作者：冷贺彬1,2, 朱平1,2
作者单位：1. 中北大学 电子测试技术国家级重点实验室, 山西 太原 030051;
2. 中北大学仪器与电子学院, 山西 太原 030051
关键词：微小型稳定平台;惯性姿态测量;指向精度;无磁转台
摘要：
传统的棱镜光学测量方法大多针对大型转台和云台，微小型稳定平台体积小无法安装光学棱镜，且光学测量成本高，为解决传统测量方法无法应用于微小型稳定平台测试中的问题，提出采用无磁转台测量方法。该文利用0.05°高精度无磁转台提供不同倾角姿态参考，采集惯组姿态数据和稳定平台控制码盘数据，分析得到稳定平台角度测量精度、角度指向精度和角度稳定精度。为验证该方法的可行性，搭建微小型稳定平台样机和上位机数据采存软件。测得自制稳定平台姿态测量误差0.6°，角度指向误差0.73°，角度稳定误差0.1°。该测量方法对微小型稳定平台的性能指标测量方面具有广泛的应用前景。
Test method for performance index of micro-stable platform based on non-magnetic turntable
LENG Hebin1,2, ZHU Ping1,2
1. Science and Technology on Electronic Test & Measurement Laboratory, North University of China, Taiyuan 030051, China;
2. School of Instrument and Electronics, North University of China, Taiyuan 030051, China
Abstract: Traditional prism optical measurement methods mostly aim at large turntable and cloud platform. The small size of micro-stable platform can not install optical prism, and the cost of optical measurement is high. In order to solve the problem that traditional measurement methods can not be applied to the testing of micro-stable platform, a non-magnetic turntable measurement method is proposed. In this paper, the 0.05 degree high precision non-magnetic turntable is used to provide reference for different tilt angles. The attitude data of INU and the control code disk data of the stabilized platform are collected, and the angle measurement accuracy, angle pointing accuracy and angle stabilization accuracy of the stabilized platform are analyzed. In order to verify the feasibility of this method, a prototype of micro stabilized platform and PC data storage software are built. The attitude measurement error of the self-made stabilized platform is 0.6 degree, the angle pointing error is 0.73 degree and the angle stabilization error is 0.1 degree. The measurement method has wide application prospects for the measurement of the performance index of small and stable platforms.
Keywords: miniature stabilized platform;inertial attitude measurement;pointing precision;non-magnetic turntable
2019, 45(6):42-45,53 收稿日期: 2018-10-22;收到修改稿日期: 2018-11-19
基金项目:
作者简介: 冷贺彬(1993-),男,安徽阜阳市人,硕士研究生,专业方向为MEMS惯性姿态测量
参考文献
[1] 许江宁, 朱涛, 卞鸿巍. 航空摄影陀螺稳定平台[J]. 仪器仪表学报, 2007(5):551-557
[2] 惯性技术测试设备主要性能测试方法:GJB 1801-1993[S]. 1993.
[3] NIU X J, LI Y, ZHANG H P, et al. Fast thermal calibration of low-grade inertial sensors and inertial measurement units[J]. Sensors, 2013, 13(9):12192-12217
[4] 赵代弟.MARG姿态测量系统抗干扰算法研究[D]. 太原:中北大学,2015.
[5] 施峥嵘.车载设备视轴稳定与跟踪技术研究[D].南京:东南大学, 2006.
[6] 赵灵.基于MEMS陀螺仪的稳定平台关键技术研究[D].南京:南京理工大学, 2012.
[7] HIKERT J M. Inertially stabilized platform technology concepts and principles[J]. Control Systems, IEEE, 2008, 28(1):26-46
[8] MASTEN M K. Inertially stabilized platforms for optical imaging systems[J]. Control Systems, IEEE, 2008, 28(1):47-64
[9] 李锡广.基于MEMS惯性器件的两轴稳定平台研究[D].太原:中北大学, 2014.
[10] 田晓春, 李杰, 范玉宝, 等. 基于FPGA的MEMS陀螺仪SAR150实时数据采集系统设计[J]. 计算机测量与控制, 2012, 20(11):3107-3112
[11] 陈国华, 王刚. 基于ADIS16255 MEMS芯片陀螺仪的应用研究[J]. 中国惯性技术学报, 2008, 16(4):480-483
[12] 高云红, 姜森, 赵丁, 等. 基于虚拟仪器的MEMS陀螺仪静态性能测试系统设计[J]. 自动化应用, 2013(11):14-16
