CN104949691A - MEMS inertial component rotation-modulation testing system based on ultrasonic motor - Google Patents

MEMS inertial component rotation-modulation testing system based on ultrasonic motor Download PDF

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CN104949691A
CN104949691A CN201510351515.0A CN201510351515A CN104949691A CN 104949691 A CN104949691 A CN 104949691A CN 201510351515 A CN201510351515 A CN 201510351515A CN 104949691 A CN104949691 A CN 104949691A
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ultrasonic motor
mems
data processing
inertial device
processing unit
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康国华
周琼峰
范凯
潘俊帆
陈雪芬
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Nanjing University of Aeronautics and Astronautics
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Nanjing University of Aeronautics and Astronautics
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C25/00Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass
    • G01C25/005Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass initial alignment, calibration or starting-up of inertial devices

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Abstract

The invention discloses an MEMS inertial component rotation-modulation testing system based on an ultrasonic motor. The MEMS inertial component rotation-modulation testing system comprises a rotary table, an inertial component, a wireless transmission unit, a data processing unit and an upper computer. The rotary table comprises a base and further comprises a coded disc, the ultrasonic motor, a table top, a driver and a bearing main shaft which are arranged inside a rotary table shell in a sleeved mode, wherein the bearing main shaft is arranged in the center of the base. The coded disc and the ultrasonic motor are coaxially arranged on the bearing main shaft, and a rotating shaft of the ultrasonic motor is fixedly connected with the table top. The upper computer sends signals to the data processing unit and outputs drive control instructions. The driver of the rotary table drives the ultrasonic motor to rotate, drives the bearing main shaft to rotate and drives the coded disc and the table top to coaxially rotate. After the inertial component obtains the angular rate information of the rotary table, the angular rate information is transmitted to the data processing unit through the wireless transmission unit to carry out strapdown resolving, and a resolving result is fed back to the upper computer. The MEMS inertial component rotation-modulation testing system has the advantages of being high in interference resisting capability, good in electromagnetic compatibility, wide in environmental application range and small and being integrated.

Description

基于超声电机的MEMS惯性器件旋转调制测试系统MEMS inertial device rotation modulation test system based on ultrasonic motor

技术领域 technical field

本发明涉及一种基于超声电机的MEMS惯性器件旋转调制测试系统,属于航空航天定位导航与控制技术领域。 The invention relates to a MEMS inertial device rotation modulation test system based on an ultrasonic motor, and belongs to the technical field of aerospace positioning, navigation and control.

背景技术 Background technique

近年来,随着微型MEMS技术和旋转调制技术越来越成熟,基于MEMS惯导器件的旋转调制系统迅速发展起来,即通过引入转动机构对MEMS惯性元件进行旋转调制,从而提高低精度、低成本MEMS惯导器件的性能。目前国外的MEMS旋转调制技术较为成熟,国内的研究起步较晚,尤其是系统的旋转调制转台,其控制精度、体积、功耗等性能指标与国外的技术水平仍有一定的差距。从查到的资料看,最早开展旋转调制技术实物研究且比较领先的是国防科技大学,2007年研制出了旋转式捷联惯导系统样机,但是精度不甚理想,单轴旋转的船试导航误差大约为17n mile/24h,实验室静态导航精度优于1n mile/24h,关于双轴旋转的误差没有给出。可见这方面仍然有很多工作需要完成。 In recent years, as micro-MEMS technology and rotational modulation technology have become more and more mature, the rotational modulation system based on MEMS inertial navigation devices has developed rapidly, that is, the rotational modulation of MEMS inertial components is carried out by introducing a rotating mechanism, thereby improving low-precision, low-cost Performance of MEMS inertial navigation devices. At present, the MEMS rotary modulation technology in foreign countries is relatively mature, and the domestic research started relatively late, especially for the rotary modulation turntable of the system, its control accuracy, volume, power consumption and other performance indicators still have a certain gap with the foreign technical level. From the information found, the National University of Defense Technology was the first to carry out physical research on rotary modulation technology and was relatively leading. In 2007, a prototype of a rotary strapdown inertial navigation system was developed, but the accuracy was not ideal. Single-axis rotary ship test navigation The error is about 17n mile/24h, the static navigation accuracy of the laboratory is better than 1n mile/24h, and the error about the dual-axis rotation is not given. It can be seen that there is still a lot of work to be done in this regard.

