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From U.S. Dynamics Corporation
The gyroscope is an instrument where the input is a rate of turn (angular rate). Any gyroscope is a torque-in, torque-out device. Therefore, the output of the gyro is a change in the gimbal angle (the gimbal turns) in response to the rate of turn input, due to gyroscopic precession. The input is a turn about the input axis (IA). The output is a turn about the output axis (OA). The precession of the gimbal takes place only when the rotor is spinning, of course. Conversely, a rotation imparted to the gimbal in its freedom axis (the OA), will cause a torque about the input axis (IA). Gyroscopes, therefore, will only provide an output response to a turn or spinning (angular) input motion, and will not respond to a linear input. Figure 1 depicts a RIG in simplistic form. It is what is known as a single degree of freedom type gyroscope. If the case is firmly tied to a structure, the freedom is in the output axis (OA), as the gimbal rolls in response to an input. Product Announcements
Topics of Interest
This applications note discusses the input signal excitation and output signal conditioning (demodulation) requirements of the transformer type output generator, or pickoff used on the US Dynamics...
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Spinning mass gyroscopes use a steadily-moving mass with a free-moving axis (gimbal). They are very fragile and require regular maintenance. When a spinning mass gyro is tilted, the gyroscopic effect...
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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.
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9.4.4 Gimbal Attitude Implementations
The primary function of gimbals is to isolate the ISA from vehicle rotations, but they are also used for other INS functions.
9.4.4.1 Accelerometer Recalibration...
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9.1.6 Vibratory Coriolis Gyroscopes (VCGs)
9.1.6.1 VCG Principles The first functional vibrational coriolis gyroscope was probably the 1851 Foucault pendulum, in which the coriolis effect from the...
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