Method and equipment for full-automatic temperature compensation test of inertia measurement assembly

A combination of inertial measurement and temperature compensation technology, which is applied in the direction of navigation through speed/acceleration measurement, which can solve the problems of difficult and large-scale promotion and application, limited compensation accuracy, waste of resource occupation, etc., to eliminate human errors and achieve high reliability. , the effect of smooth rotation rate

Active Publication Date: 2013-11-27
THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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AI Technical Summary

Problems solved by technology

However, the test time usually takes about 7 days. The time is too long, and the resources are seriously wasted. In the test, the speed table and the incubator need to be manually operated at regular intervals. The workload is heavy and error-prone, and the temperature of each parameter needs to be repeated in the compensation test. Testing is a waste of manpower and material resources. The product needs to be powered off every time the parameter is switched. The parameters of the inertial group are affected by the successive power-on of the product and the temperature change environment. The compensation accuracy is limited and the compensation efficiency is extremely low. It is difficult to promote and apply on a large scale.

Method used

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  • Method and equipment for full-automatic temperature compensation test of inertia measurement assembly
  • Method and equipment for full-automatic temperature compensation test of inertia measurement assembly
  • Method and equipment for full-automatic temperature compensation test of inertia measurement assembly

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Embodiment Construction

[0036] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0037] Such as figure 1 and figure 2 As shown, the inertial measurement combined automatic temperature compensation test equipment of the present invention includes: a base 9; a left support frame 10.1 and a right support frame 10.2 are respectively provided on the base 9; a left support frame 10.1 and a right support frame 10.2 are respectively provided with a left The axes of the transverse rotating shaft 11.1 and the right transverse shaft 11.2, the left transverse rotating shaft 11.1 and the right transverse shaft 11.2 are all horizontal. A thermostat 2 is arranged between the left transverse shaft 11.1 and the right transverse shaft 11.2, that is, the left and right ends of the thermostat 2 are respectively connected with the left transverse shaft 11.1 and the right transverse shaft 11.2, and when the left transverse shaft 11.1...

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Abstract

The invention discloses a method and equipment for a temperature compensation full-automatic test of an inertia measurement assembly. The equipment comprises a base, two support frames, two transverse rotating shafts, an incubator, a fixing seat, a longitudinal rotating shaft, a placement table facet, a temperature control cabinet, a driving device, an inertia measurement assembly testing device and a processing unit, wherein the two support frames are arranged on the base; the two transverse rotating shafts are arranged on the two support frames; the left end and the right end of the incubator are respectively connected with the two transverse rotating shafts; the fixing seat is fixedly arranged on the inner wall of the incubator; the longitudinal rotating shaft is arranged on the fixing seat; the placement table facet is fixedly connected with the longitudinal rotating shaft and used for mounting the inertia measurement assembly; the temperature control cabinet is connected with the incubator; the driving device is connected with both the two transverse rotating shafts and the longitudinal rotating shaft; the inertia measurement assembly testing device is connected with the inertia measurement assembly through a CAN bus; the processing unit is connected with the temperature control cabinet, the driving device and the inertia measurement assembly testing device. The full-automatic temperature compensation test of the inertia measurement assembly performed by adopting the equipment provided by the invention has the advantages that the process is automatic, parameters are calculated automatically, the compensation efficiency is high, the reliability is high, and the compensation precision is high.

Description

technical field [0001] The invention relates to temperature compensation of inertial measurement combination, in particular to an inertial measurement combination automatic temperature compensation test method and equipment, and belongs to the technical field of inertial measurement combination test. Background technique [0002] The inertial measurement combination is mainly composed of gyroscopes, accelerometers and related circuits. It is the core component of the control system. It is mainly used for the angular velocity and acceleration in the motion of the sensitive carrier, and provides attitude and position information for the system guidance control. The accuracy of the inertial measurement combination will directly affect the final guidance accuracy. [0003] In the application of inertial measurement combination, since the accuracy of gyroscope and accelerometer is easily affected by temperature, temperature control measures are usually taken to make the product w...

Claims

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Application Information

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IPC IPC(8): G01C21/16
Inventor 吕江涛陆俊清刘源远王勇何健伟袁慧铮
Owner THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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