目前,有文献分析了单轴旋转运动旋转轴的选取、旋转速率对误差调制效果的影响及旋转方案的评价准则,然后在此基础上,对单轴旋转式捷联惯导系统在不同的旋转运动方案下对惯性测量组件的误差调制机理进行了研究,最后仿真分析比较了不同旋转运动方案的误差。也有文献提出了将 IMU 倾斜安装的改进单轴旋转方案,从原理上分析了该方案能够完全消除三个方向上的惯性器件误差,分析了转位机构信息与光纤陀螺信息的时间同步性问题,推导了延迟时间对旋转式捷联惯导系统姿态误差的影响,给出了一种延迟时间的测量方法和补偿策略,并进行了相关试验验证。 At present, some literatures have analyzed the selection of the rotation axis of the single-axis rotation motion, the influence of the rotation rate on the error modulation effect and the evaluation criteria of the rotation scheme, and then on this basis, the single-axis rotation SINS in different rotation The error modulation mechanism of the inertial measurement component is studied under the motion scheme, and finally the error of different rotation motion schemes is compared by simulation analysis. There are also literatures that propose an improved single-axis rotation scheme that installs the IMU obliquely. It is analyzed in principle that this scheme can completely eliminate the inertial device errors in three directions, and the time synchronization between the information of the indexing mechanism and the information of the fiber optic gyroscope is analyzed. The influence of the delay time on the attitude error of the rotary strapdown inertial navigation system is deduced, and a delay time measurement method and compensation strategy are given, and related experiments are carried out to verify.

另外,根据MEMS器件的误差特性,选择了一种适合MEMS器件捷联惯导系统的旋转调制方案并自主研发了原理样机。静态和车载实验表明:旋转调制可以明显抑制MEMS器件常值误差对导航精度的影响,200s内俯仰和横滚姿态精度提高了5倍,速度和位置精度提高了近10倍。其他文献设计了利用高精度单轴转台的陀螺仪静态漂移测试的翻滚法、动态漂移测试的恒速试验和角振动试验。分析了测试转台速率精度和速率平稳性对陀螺测试带来的影响,提出了转台基座倾斜的自动补偿,验证了高精度单轴转台的大角速度对陀螺漂移测试带来的好处。此外,现有试验表明,强磁场下MEMS器件输出将收到严重影响,而常规基于电磁原理的电机其主轴方向的磁场恰好是最大,因此尤其不适合MEMS器件的误差调制。 In addition, according to the error characteristics of MEMS devices, a rotation modulation scheme suitable for the strapdown inertial navigation system of MEMS devices was selected and a prototype was independently developed. Static and vehicle experiments show that the rotation modulation can significantly suppress the influence of MEMS device constant error on navigation accuracy, the accuracy of pitch and roll attitude is increased by 5 times, and the accuracy of speed and position is increased by nearly 10 times within 200s. Other literatures have designed the tumbling method of the gyroscope static drift test, the constant speed test and the angular vibration test of the dynamic drift test using a high-precision single-axis turntable. The influence of the test turntable rate accuracy and rate stability on the gyro test is analyzed, and the automatic compensation of the turntable base tilt is proposed, and the benefits of the high angular velocity of the high-precision single-axis turntable on the gyro drift test are verified. In addition, existing tests have shown that the output of MEMS devices will be seriously affected under strong magnetic fields, and the magnetic field in the direction of the main axis of conventional electromagnetic-based motors happens to be the largest, so it is especially not suitable for error modulation of MEMS devices.

