From Global Positioning Systems, Inertial Navigation, and Integration

9.1.2 Early Accelerometers

Pendulum clocks were used in the eighteen century for measuring the acceleration due to gravity, but these devices were not usable on moving platforms. Drag Cup Accelerometer An early "integrating" accelerometer design is illustrated in Fig. 9.4. It has two independent moving parts, both able to rotate on a common shaft axis:

  1. A bar magnetic, the rotation rate of which is controlled by a dc motor.
  2. A nonferrous metal "drag cup" that will be dragged along by the currents
    induced in the metal by the moving magnetic field, producing a torque on
    the drag cup that is proportional to the magnet rotation rate. The drag cup
    also has a proof mass attached to one point, so that acceleration along the
    "input axis" direction shown in the illustration will also create a torque on
    the drag cup.

The DC current to the motor is servoed to keep the drag cup from rotating, so that the magnet rotation rate will be proportional to acceleration and each rotation of the magnet will be proportional to the resulting velocity increment over that time period. At very low input accelerations (e.g., during gimbaled IMU leveling), inhomogeneities in the drag cup material...

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Satellite communications equipment is used for the transmission, conditioning, and reception of satellite signals in worldwide telecommunications.
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GPS chips and modules compare signals from several geo-positioning satellites to determine position on the Earth's surface. GPS is an initialism for global positioning system.

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Inertial sensors are semiconductor devices used to measure acceleration, changes in inclination, and gyration.

Topics of Interest

9.1.3 Feedback Control Technology Feedback Control Practical inertial navigation began to evolve in the 1950s, using technologies that had evolved in the early twentieth century, or were...

9.1.4 Rotating Coriolis Multisensors Coriolis Effect Gustav Gaspard de Coriolis (1792-1843) published a report in 1835 [39] describing the effects of coordinate rotation on Newton s laws of...

9.3.3 Other Calibration Parameters Nonlinearities Sensor input/output nonlinearities are generally modeled by polynomials: where the first two parameters a0 = bias and a1 = scale factor. The...

9.1.7 MEMS Technology Microelectromechanical systems (MEMS) evolved from silicon semiconductor manufacturing in the late 1970s as an inexpensive mass manufacturing technology for sensors at...

9.1.6 Vibratory Coriolis Gyroscopes (VCGs) VCG Principles The first functional vibrational coriolis gyroscope was probably the 1851 Foucault pendulum, in which the coriolis effect from the...