[go: up one dir, main page]

CN107167135A - A kind of scanning mirror points to high-precision static state angle measurement method - Google Patents

A kind of scanning mirror points to high-precision static state angle measurement method Download PDF

Info

Publication number
CN107167135A
CN107167135A CN201710563629.0A CN201710563629A CN107167135A CN 107167135 A CN107167135 A CN 107167135A CN 201710563629 A CN201710563629 A CN 201710563629A CN 107167135 A CN107167135 A CN 107167135A
Authority
CN
China
Prior art keywords
scanning mirror
angle measurement
gyro
angle
goniometer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201710563629.0A
Other languages
Chinese (zh)
Other versions
CN107167135B (en
Inventor
王淦泉
王伟成
刘德胜
李盼盼
龚德仁
游力军
赵立忠
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanghai Institute of Technical Physics of CAS
Original Assignee
Shanghai Institute of Technical Physics of CAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shanghai Institute of Technical Physics of CAS filed Critical Shanghai Institute of Technical Physics of CAS
Priority to CN201710563629.0A priority Critical patent/CN107167135B/en
Publication of CN107167135A publication Critical patent/CN107167135A/en
Application granted granted Critical
Publication of CN107167135B publication Critical patent/CN107167135B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/18Stabilised platforms, e.g. by gyroscope
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/20Instruments for performing navigational calculations

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Optical Scanning Systems (AREA)

Abstract

本发明公开了一种扫描镜指向高精度静态测角方法,该方法将高精度陀螺测角仪安装并固定在扫描镜转轴上,在扫描控制器的作用下,使得陀螺测角仪与扫描镜在力矩电机的驱动下同步作连续低于1°/s匀速运动,从而获取该速度条件下的扫描镜运动角度数据。测量时,感应同步器组件测角数据以及激光陀螺的测角数据均传至外围计算机,由计算机对二组测角数据进行比对,并通过合适的算法对感应同步器组件测角数据进行校正。本发明的有益效果是采集数据频率可到2000Hz以上,测量范围可达10°以上,测量精度可达0.3″(3σ),测试角度间隔为1.8″。经校正后扫描镜指向精度达到0.5″(3σ)。

The invention discloses a scanning mirror pointing high-precision static angle measurement method. In the method, a high-precision gyro goniometer is installed and fixed on the rotating shaft of the scanning mirror. Under the action of the scanning controller, the gyro goniometer and the scanning mirror Under the drive of the torque motor, it is synchronously and continuously moving at a uniform speed lower than 1°/s, so as to obtain the motion angle data of the scanning mirror under this speed condition. During the measurement, the angle measurement data of the inductosynchronizer component and the angle measurement data of the laser gyroscope are transmitted to the peripheral computer, and the computer compares the two sets of angle measurement data, and corrects the angle measurement data of the inductosynchronizer component through a suitable algorithm . The beneficial effect of the invention is that the frequency of data collection can reach more than 2000 Hz, the measurement range can reach more than 10°, the measurement accuracy can reach 0.3" (3σ), and the test angle interval is 1.8". After correction, the pointing accuracy of the scanning mirror reaches 0.5″ (3σ).

Description

一种扫描镜指向高精度静态测角方法A Scanning Mirror Pointing High Precision Static Angle Measurement Method

技术领域technical field

本发明涉及一种空间扫描机构在线高精度静态测角方法,属于扫描机构测角技术领域。The invention relates to an online high-precision static angle measurement method of a space scanning mechanism, which belongs to the technical field of angle measurement of a scanning mechanism.