尽管目前的MEMS技术得到逐步改进,但是其仍然存在问题。传统的旋转调制转台由于电机、驱动器等设备的限制,导致系统控制精度低、体积大、功耗高、剩磁强,掉电易失锁,以及系统中传输方式不够灵活,因此使得系统不利于实现小型化和集成化。 Although the current MEMS technology has been gradually improved, it still has problems. Due to the limitations of motors, drivers and other equipment, the traditional rotary modulation turntable leads to low system control accuracy, large volume, high power consumption, strong residual magnetism, easy loss of lock when power is off, and inflexible transmission methods in the system, which makes the system unfavorable. Realize miniaturization and integration.

发明内容 Contents of the invention

本发明所要解决的技术问题在于克服现有技术的不足,提供一种基于超声电机的MEMS惯性器件旋转调制测试系统,解决现有系统控制精度低、体积大、功耗高、剩磁强等、掉电失锁等问题,具有强抗干扰能力、电磁兼容性好、环境适应范围广、可小型化和集成化等优点。 The technical problem to be solved by the present invention is to overcome the deficiencies of the prior art, provide a MEMS inertial device rotation modulation test system based on an ultrasonic motor, and solve the problems of low control accuracy, large volume, high power consumption, and strong residual magnetism in the existing system. It has the advantages of strong anti-interference ability, good electromagnetic compatibility, wide range of environmental adaptability, miniaturization and integration, etc.

本发明具体采用以下技术方案解决上述技术问题: The present invention specifically adopts the following technical solutions to solve the above technical problems:

一种基于超声电机的MEMS惯性器件旋转调制测试系统,包括转台、惯性器件、无线传输单元、数据处理单元、上位机,所述转台包括基座及套置在转台外壳内的码盘、超声电机、台面、驱动器和轴承主轴;其中轴承主轴安装在基座的中心处,所述码盘和超声电机同轴安装于轴承主轴上,超声电机的转轴与台面固定连接;所述驱动器与超声电机输入端连接,所述惯性器件设置于台面的中心;所述上位机用于发送控制信号;所述数据处理单元用于接收控制信号及生成驱动控制指令;所述驱动器用于根据控制指令驱动超声电机旋转,及带动轴承主轴和码盘、台面进行同轴旋转;所述惯性器件用于获得转台的角速率信息及通过无线传输单元进行传输;所述数据处理单元用于对所接收的角速率信息进行捷联解算,及将获得的解算结果反馈至上位机。 A MEMS inertial device rotation modulation test system based on an ultrasonic motor, including a turntable, an inertial device, a wireless transmission unit, a data processing unit, and a host computer. , a table, a driver and a bearing main shaft; wherein the bearing main shaft is installed at the center of the base, the code disc and the ultrasonic motor are coaxially installed on the bearing main shaft, and the rotating shaft of the ultrasonic motor is fixedly connected to the table; the driver and the ultrasonic motor input terminal connection, the inertial device is set at the center of the table; the host computer is used to send control signals; the data processing unit is used to receive control signals and generate drive control instructions; the driver is used to drive the ultrasonic motor according to the control instructions Rotate, and drive the bearing spindle, the code disc, and the table to rotate coaxially; the inertial device is used to obtain the angular rate information of the turntable and transmit it through the wireless transmission unit; the data processing unit is used to process the received angular rate information Perform strapdown calculations, and feed back the obtained calculation results to the host computer.

进一步地,作为本发明优选的技术方案:所述惯性器件包括MEMS陀螺和加速度计。 Further, as a preferred technical solution of the present invention: the inertial device includes a MEMS gyroscope and an accelerometer.

进一步地,作为本发明优选的技术方案:所述角速率信息包括角速率、角度和旋转角加速度。 Further, as a preferred technical solution of the present invention: the angular rate information includes angular rate, angle and rotational angular acceleration.

进一步地,作为本发明优选的技术方案:所述无线传输单元为无线蓝牙模块。 Further, as a preferred technical solution of the present invention: the wireless transmission unit is a wireless Bluetooth module.

