    q2 = Quaternion(axis=[0, 1, 0], angle=theta)
    q3 = Quaternion(axis=[0, 0, 1], angle=psi)
    quaternion = q3 * q2 * q1
    return quaternion

def quaternion2euler(quaternion):
    """
    Get Euler angles representation of quaternion [w, x, y, z].

    Args:
        quaternion (list/np.array): Quaternion to convert.

    Returns:
        euler (np.array): Euler angles representation of quaternion.
    """
    w = quaternion[0]
    x = quaternion[1]
    y = quaternion[2]
    z = quaternion[3]
    phi = np.arctan2(2 * ((w * x) + (y * z)), 1 - 2 * (x**2 + y**2))
    theta = np.arcsin(2 * ((w * y) - (z * x)))
    psi = np.arctan2(2 * ((w * z) + (x * y)), 1 - 2 * (y**2 + z**2))
    euler = np.array([phi, theta, psi])
    return euler

def heading2vector(heading):
    """
    Get vector representation of heading.

    Args:
        heading (list): Heading [direction, pitch] (rad).

    Returns:
        vector (np.array): Unit vector representation of heading.
    """
    direction = heading[0]
    pitch = heading[1]
    R = euler2rotationMatrix([0, pitch, direction])
    vector = np.dot(R, [1,0,0])
    return vector

def lonlatalt2cartesian(celestialbody, longitude, latitude, altitude):
    """
    Convert from longitude, latitude, altitude to x, y, z.

    Args:
        celestialbody (obj): CelestialBody object.
        longitude (double): Longitude (deg).
        latitude (double): Latitude (deg).
        altitude (double): Altitude above notional sea level (m).

    Returns:
        cartesian (list): Cartesian coordinates [x, y, z] (m).
    """
    R = celestialbody.getRadius() + altitude
    longitude = np.deg2rad(longitude)
    latitude = np.deg2rad(latitude)
    x = R * np.cos(latitude) * np.cos(longitude)
    y = R * np.cos(latitude) * np.sin(longitude)
    z = R * np.sin(latitude)
    cartesian = np.array([x, y, z])
    return cartesian

def cartesian2lonlatalt(celestialbody, cartesian):
    """
    Convert from x, y, z to longitude, latitude, altitude.

    Args:
        celestialbody (obj): CelestialBody object.
        cartesian (list): Cartesian coordinates [x, y, z] (m).

    Returns:
        longitude (double): Longitude (deg).
        latitude (double): Latitude (deg).
        altitude (double): Altitude above notional sea level (m).
    """
    x = cartesian[0]
    y = cartesian[1]
    z = cartesian[2]
    R = np.linalg.norm(cartesian)
    longitude = np.arcsin(z / R)
    longitude = np.rad2deg(longitude)
    latitude = np.arctan2(y, x)
    latitude = np.rad2deg(latitude)
    altitude = R - celestialbody.getRadius()
    return longitude, latitude, altitude

# Date: 06/01/2019
# Author: <NAME>
# Math helper functions
import numpy as np
from pyquaternion import Quaternion

def referenceFrames2rotationMatrix(referenceFrame1, referenceFrame2):
    """
    Rotation matrix for converting from referenceFrame1 to referenceFrame2.

    Args:
        referenceFrame1 (object): referenceFrame1 object.
        referenceFrame2 (object): referenceFrame2 object.

    Returns:
        R (np.array): Rotation matrix to convert from referenceFrame1 to
                      referenceFrame2.
    """
    i, j, k = referenceFrame1.getIJK()

    i_d, j_d, k_d = referenceFrame2.getIJK()

    R = np.array([[np.dot(i,i_d), np.dot(j,i_d), np.dot(k,i_d)],
                  [np.dot(i,j_d), np.dot(j,j_d), np.dot(k,j_d)],
                  [np.dot(i,k_d), np.dot(j,k_d), np.dot(k,k_d)]])
    return R

def euler2rotationMatrix(euler):
    """
    Get rotation matrix defined by phi, theta, psi.

    Args:
        euler (list/np.array): Euler angles to convert.

