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Chapters
Excerpts of 'Avionics for Pilots & Engineers' This HTML formatting you are viewing is not fully accurate and not representative of the actual book format. |
COORDINATE SYSTEMS FOR NAVIGATION
Earth was born in a molten state. While cooling, it bulged out due to its rotation and its surface settled in a way that it approximately represented points of equal gravitation. The earth has finally taken the shape of an ellipsoid with an uneven surface. Surface of seawaters, however does contains points of equal gravitation more precisely, ignoring tidal disturbances and water flows. This surface can be theoretically extended under landmasses to form an enclosed surface, which is known as Geoid. The Geoid is again not a precise ellipsoid in mathematical terms. For navigational computations a perfect ellipsoid is assumed with following qualifications:
See Fig. 2. Due to rotation of the earth (at 15.041067 degrees per hour), a body at a point P experiences a centrifugal force away from the axis of rotation. Thus, the apparent gravity is not only due to the mass of the earth, but a resultant (gl) of the actual gravitation (g) and the acceleration acf due to centrifugal force given by: acf = wiex(wiexR) = |w2ie Rcosf|Ucf (1) where Ucf is unit vector in direction of centrifugal force.
gl represents local gravitation, which is a vertical line as seen with a plumb line. We can see that acf is maximum in equatorial plane and approaches zero at the poles. It is always directed along radial from axis of rotation and parallel to equatorial plane. This direction is shown by unit vector Ucf as shown in the above figure. Its magnitude as you can find from Equation (1) above, is proportional to cosf, wheref is latitude of the point P under consideration. We define three types of latitude angles. · Geocentric latitude: fc made by line PO · Geodetic latitude: fT made by line PCBA; this line is normal to the ellipsoid. · Astronomical latitude: fA made by line PD Note: The centrifugal force plays important role in function of accelerometers in inertial navigation.............
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