进一步地,作为本发明优选的技术方案:所述数据处理单元为计算机。 Further, as a preferred technical solution of the present invention: the data processing unit is a computer.

进一步地,作为本发明优选的技术方案:所述计算机采用嵌入式计算机。 Further, as a preferred technical solution of the present invention: the computer adopts an embedded computer.

本发明采用上述技术方案,能产生如下技术效果: The present invention adopts above-mentioned technical scheme, can produce following technical effect:

(1)、本发明提供的基于超声电机的MEMS惯性器件旋转调制测试系统,基于新型超声电机技术的发展和应用,研制超声电机调制转台,及结合无线传输技术,通过仿真分析和验证算法,实现系统的旋转调制功能。该转台不仅克服了传统转台体积大、功耗大、精度低、剩磁大等困难,而且具有强抗干扰能力、电磁兼容性好、环境适应范围广、可小型化和集成化等优点,为后期研制高精度、低成本的MEMS旋转调制系统以及MEMS惯导系统提供强而有力技术支持。 (1) The ultrasonic motor-based MEMS inertial device rotation modulation test system provided by the present invention, based on the development and application of new ultrasonic motor technology, develops an ultrasonic motor modulation turntable, and combines wireless transmission technology, through simulation analysis and verification algorithms, to achieve Rotary modulation function of the system. The turntable not only overcomes the difficulties of traditional turntables such as large volume, high power consumption, low precision, and large residual magnetism, but also has the advantages of strong anti-interference ability, good electromagnetic compatibility, wide environmental adaptability, miniaturization and integration, etc. The later development of high-precision, low-cost MEMS rotary modulation system and MEMS inertial navigation system provides strong technical support.

(2)、基于超声电机转台及MEMS惯性器件,利用本发明研制的超声电机转台调制MEMS陀螺,与传统转台相比,可提高调制精度且无强磁干扰,控制精度高。 (2) Based on the ultrasonic motor turntable and MEMS inertial devices, the ultrasonic motor turntable developed by the present invention is used to modulate the MEMS gyroscope. Compared with the traditional turntable, the modulation accuracy can be improved without strong magnetic interference, and the control accuracy is high.

(3)、系统以嵌入式计算机为核心控制板,完成旋转调制系统的搭建,通过实物实现上述旋转调制系统,完成系统测试实验。通过实验结果的分析,可以精准地验证超声电机转台对MEMS陀螺旋转调制的影响,为后期研制高精度、低成本的MEMS旋转惯导系统提供技术支持。 (3) The system takes the embedded computer as the core control board to complete the construction of the rotary modulation system, realize the above rotary modulation system through the physical object, and complete the system test experiment. Through the analysis of the experimental results, the influence of the ultrasonic motor turntable on the rotation modulation of the MEMS gyro can be accurately verified, and technical support can be provided for the later development of a high-precision, low-cost MEMS rotary inertial navigation system.

附图说明 Description of drawings

图1为本发明基于超声电机的MEMS惯性器件旋转调制测试系统的模块示意图。 FIG. 1 is a block diagram of the MEMS inertial device rotation modulation testing system based on an ultrasonic motor according to the present invention.

图2为本发明中转台的机构示意图。 Fig. 2 is a schematic diagram of the mechanism of the repeater of the present invention.

其中标号解释:1-基座、2-码盘、3-超声电机、4-台面、5-驱动器、6-外壳、7-轴承主轴。 Explanation of the labels: 1-base, 2-code disc, 3-ultrasonic motor, 4-table, 5-driver, 6-housing, 7-bearing spindle.

具体实施方式 Detailed ways

下面结合说明书附图,对本发明的实施方式进行描述。 Embodiments of the present invention will be described below in conjunction with the accompanying drawings.

