A two-axis integrated gyro accelerometer and servo control method
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- BEIJING INST OF AEROSPACE CONTROL DEVICES
- Publication Date
- 2020-11-10
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Abstract
Description
technical field
[0001] The invention relates to a two-axis gyro accelerometer and a servo control method, in particular to an accelerometer for an inertial stable platform, which belongs to the field of aviation and aerospace for high-precision apparent acceleration measurement. Background technique
[0002] In high-precision inertial stabilization platforms, quartz flexible accelerometers and pendulum integrating gyro accelerometers are mainly used at present, both of which are single-degree-of-freedom accelerometers, and each accelerometer is sensitive to apparent acceleration in one direction.
[0003] Taking the Pendulum Integral Gyro Accelerometer (PIGA) as an example, it is a pendulum accelerometer that uses gyro torque for feedback. Its working principle is shown in the figure below. In the figure, OX 1 Y 1 Z 1 is the coordinate system fixed to the frame, OX 1 is the input axis; Oxyz is the Ley difference coordinate system, and the Oz axis coincides with the rotor...