    Returns:
        R (np.array): Rotation matrix representation of Euler angles.
    """
    phi = euler[0]
    theta = euler[1]
    psi = euler[2]
    Rx = np.array([[1, 0, 0],
                   [0, np.cos(phi), -np.sin(phi)],
                   [0, np.sin(phi), np.cos(phi)]])

    Ry = np.array([[np.cos(theta), 0, np.sin(theta)],
                   [0, 1, 0],
                   [-np.sin(theta), 0, np.cos(theta)]])

    Rz = np.array([[np.cos(psi), -np.sin(psi), 0],
                   [np.sin(psi), np.cos(psi), 0],
                   [0, 0, 1]])

    R = np.matmul(Rz, np.matmul(Ry, Rx))
    return R

def rotationMatrix2euler(R):
    """
    Get Euler angles representation of rotation matrix R.

    Args:
        R (np.array): Rotation matrix to convert.

    Returns:
        euler (np.array): Euler angles representation of rotation matrix.
    """
    quaternion = rotationMatrix2quaternion(R)
    euler = quaternion2euler(quaternion)
    return euler

def quaternion2rotationMatrix(quaternion):
    """
    Get rotation matrix representation of quaternion [w, x, y, z].

    Args:
        quaternion (list/np.array): Quaternion to convert.

    Returns:
        R (np.array): Rotation matrix representation of quaternion.
    """
    w = quaternion[0]
    x = quaternion[1]
    y = quaternion[2]
    z = quaternion[3]
    R = np.array([[w**2 + x**2 - y**2 - z**2, (2*x*y) - (2*w*z), (2*x*z) + (2*w*y)],
                  [(2*x*y) + (2*w*z), w**2 - x**2 + y**2 - z**2, (2*y*z) + (2*w*x)],
                  [(2*x*z) - (2*w*y), (2*y*z) + (2*w*x), w**2 - x**2 - y**2 + z**2]])
    return R

def rotationMatrix2quaternion(R):
    """
    Get quaternion representation of rotation matrix R.

    Args:
        R (np.array): Rotation matrix to convert.

    Returns:
        quaternion (np.array): Quaternion representation of R.
    """
    w = 0.5 * np.sqrt(R[0,0]**2 + R[1,1]**2 + R[2,2]**2 + 1)
    x = (R[1,2] - R[2,1]) / (4 * w)
    y = (R[2,0] - R[0,2]) / (4 * w)
    z = (R[0,1] - R[1,0]) / (4 * w)
    quaternion = np.array([w, x, y, z])
    quaternion = Quaternion(quaternion)
    return quaternion

def euler2quaternion(euler):
    """
    Get quaternion representation of Euler angles phi, theta, psi.

    Args:
        euler (list/np.array): Euler angles to convert.

    Returns:
        quaternion (np.array): Quaternion representation of Euler angles.
    """
    phi = euler[0]
    theta = euler[1]
    psi = euler[2]
    q1 = Quaternion(axis=[1, 0, 0], angle=phi)
    q2 = Quaternion(axis=[0, 1, 0], angle=theta)
    q3 = Quaternion(axis=[0, 0, 1], angle=psi)
    quaternion = q3 * q2 * q1
    return quaternion

def quaternion2euler(quaternion):
    """
    Get Euler angles representation of quaternion [w, x, y, z].

    Args:
        quaternion (list/np.array): Quaternion to convert.

    Returns:
        euler (np.array): Euler angles representation of quaternion.
    """
    w = quaternion[0]
    x = quaternion[1]
    y = quaternion[2]
    z = quaternion[3]
    phi = np.arctan2(2 * ((w * x) + (y * z)), 1 - 2 * (x**2 + y**2))
    theta = np.arcsin(2 * ((w * y) - (z * x)))
    psi = np.arctan2(2 * ((w * z) + (x * y)), 1 - 2 * (y**2 + z**2))
    euler = np.array([phi, theta, psi])
    return euler

def heading2vector(heading):
    """
    Get vector representation of heading.

    Args:
        heading (list): Heading [direction, pitch] (rad).