 如图1所示,本发明设计了一种基于超声电机的MEMS惯性器件旋转调制测试系统,包括转台、惯性器件、无线传输单元、数据处理单元、上位机,其中所述转台的结构如图2所示,包括基座1及套置在转台外壳6内的码盘2、超声电机3、台面4、驱动器5和轴承主轴7;其中轴承主轴7安装在基座1的中心处,所述码盘2和超声电机3同轴安装于轴承主轴7上,超声电机3的转轴与台面4固定连接;所述驱动器5与超声电机3输入端连接,所述惯性器件设置于台面4的中心;所述上位机用于发送控制信号;所述数据处理单元用于接收控制信号及生成驱动控制指令;所述驱动器用于根据控制指令驱动超声电机旋转,及带动轴承主轴和码盘、台面进行同轴旋转;所述惯性器件用于获得转台的角速率信息及通过无线传输单元进行传输;所述数据处理单元用于对所接收的角速率信息进行捷联解算,及将获得的解算结果反馈至上位机。 As shown in Figure 1, the present invention designs a MEMS inertial device rotation modulation test system based on an ultrasonic motor, including a turntable, an inertial device, a wireless transmission unit, a data processing unit, and a host computer, wherein the structure of the turntable is shown in Figure 2 As shown, it includes a base 1 and a code disc 2 nested in the turntable shell 6, an ultrasonic motor 3, a table 4, a driver 5 and a bearing main shaft 7; wherein the bearing main shaft 7 is installed at the center of the base 1, and the code The disk 2 and the ultrasonic motor 3 are coaxially installed on the bearing main shaft 7, and the rotating shaft of the ultrasonic motor 3 is fixedly connected to the table 4; the driver 5 is connected to the input end of the ultrasonic motor 3, and the inertial device is arranged at the center of the table 4; The upper computer is used to send control signals; the data processing unit is used to receive control signals and generate drive control instructions; the driver is used to drive the ultrasonic motor to rotate according to the control instructions, and drive the bearing spindle, code disc, and table to perform coaxial Rotate; the inertial device is used to obtain the angular rate information of the turntable and transmit it through the wireless transmission unit; the data processing unit is used to perform strapdown calculation on the received angular rate information, and feed back the obtained solution result to the host computer.

其原理是:由上位机向数据处理单元发送控制信号,数据处理单元输出驱动控制指令;所述转台的驱动器5根据控制指令驱动超声电机3旋转,带动轴承主轴7转动以及码盘2、台面4同轴旋转;所述惯性器件获得转台的角速率信息,及通过无线传输单元传输至数据处理单元进行捷联解算;由数据处理单元将解算结果反馈至上位机。 The principle is: the upper computer sends a control signal to the data processing unit, and the data processing unit outputs a drive control command; the driver 5 of the turntable drives the ultrasonic motor 3 to rotate according to the control command, driving the bearing spindle 7 to rotate and the code disc 2 and the table 4 Coaxial rotation; the inertial device obtains the angular rate information of the turntable, and transmits it to the data processing unit through the wireless transmission unit for strapdown calculation; the data processing unit feeds back the calculation result to the host computer.

进一步地,系统中惯性器件可以采用MEMS陀螺和加速度计,为了更清晰的分析旋转对惯性元器件各项误差的调制特性,选取ADI低精度的MEMS陀螺作为系统角速率敏感元器件,陀螺通过RS232接口以数字信号的方式实时输出敏感到的角速率信息。以及选取加速度计测量转台的旋转角加速度。与传统转台相比,系统可提高调制精度且无磁干扰,控制精度高。 Furthermore, MEMS gyroscopes and accelerometers can be used for inertial components in the system. In order to more clearly analyze the modulation characteristics of rotation on the errors of inertial components, ADI’s low-precision MEMS gyroscopes are selected as system angular rate sensitive components. The gyroscopes are connected through RS232 The interface outputs sensitive angular rate information in real time in the form of digital signals. And select the accelerometer to measure the rotational angular acceleration of the turntable. Compared with the traditional turntable, the system can improve the modulation accuracy and has no magnetic interference, and the control accuracy is high.

