System and method for optical calibration of dynamic navigation capability of inertia measurement unit

An inertial measurement and calibration system technology, applied in measurement devices, instruments, etc., can solve the problems of low accuracy, difficult to guarantee parallel light, and inflexibility, and achieve the effect of high measurement accuracy

Active Publication Date: 2016-11-23
ZHEJIANG UNIV
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Problems solved by technology

Disadvantages: low precision, difficult to ensure parallel light, small measurement range, not flexible enough; 3) This method needs to install a reflector on the three mutually orthogonal surfaces of the measured object to achieve specular reflection of the laser , while the PSD realizes the reception of the reflected laser light, the torsion during the vibration process makes the reflected laser light enter different positions of the PSD, by detecting the position change of the reflected laser light, the torsion angle is measured in real time
[0004] With the continuous expansion of the industrial measurement field and the continuous improvement of measurement accuracy and measurement speed, the traditional contact measurement and cannot meet the demand

Method used

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  • System and method for optical calibration of dynamic navigation capability of inertia measurement unit
  • System and method for optical calibration of dynamic navigation capability of inertia measurement unit
  • System and method for optical calibration of dynamic navigation capability of inertia measurement unit

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Embodiment Construction

[0019] The present invention is described in detail below in conjunction with accompanying drawing.

[0020] like figure 1 and figure 2As shown, an optical calibration system for inertial measurement combined dynamic navigation performance includes an optical calibration device, an information collection module, a DSP, a communication interface and a PC, and the information collection module includes a first information collection unit and a second information collection unit and synchronization module, the first information collection unit collects the displacement data of three angular displacement measurement assemblies, the second information collection unit collects the data of the inertial measurement combination (3) to be measured, and the synchronization module sends information collection module one and information collection module two simultaneously Send a synchronous acquisition command, the information acquisition module is connected to the DSP, and the DSP is c...

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Abstract

The invention discloses a system and method for optical calibration of the dynamic navigation capability of an inertia measurement unit. The method of measuring displacement with a single laser displacement sensor and measuring angle with two laser displacement sensors is adopted to measure the displacement and angle of the inertia measurement unit from three dimensions in an external environment where a vibrating table is provided for dynamic navigation capability testing in real time, measured angle and displacement information is compared with an output value of the inertia measurement unit, and then calibration of the dynamic navigation capability of the inertia measurement unit is achieved. By the adoption of the method, non-contact measurement is achieved, output of the inertia measurement unit is measured in real time, bandwidth is large, stability is high, and application prospects are broad.

Description

technical field [0001] The invention relates to an optical calibration system and method for inertial measurement combined dynamic navigation performance, belonging to the field of optical sensing and measurement. technical background [0002] The inertial measurement unit is the core measurement unit of inertial navigation, and its performance determines the navigation accuracy and attitude control accuracy of the carrier. Whether the inertial measurement combination can accurately reflect the actual motion information of the carrier in a dynamic environment is the key to evaluating the performance of the inertial measurement instrument. In order to accurately evaluate the dynamic navigation accuracy and attitude measurement accuracy of the inertial measurement combination under dynamic conditions during the ground test phase, another independent evaluation method needs to be provided to evaluate the navigation and attitude measurement performance of the inertial measuremen...

Claims

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Application Information

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IPC IPC(8): G01C25/00
CPCG01C25/005
Inventor 张登伟陈磊舒晓武刘承
Owner ZHEJIANG UNIV
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