    Returns:
        vector (np.array): Unit vector representation of heading.
    """
    direction = heading[0]
    pitch = heading[1]
    R = euler2rotationMatrix([0, pitch, direction])
    vector = np.dot(R, [1,0,0])
    return vector

def lonlatalt2cartesian(celestialbody, longitude, latitude, altitude):
    """
    Convert from longitude, latitude, altitude to x, y, z.

    Args:
        celestialbody (obj): CelestialBody object.
        longitude (double): Longitude (deg).
        latitude (double): Latitude (deg).
        altitude (double): Altitude above notional sea level (m).

    Returns:
        cartesian (list): Cartesian coordinates [x, y, z] (m).
    """
    R = celestialbody.getRadius() + altitude
    longitude = np.deg2rad(longitude)
    latitude = np.deg2rad(latitude)
    x = R * np.cos(latitude) * np.cos(longitude)
    y = R * np.cos(latitude) * np.sin(longitude)
    z = R * np.sin(latitude)
    cartesian = np.array([x, y, z])
    return cartesian

def cartesian2lonlatalt(celestialbody, cartesian):
    """
    Convert from x, y, z to longitude, latitude, altitude.

    Args:
        celestialbody (obj): CelestialBody object.
        cartesian (list): Cartesian coordinates [x, y, z] (m).

    Returns:
        longitude (double): Longitude (deg).
        latitude (double): Latitude (deg).
        altitude (double): Altitude above notional sea level (m).
    """
    x = cartesian[0]
    y = cartesian[1]
    z = cartesian[2]
    R = np.linalg.norm(cartesian)
    longitude = np.arcsin(z / R)
    longitude = np.rad2deg(longitude)
    latitude = np.arctan2(y, x)
    latitude = np.rad2deg(latitude)
    altitude = R - celestialbody.getRadius()
    return longitude, latitude, altitude
# Date: 06/01/2019 # Author: <NAME> # Math helper functions Rotation matrix for converting from referenceFrame1 to referenceFrame2.      Args:         referenceFrame1 (object): referenceFrame1 object.         referenceFrame2 (object): referenceFrame2 object.      Returns:         R (np.array): Rotation matrix to convert from referenceFrame1 to                       referenceFrame2. Get rotation matrix defined by phi, theta, psi.      Args:         euler (list/np.array): Euler angles to convert.      Returns:         R (np.array): Rotation matrix representation of Euler angles. Get Euler angles representation of rotation matrix R.      Args:         R (np.array): Rotation matrix to convert.      Returns:         euler (np.array): Euler angles representation of rotation matrix. Get rotation matrix representation of quaternion [w, x, y, z].      Args:         quaternion (list/np.array): Quaternion to convert.      Returns:         R (np.array): Rotation matrix representation of quaternion. Get quaternion representation of rotation matrix R.      Args:         R (np.array): Rotation matrix to convert.      Returns:         quaternion (np.array): Quaternion representation of R. Get quaternion representation of Euler angles phi, theta, psi.      Args:         euler (list/np.array): Euler angles to convert.      Returns:         quaternion (np.array): Quaternion representation of Euler angles. Get Euler angles representation of quaternion [w, x, y, z].      Args:         quaternion (list/np.array): Quaternion to convert.      Returns:         euler (np.array): Euler angles representation of quaternion. Get vector representation of heading.      Args:         heading (list): Heading [direction, pitch] (rad).      Returns:         vector (np.array): Unit vector representation of heading. Convert from longitude, latitude, altitude to x, y, z.      Args:         celestialbody (obj): CelestialBody object.         longitude (double): Longitude (deg).         latitude (double): Latitude (deg).         altitude (double): Altitude above notional sea level (m).      Returns:         cartesian (list): Cartesian coordinates [x, y, z] (m). Convert from x, y, z to longitude, latitude, altitude.      Args:         celestialbody (obj): CelestialBody object.         cartesian (list): Cartesian coordinates [x, y, z] (m).      Returns:         longitude (double): Longitude (deg).         latitude (double): Latitude (deg).         altitude (double): Altitude above notional sea level (m).