背景技术Background technique

空间高精度扫描机构一般采用圆感应同步器作为角度传感器,圆感应同步器由转子和定子组成。扫描机构组装时,圆感应同步器的转子和定子分别安装在机构框架和转轴上。感应同步器测角信号经过电路放大和转换,传输给控制器,感应同步器及其信息处理电路、电机及其控制电路构成一个完整的闭环控制系统。同时,由于感应同步器自身的偏差,综合静态误差可能超过1″(1σ),导致感应同步器组件测角精度不能满足实际扫描镜指向时测量和控制精度要求,需要一种方法对扫描镜指向精度进行测试,并利用测试结果对感应同步器组件精度进行校正,使扫描镜指向精度进一步提高。The space high-precision scanning mechanism generally uses a circular induction synchronizer as an angle sensor, and the circular induction synchronizer is composed of a rotor and a stator. When the scanning mechanism is assembled, the rotor and stator of the circular induction synchronizer are installed on the mechanism frame and the rotating shaft respectively. The angle measurement signal of the induction synchronizer is amplified and converted by the circuit, and then transmitted to the controller. The induction synchronizer and its information processing circuit, the motor and its control circuit constitute a complete closed-loop control system. At the same time, due to the deviation of the inductosynchronizer itself, the comprehensive static error may exceed 1″ (1σ), resulting in the angular measurement accuracy of the inductosynchronizer components not meeting the measurement and control accuracy requirements of the actual scanning mirror pointing. The precision is tested, and the test results are used to correct the precision of the inductive synchronizer components, so that the pointing precision of the scanning mirror is further improved.

目前空间高精度扫描机构的测角一般采用高精度经纬仪进行静态角度测量。采用高精度经纬仪进行静态角度测量时,受仪器自身和读数等误差因素的影响,精度一般低于1″(1σ)。同时,由于受时间成本因素的影响,经纬仪进行静态角度测量的密度不会很高,即相邻二个测量点之间的角度间隔较大。相邻二点之间的角度值通过内插推导,因而无法获得连续的高精度角度测量值,将不利于实现高精度角度修正算法,无法实现扫描镜指向精度的进一步提高。At present, the angle measurement of space high-precision scanning mechanism generally uses high-precision theodolite for static angle measurement. When using a high-precision theodolite for static angle measurement, the accuracy is generally lower than 1″ (1σ) due to the influence of error factors such as the instrument itself and readings. At the same time, due to the influence of time and cost factors, the density of the theodolite for static angle measurement will not Very high, that is, the angle interval between two adjacent measurement points is relatively large. The angle value between two adjacent points is derived by interpolation, so it is impossible to obtain continuous high-precision angle measurement values, which is not conducive to the realization of high-precision angle The correction algorithm cannot further improve the pointing accuracy of the scanning mirror.

发明内容Contents of the invention

本发明目的是,在现有空间高精度扫描机构扫描镜指向精度基础上,提出一种激光陀螺测角仪在线测试方法,实现扫描镜指向高精度、高密度、大范围静态测量,并将测量结果用于感应同步器组件精度校正,可以明显提高扫描镜的指向精度。The object of the present invention is to propose a laser gyro goniometer online test method on the basis of the pointing accuracy of the scanning mirror of the existing high-precision scanning mechanism in space, to realize high-precision, high-density, and large-scale static measurement of the scanning mirror pointing, and to measure The results are used to correct the precision of the inductosynchronizer assembly, which can obviously improve the pointing precision of the scanning mirror.

本发明的技术方案是将高精度陀螺测角仪安装并固定在扫描镜转轴上,在扫描控制器的作用下,使得陀螺测角仪与扫描镜在力矩电机的驱动下同步作连续低于1°/s匀速运动,从而获取该速度条件下的扫描镜运动角度数据。测量时,感应同步器组件测角数据以及激光陀螺的测角数据均传至外围计算机,由计算机对二组测角数据进行比对,并通过合适的算法对感应同步器组件测角数据进行校正。经过校正后的感应同步器组件测角数据被重新用于闭环控制,明显提高了扫描镜指向精度。The technical solution of the present invention is to install and fix the high-precision gyro goniometer on the rotating shaft of the scanning mirror. °/s at a constant speed, so as to obtain the motion angle data of the scanning mirror under this speed condition. During the measurement, the angle measurement data of the inductosynchronizer components and the angle measurement data of the laser gyroscope are transmitted to the peripheral computer, and the computer compares the two sets of angle measurement data, and corrects the angle measurement data of the inductosynchronizer components through a suitable algorithm . The corrected angle measurement data of the inductosynchronizer assembly is reused for closed-loop control, which significantly improves the pointing accuracy of the scanning mirror.

