Method for calibrating zero offset of quartz flexible accelerometer component
An accelerometer, zero offset technology, applied in the testing/calibration of velocity/acceleration/shock measurement equipment, velocity/acceleration/shock measurement, navigation through velocity/acceleration measurement, etc. Many problems, such as poor real-time performance
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- Publication Date
- 2011-02-16
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention relates to a component calibration method, in particular to a calibration technology for the zero offset of a quartz flexible accelerometer assembly. Background technique
[0002] In the strapdown inertial navigation system, the accelerometer component is used as a sensor of the specific force acceleration of the sensitive carrier, and its accuracy directly affects the navigation accuracy of the strapdown inertial navigation system. The quartz flexible accelerometer has the advantages of simple structure and process, low cost and high reliability. Therefore, the quartz flexible accelerometer assembly composed of the quartz flexible accelerometer is widely used in the strapdown inertial navigation system.
[0003] Calibration technology is a method to improve the measurement accuracy of the quartz flexible accelerometer from the aspect of software. The accelerometer zero offset refers to the deviation from the zero point of the specific ...
Examples
Embodiment Construction
[0084] The present invention is described in more detail below in conjunction with accompanying drawing example:
[0085] The measurement method of the zero offset of the quartz flexible accelerometer assembly described in this embodiment, its specific implementation steps are as follows:
[0086] Step 1. Place the strapdown inertial navigation system equipped with quartz flexible accelerometer components on the three-axis position turntable. The axis of rotation of the frame is parallel. The strapdown inertial navigation system is preheated, and the preheating time is set according to the specific system.
[0087] Step 2. Operate the three-axis position turntable to adjust the strapdown inertial navigation system (that is, the quartz flexible accelerometer assembly) to figure 1 location shown. Capture the output of the quartz flexure accelerometer and fiber optic gyroscope assembly in terms of gravitational acceleration and the Earth's angular velocity Coarse alignment...