在此基础上,系统中,MEMS陀螺和加速度计组件直接输出的是在惯性测量组件坐标系下的角速率和比力信息,需要通过惯性测量组件坐标系到载体坐标系的转换矩阵将这些信息转换到载体坐标系中来,再通过数据处理模块求解出运载体的导航参数。根据导航参数,能够验证系统在有惯性器件的基础下,使得系统导航精度得到有效提高。 On this basis, in the system, the MEMS gyroscope and accelerometer components directly output the angular rate and specific force information in the coordinate system of the inertial measurement component, which needs to be transformed by the conversion matrix from the coordinate system of the inertial measurement component to the carrier coordinate system Convert to the carrier coordinate system, and then solve the navigation parameters of the carrier through the data processing module. According to the navigation parameters, it can be verified that the system's navigation accuracy is effectively improved on the basis of inertial devices.

系统在实现数据传输时,可以采用无线蓝牙模块,通过无线传输方式降低系统硬件上的复杂性,实现无线方式下的可靠传输。 When the system realizes data transmission, the wireless Bluetooth module can be used to reduce the complexity of the system hardware through wireless transmission and realize reliable transmission in wireless mode.

并且,系统中的数据处理单元,其主要功能是实现数据的处理,可以采用计算机。并且计算机采用嵌入式,可利用FPGA控制板,实现对转动机构的控制、与传感器的串口通讯、导航捷联解算及显示存储等功能。转台控制和捷联解算一体控制化,转台控制和器件精度之间通常是开环的:控制指令只保证转台的精确性,本系统把器件精度和转台控制关联起来,增加一个惯性器件精度的评估模块,使得MEMS实时精度评估,若改善不到一个数量级,则通过FPGA修改算法,让转台加速或者换向等。 Moreover, the data processing unit in the system, whose main function is to realize data processing, may use a computer. And the computer is embedded, and the FPGA control board can be used to realize functions such as control of the rotating mechanism, serial communication with the sensor, navigation strapdown solution, display and storage. Turntable control and strapdown calculation are integrated control, and there is usually an open loop between turntable control and device accuracy: the control command only guarantees the accuracy of the turntable, this system associates the device accuracy with the turntable control, adding an inertial device accuracy The evaluation module enables the real-time accuracy evaluation of MEMS. If the improvement is less than an order of magnitude, the algorithm is modified through the FPGA to accelerate or change the direction of the turntable.

      综上,本发明提供的基于超声电机的MEMS惯性器件旋转调制测试系统,基于新型超声电机技术的发展和应用,研制超声电机调制转台,及结合无线传输技术,通过仿真分析和验证算法,实现系统的旋转调制功能。该转台不仅克服了传统转台体积大、功耗大、精度低等困难,而且具有强抗干扰能力、电磁兼容性好、环境适应范围广、可小型化和集成化等优点,为后期研制高精度、低成本的MEMS旋转调制系统以及MEMS惯导系统提供强而有力技术支持。 In summary, the ultrasonic motor-based MEMS inertial device rotation modulation test system provided by the present invention, based on the development and application of new ultrasonic motor technology, develops an ultrasonic motor modulation turntable, and combines wireless transmission technology, through simulation analysis and verification algorithms, to realize the system Rotary modulation function. The turntable not only overcomes the difficulties of traditional turntables such as large volume, high power consumption, and low precision, but also has the advantages of strong anti-interference ability, good electromagnetic compatibility, wide environmental adaptability, miniaturization and integration, etc. , low-cost MEMS rotary modulation system and MEMS inertial navigation system provide strong technical support.

上面结合附图对本发明的实施方式作了详细说明,但是本发明并不限于上述实施方式,在本领域普通技术人员所具备的知识范围内,还可以在不脱离本发明宗旨的前提下做出各种变化。 The embodiments of the present invention have been described in detail above in conjunction with the accompanying drawings, but the present invention is not limited to the above embodiments, and can also be made without departing from the gist of the present invention within the scope of knowledge possessed by those of ordinary skill in the art. Variations.