本发明的有益效果是采集数据频率可到2000Hz以上,测量范围可达10°以上,测量精度可达0.3″(3σ),测试角度间隔为1.8″。经校正后扫描镜指向精度达到0.5″(3σ)。The beneficial effect of the invention is that the frequency of data collection can reach more than 2000 Hz, the measurement range can reach more than 10°, the measurement accuracy can reach 0.3" (3σ), and the test angle interval is 1.8". After correction, the pointing accuracy of the scanning mirror reaches 0.5″ (3σ).

所述高精度扫描机构静态测角方法由陀螺测角仪、感应同步器及其处理电路、扫描镜及其机构组件、扫描控制器和控制计算机等组成的装置来实现。The high-precision scanning mechanism static angle measurement method is realized by a device composed of a gyro goniometer, an inductive synchronizer and its processing circuit, a scanning mirror and its mechanism components, a scanning controller, and a control computer.

所述陀螺测角仪由激光陀螺及其固定工装、陀螺测试计算机组成。The gyro goniometer is composed of a laser gyro and its fixed tooling, and a gyro test computer.

附图说明Description of drawings

图1是扫描镜运动高精度动态测角方法布局图。Figure 1 is a layout diagram of the high-precision dynamic angle measurement method for scanning mirror movement.

图1中,1是激光陀螺;2是扫描机构框架;3是扫描镜及其转轴;4是感应同步器。In Fig. 1, 1 is a laser gyro; 2 is a scanning mechanism frame; 3 is a scanning mirror and its rotating shaft; 4 is an inductive synchronizer.

图2是扫描镜运动高精度动态测角方法数据处理流程图。Fig. 2 is a flow chart of data processing of the high-precision dynamic angle measurement method for scanning mirror movement.

具体实施方式detailed description

下面结合举例对本发明的具体实施作详细说明。The specific implementation of the present invention will be described in detail below in conjunction with examples.

如图1和图2所示,本发明“一种扫描镜运动高精度动态测角方法”由陀螺测角仪及其计算机系统组成的测角装置来具体实施。As shown in Fig. 1 and Fig. 2, "a high-precision dynamic angle measurement method for scanning mirror motion" of the present invention is embodied by an angle measurement device composed of a gyro goniometer and a computer system.

首先将高精度激光陀螺及其固定工装组成的陀螺测角仪1安装并固定在扫描镜转轴上;扫描机构框架2支承着扫描镜及其转轴3,扫描控制器驱动力矩电机及扫描镜运动,感应同步器4作为角度反馈元件。扫描控制器根据目标角度位置的要求发送运动控制指令,扫描镜在扫描控制器的控制下作闭环运动。由于陀螺测角仪与转轴固联,使得陀螺测角仪与扫描机构转动部分在力矩电机的驱动下一起作连续、缓慢的匀速运动,可以认为陀螺测角仪和感应同步器的运动角度值是相同的。陀螺与感应同步器同步进行角度采样,陀螺测角数据经过电路处理后,实时发送到陀螺测试计算机;感应同步器测角数据经过电路处理后,实时发送到扫描控制器中。将感应同步器的角度数据和激光陀螺的角度数据用合适的算法进行比对和校正,并将校正结果带入扫描控制器获得的感应同步器组件测角反馈数据,对感应同步器组件测角反馈数据进行校正,并重新用于扫描镜指向反馈控制,从而实现了扫描镜指向高精度静态角度测试和校正,并明显提高了扫描镜指向精度。First, the gyro goniometer 1 composed of a high-precision laser gyro and its fixed tooling is installed and fixed on the rotating shaft of the scanning mirror; the scanning mechanism frame 2 supports the scanning mirror and its rotating shaft 3, and the scanning controller drives the torque motor and the scanning mirror to move. The induction synchronizer 4 is used as an angle feedback element. The scanning controller sends motion control instructions according to the requirements of the target angular position, and the scanning mirror performs closed-loop movement under the control of the scanning controller. Since the gyro goniometer is fixedly connected to the rotating shaft, the gyro goniometer and the rotating part of the scanning mechanism are driven by the torque motor to move continuously and slowly at a uniform speed. It can be considered that the movement angle value of the gyro goniometer and the induction synchronizer is identical. The gyro and the induction synchronizer perform angle sampling synchronously, and the angle measurement data of the gyro are sent to the gyro test computer in real time after being processed by the circuit; the angle measurement data of the induction synchronizer are processed by the circuit, and then sent to the scanning controller in real time. Compare and correct the angle data of the induction synchronizer and the angle data of the laser gyroscope with a suitable algorithm, and bring the correction result into the angle measurement feedback data of the induction synchronizer component obtained by the scan controller, and measure the angle of the induction synchronizer component The feedback data is corrected and reused for the scanning mirror pointing feedback control, thus realizing the high-precision static angle test and correction of the scanning mirror pointing, and significantly improving the pointing accuracy of the scanning mirror.

