Foundations of Space Dynamics. Ashish Tewari

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coupled, such as when the rigid body experiences an appreciable gravity‐gradient torque during its orbit. Furthermore, when designing an attitude control system for a spacecraft, it is necessary to account for its orbital motion. Therefore, while elements of orbital mechanics and attitude dynamics can be grasped separately, their practical application involves a combined approach.

      Space flight requires a definite background of objects to measure distances, as well as to orient the spacecraft in specific directions. Since fixed objects are hard to come by in practice, navigation and attitude determination are non‐trivial problems in space flight. Such a problem does not exist for the motion taking place on, or very close to, a solid surface, where ground‐fixed objects can serve as useful references for both navigation and orientation of the vehicles.

Geometrical interpretation of the equinoctial sidereal frame (I, J, K), the ecliptic synodic frame (i, j, k), and Earth centred celestial meridian.

       1.2.1 Sidereal Frame

      The rate of rotation of Earth on its own axis (normal to the equatorial plane) is from the west to the east, and can be measured in a sidereal reference frame oriented with the vernal equinox direction. This rate is called the sidereal rotation rate, and would be the true rotation rate of Earth if the vernal equinox were a constant direction. A sidereal day is the period of rotation of Earth measured from the vernal equinox. If the sun is used for timing the rotational rate of Earth, the period from noon to noon is a mean solar day (m.s.d.) of 24‐hour duration. However, the mean solar day is not the true rotational rate of Earth because of Earth's orbit around the sun, which also takes place from the west to the east. To calculate the sidereal day from the mean solar day, a correction must be applied by adding the average rate at which Earth orbits the sun. The tropical year is the period of Earth's orbit around the sun measured from one vernal equinox to the next, and equals 365.242 mean solar days. This implies that the mean apparent sun is slightly less than one degree per day (images). Such a correction gives the sidereal day as the following:

      (1.3)equation

      or 23 hr., 56 min., 4.0904 s.

      Apart from the precession and the nutation of Earth's spin axis, there is also a precession of the ecliptic caused by the gravitational attraction of the other planets. This is a much smaller variation in the equinoxes (about 100 times smaller than that caused by luni‐solar attraction).

      Since the vernal equinox moves slightly westward every year, the

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