Claims (6)

1.基于超声电机的MEMS惯性器件旋转调制测试系统,其特征在于:包括转台、惯性器件、无线传输单元、数据处理单元、上位机,所述转台包括基座及套置在转台外壳内的码盘、超声电机、台面、驱动器和轴承主轴;其中轴承主轴安装在基座的中心处,所述码盘和超声电机同轴安装于轴承主轴上,超声电机的转轴与台面固定连接;所述驱动器与超声电机输入端连接,所述惯性器件设置于台面的中心;所述上位机用于发送控制信号;所述数据处理单元用于接收控制信号及生成驱动控制指令;所述驱动器用于根据控制指令驱动超声电机旋转,及带动轴承主轴和码盘、台面进行同轴旋转;所述惯性器件用于获得转台的角速率信息及通过无线传输单元进行传输;所述数据处理单元用于对所接收的角速率信息进行捷联解算,及将获得的解算结果反馈至上位机。 1. The rotating modulation test system of MEMS inertial devices based on ultrasonic motors is characterized in that: it includes a turntable, an inertial device, a wireless transmission unit, a data processing unit, and a host computer, and the turntable includes a base and a code set in the turntable shell. Disc, ultrasonic motor, table, driver and bearing main shaft; wherein the bearing main shaft is installed at the center of the base, the code disc and the ultrasonic motor are coaxially installed on the bearing main shaft, and the rotating shaft of the ultrasonic motor is fixedly connected with the table; the driver Connected to the input end of the ultrasonic motor, the inertial device is arranged at the center of the table; the host computer is used to send control signals; the data processing unit is used to receive control signals and generate drive control instructions; the driver is used to The command drives the ultrasonic motor to rotate, and drives the bearing spindle, the code disc, and the table to rotate coaxially; the inertial device is used to obtain the angular rate information of the turntable and transmit it through the wireless transmission unit; the data processing unit is used to process the received The angular rate information is used for strapdown calculations, and the obtained calculation results are fed back to the host computer. 2.根据权利要求1所述基于超声电机的MEMS惯性器件旋转调制测试系统,其特征在于:所述惯性器件包括MEMS陀螺和加速度计。 2. The MEMS inertial device rotation modulation test system based on the ultrasonic motor according to claim 1, characterized in that: the inertial device includes a MEMS gyroscope and an accelerometer. 3.根据权利要求1所述基于超声电机的MEMS惯性器件旋转调制测试系统,其特征在于:所述角速率信息包括角速率、角度和旋转角加速度。 3. The MEMS inertial device rotation modulation test system based on the ultrasonic motor according to claim 1, wherein the angular rate information includes angular rate, angle and rotational angular acceleration. 4.根据权利要求1所述基于超声电机的MEMS惯性器件旋转调制测试系统,其特征在于:所述无线传输单元为无线蓝牙模块。 4. The MEMS inertial device rotation modulation test system based on ultrasonic motor according to claim 1, characterized in that: the wireless transmission unit is a wireless Bluetooth module. 5.根据权利要求1所述基于超声电机的MEMS惯性器件旋转调制测试系统,其特征在于:所述数据处理单元为计算机。 5. The ultrasonic motor-based MEMS inertial device rotation modulation testing system according to claim 1, characterized in that: the data processing unit is a computer. 6.根据权利要求5所述基于超声电机的MEMS惯性器件旋转调制测试系统,其特征在于:所述计算机采用嵌入式计算机。 6. The MEMS inertial device rotational modulation test system based on the ultrasonic motor according to claim 5, characterized in that: the computer is an embedded computer.
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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107014400A (en) * 2017-05-22 2017-08-04 南京信息工程大学 The self-checking device and calibration method of unmanned plane inertial navigation unit
CN107192853A (en) * 2017-07-24 2017-09-22 桂林航天工业学院 Angular-rate sensor test device and system
CN109142790A (en) * 2018-08-30 2019-01-04 恒有(苏州)精工机电有限公司 Acceleration transducer based on lonely pole ultrasound electric machine
CN109254536A (en) * 2017-07-13 2019-01-22 北京信息科技大学 A kind of high dynamic gyro error control simulator
CN109959393A (en) * 2019-04-10 2019-07-02 中国航空工业集团公司北京航空精密机械研究所 Decision maker and its method for electronic inertial navigation turntable driving state
CN110940352A (en) * 2019-11-08 2020-03-31 中国计量科学研究院 Automatic calibration system of micro-electro-mechanical system inertia measurement unit and calibration verification method thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5751425A (en) * 1996-12-30 1998-05-12 Litton Systems, Inc. Apparatus and method for detecting rotation rate, Faraday bias and cavity length in a ring laser gyroscope
CN101701825A (en) * 2009-09-28 2010-05-05 龙兴武 High-precision laser gyroscope single-shaft rotating inertial navigation system
CN202126265U (en) * 2011-06-24 2012-01-25 西安测绘研究所 Dynamic rotating and modulating gyro north seeker
CN102840856A (en) * 2011-06-24 2012-12-26 西安测绘研究所 Dynamically rotary modulated north-seeking method for gyroscope
CN103344226A (en) * 2013-06-27 2013-10-09 南京航空航天大学 North seeking system and method based on MEMS (Micro-electromechanical Systems) rotation technique