Claims (1)

1.一种扫描镜指向高精度静态测角方法,所述方法由陀螺测角仪和主机系统组成的测试装置来实现;所述的测试装置包括陀螺测角仪、感应同步器及其处理电路、扫描镜及其机构组件、扫描控制器和控制计算机;其特征在于方法如下:1. A scanning mirror points to a high-precision static angle measurement method, and the method is realized by a test device composed of a gyro goniometer and a host system; the test device includes a gyro goniometer, an inductive synchronizer and a processing circuit thereof , a scanning mirror and its mechanism components, a scanning controller and a control computer; it is characterized in that the method is as follows: 将陀螺测角仪安装并固定在扫描镜转轴上,在扫描控制器的作用下,使得陀螺测角仪与扫描镜在力矩电机的驱动下同步作低于1°/s的连续缓慢地匀速运动,从而实现该种速度条件下的扫描镜运动角度数据;由于速度非常低,感应同步器高频谐波误差影响可以忽略,可以用动态测试数据直接作为静态测试结果,从而实现扫描镜指向高精度、高密度和快速测量;测量时,感应同步器组件测角数据以及激光陀螺的测角数据均传至外围计算机,由计算机对二组测角数据进行比对,并通过合适的算法对感应同步器组件测角数据进行校正。经过校正后的感应同步器组件测角数据被重新用于闭环控制,明显提高了扫描镜指向精度。Install and fix the gyro goniometer on the rotating shaft of the scanning mirror, and under the action of the scanning controller, the gyro goniometer and the scanning mirror are driven by the torque motor synchronously and continuously and slowly at a uniform speed below 1°/s , so as to realize the motion angle data of the scanning mirror under this speed condition; because the speed is very low, the influence of the high-frequency harmonic error of the inductive synchronizer can be ignored, and the dynamic test data can be directly used as the static test result, so as to realize the high precision of the scanning mirror pointing , high-density and fast measurement; during measurement, the angle measurement data of the induction synchronizer component and the angle measurement data of the laser gyroscope are transmitted to the peripheral computer, and the computer compares the two sets of angle measurement data, and synchronizes the induction through a suitable algorithm The angle measurement data of the sensor component is corrected. The corrected angle measurement data of the inductosynchronizer assembly is reused for closed-loop control, which significantly improves the pointing accuracy of the scanning mirror.
CN201710563629.0A 2017-07-12 2017-07-12 A high-precision static angle measurement method for scanning mirror pointing Active CN107167135B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710563629.0A CN107167135B (en) 2017-07-12 2017-07-12 A high-precision static angle measurement method for scanning mirror pointing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710563629.0A CN107167135B (en) 2017-07-12 2017-07-12 A high-precision static angle measurement method for scanning mirror pointing

