How positions are described: where the origin is, how the axes point, and what kind of coordinates are used. See also ENAE 441: Reference Frames.

Defining a Coordinate System

  1. Center: location of the origin
    1. Center of the Earth / gravitation (orbit center)
    2. Observation site on the surface
    3. A satellite
  2. Orientation: principal (first) axis, polar (third) axis
    1. For Earth-centered: the polar axis is the north pole axis
    2. For orbit-centered (perifocal): angular momentum
    3. Satellite-centered: angular momentum
  3. Type: Cartesian, polar
    1. Cylindrical
    2. Spherical
    3. Distance

Spherical and Cartesian Coordinates

  • Spherical to Cartesian (Matlab sph2cart, AstroPy spherical_to_cartesian):
    • [𝑥𝑦𝑧]=[𝑟cos𝜑cos𝜃𝑟cos𝜑sin𝜃𝑟sin𝜑]
  • Cartesian to spherical (Matlab cart2sph, AstroPy cartesian_to_spherical):
    • 𝑟=√𝑥2+𝑦2+𝑧2𝜃=arctan(𝑦,𝑥)𝜑=arctan(𝑧,√𝑥2+𝑦2)
    • with the two-argument arctangent
    • 𝜃: azimuthal angle in the equatorial plane; 𝜑: elevation above it

Earth-Centered Frames

  • Curtis Fig 1.18: Earth-centered inertial frame (𝑋𝑌𝑍) and an Earth-centered noninertial 𝑥′𝑦′𝑧′ frame embedded in and rotating with the Earth
    • 𝑋 along the vernal equinox direction, 𝑍 along the spin axis
    • 𝑥′ through the Greenwich meridian; a surface point 𝑃 is located by east longitude and north latitude 𝜑, with a local East / North / Zenith frame drawn at 𝑃
  • Two Earth-centered reference frames:
    1. Inertial: principal axis is fixed to the vernal equinox
    2. Rotating (body fixed): principal axis points to the prime meridian
  • Celestial sphere (directions in space) vs Earth sphere (points on the ground)

Geocentric Equatorial Frame

  • Curtis sec. 4.2
  • Geocentric equatorial (̂𝐈,̂𝐉,̂𝐊), also called ECI:
    • ̂𝐈 = principal axis, points to the vernal equinox
    • ̂𝐊 = polar axis
    • Equinox, or ascending node (where the Sun crosses the equator going north)
  • Polar angles:
    • Right ascension 𝛼
    • Declination 𝛿
  • The axes slowly move because of the precession of the equinoxes, nutation, and polar motion (see Precision Reference Frames)

Earth-Centered Earth-Fixed Frame

  • ECEF: rotates with the Earth
  • Polar angles:
    • Longitude 𝜆
    • Latitude 𝜑

Transformation Between ECI and ECEF

  • Sketch: in the equatorial plane, the prime meridian is at angle 𝜃𝐺 from ̂𝐈, and a local meridian is a further 𝜆 (east longitude) beyond it
  • 𝜃𝐺: right ascension of the prime meridian = Greenwich sidereal time (GST)
  • 𝜃𝐿: right ascension of the local meridian = local sidereal time
    • 𝜃𝐿=𝜃𝐺+𝜆
  • Transform by rotating between the two frames (about the common polar axis by 𝜃𝐺)
  • 𝜃𝐺 as a function of time: Sidereal Time

Lunar Coordinate Frames

  • Earth and lunar axes, equatorial planes, lunar orbit plane and ecliptic, with their angles (from Dr. Healy's notes)
    • Earth obliquity 23.44°; lunar orbital inclination to the ecliptic 5.14°
    • Lunar obliquity 6.68° (to its orbit plane), 1.54° to the ecliptic
  • Non-rotating frame: principal axis defined by the cross product of the Earth’s mean rotational pole of J2000 with the Moon’s rotational north pole
  • Rotating frames:
    • PA: principal axis frame, based on the Moon’s moments of inertia
    • ME: mean Earth (older)