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5751425A (en) * 1996-12-30 1998-05-12 Litton Systems, Inc. Apparatus and method for detecting rotation rate, Faraday bias and cavity length in a ring laser gyroscope
CN101701825A (en) * 2009-09-28 2010-05-05 龙兴武 High-precision laser gyroscope single-shaft rotating inertial navigation system
CN202126265U (en) * 2011-06-24 2012-01-25 西安测绘研究所 Dynamic rotating and modulating gyro north seeker
CN102840856A (en) * 2011-06-24 2012-12-26 西安测绘研究所 Dynamically rotary modulated north-seeking method for gyroscope
CN103344226A (en) * 2013-06-27 2013-10-09 南京航空航天大学 North seeking system and method based on MEMS (Micro-electromechanical Systems) rotation technique

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
孙伟等: "基于IMU旋转的MEMS器件误差调制技术研究", 《电子测量与仪器学报》 *
徐烨烽等: "MEMS旋转调制式航姿参考系统设计及误差补偿", 《兵工学报》 *
朱华等: "微型旋转超声电机的发展和现状", 《压电与声光》 *
王学运等: "MEMS器件捷联惯导系统旋转调制技术", 《东北大学学报(自然科学版)》 *

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107014400A (en) * 2017-05-22 2017-08-04 南京信息工程大学 The self-checking device and calibration method of unmanned plane inertial navigation unit
CN107014400B (en) * 2017-05-22 2023-09-26 南京信息工程大学 Automatic calibration device and calibration method for UAV inertial navigation unit
CN109254536A (en) * 2017-07-13 2019-01-22 北京信息科技大学 A kind of high dynamic gyro error control simulator
CN107192853A (en) * 2017-07-24 2017-09-22 桂林航天工业学院 Angular-rate sensor test device and system
CN109142790A (en) * 2018-08-30 2019-01-04 恒有(苏州)精工机电有限公司 Acceleration transducer based on lonely pole ultrasound electric machine
CN109959393A (en) * 2019-04-10 2019-07-02 中国航空工业集团公司北京航空精密机械研究所 Decision maker and its method for electronic inertial navigation turntable driving state
CN109959393B (en) * 2019-04-10 2024-09-27 中国航空工业集团公司北京航空精密机械研究所 Device and method for judging galloping state of electric inertial navigation turntable
CN110940352A (en) * 2019-11-08 2020-03-31 中国计量科学研究院 Automatic calibration system of micro-electro-mechanical system inertia measurement unit and calibration verification method thereof
CN110940352B (en) * 2019-11-08 2022-03-08 中国计量科学研究院 Automatic calibration system of micro-electro-mechanical system inertia measurement unit and calibration verification method thereof

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