Publications (2)

Publication Number Publication Date
CN107167135A true CN107167135A (en) 2017-09-15
CN107167135B CN107167135B (en) 2020-10-13

Family

ID=59823885

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710563629.0A Active CN107167135B (en) 2017-07-12 2017-07-12 A high-precision static angle measurement method for scanning mirror pointing

Country Status (1)

Country Link
CN (1) CN107167135B (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110113853A1 (en) * 2009-11-13 2011-05-19 Sick Sensors Ltd Method for calibrating a rotational angle sensor
CN102879032A (en) * 2012-09-25 2013-01-16 中国科学院西安光学精密机械研究所 Dynamic measuring device for angle measurement precision
CN104697436A (en) * 2015-02-15 2015-06-10 中国科学院西安光学精密机械研究所 A Method for Analyzing the Error Model of Circular Inductor Synchronizer Based on Fourier Series
CN105091844A (en) * 2014-05-07 2015-11-25 中国航空工业第六一八研究所 High-precision dynamic angle measuring device and method

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110113853A1 (en) * 2009-11-13 2011-05-19 Sick Sensors Ltd Method for calibrating a rotational angle sensor
CN102879032A (en) * 2012-09-25 2013-01-16 中国科学院西安光学精密机械研究所 Dynamic measuring device for angle measurement precision
CN105091844A (en) * 2014-05-07 2015-11-25 中国航空工业第六一八研究所 High-precision dynamic angle measuring device and method
CN104697436A (en) * 2015-02-15 2015-06-10 中国科学院西安光学精密机械研究所 A Method for Analyzing the Error Model of Circular Inductor Synchronizer Based on Fourier Series

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
孙玉良: "高控制精度的扫描系统研究", 《中国优秀硕士学位论文全文数据库》 *

Also Published As

Publication number Publication date
CN107167135B (en) 2020-10-13

Similar Documents

Publication Publication Date Title
CN104101361B (en) Inertial platform angle sensor error calibration compensation method
TWI504861B (en) Calibration device for encoder positioning and calibration method thereof
CN108759657B (en) A kind of automatic detection device and method of induction synchronizer angle
JP2016001982A (en) Apparatus and method for compensating resolver position error
CN108759658B (en) An Analysis and Compensation Method of Induction Synchronizer Angle Measurement Error
JP2016090434A (en) Shape measuring device and shape measuring method
CN111288952B (en) Automatic centering adjusting tool for rotary transformer
CN110160436A (en) A kind of error measurement method and measuring device of linear displacement transducer
CN109186658A (en) A kind of conductive plastic potentiometer rating test device and method
CN114012719A (en) Zero calibration method and system for six-axis robot
CN108469849A (en) A kind of random angular oscillation control method
CN106557092B (en) The adjusting method of the practical rotation angle and feedback angle corresponding relationship of electric steering engine
CN102607598B (en) Method and device for production of gyroscope hardware
WO2015083275A1 (en) Trajectory measurement device, numerical control device, and trajectory measurement method
CN208751603U (en) Encoder corrects system
CN204595620U (en) A kind of visual apparatus is as the parallel connection platform follow-up control apparatus of sensor
CN103591967A (en) Optical Chirp Signal Generation Method for Optical Servo System Spectrum Curve Test
CN107167135B (en) A high-precision static angle measurement method for scanning mirror pointing
CN105571811A (en) Method of measuring aircraft actual attack angle value in wind tunnel experiment
CN107389051B (en) A high-precision dynamic angle measurement method for scanning mirror motion
CN101424543B (en) Measuring set and method of gyroscope phase response
CN102830249A (en) Method for identifying transfer function of acceleration transducer
CN106643469A (en) On-orbit comprehensive compensation implementation method of inductosyn error calibration
CN108845594A (en) Vibration harmonics iteration control method based on transmission function
CN107742997A (en) Dual-axis indexing mechanism control system, control method and strapdown inertial group self-calibration method

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant