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用于水下ROV控制的姿态融合技术研究 被引量:1

Research on Attitude Fusion Technique for Underwater ROV Control
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摘要 出于对海洋探索的目的,本文研究设计了一个低功耗、体积小、准确度高的实时性好的水下ROV空间姿态控制系统。系统硬件部分主要由陀螺仪、加速度计以及能耗比较高的ARM-M3内核处理器及相关的外围功能电路组成。硬件部分负责从传感器获取三轴的姿态数据并通过姿态融合算法得出空间角,并通过相关接口上传至上位机观察处理,根据测试结果证明本文设计的基于惯性传感器的姿态检测系统能够用于对水下ROV的姿态控制。 For the purpose of exploring the seas, a low-power, small size and high accuracy real-time underwater ROV space attitude control system is designed. System hardware is mainly composed of three-axis gyroscope, three-axis accelerometer and low-power ARM-M3 core processor and related peripheral functional circuit. The hardware part is responsible for obtaining the three-axis attitude data from the sensor and obtaining the spatial angle through the attitude fusion algorithm, and uploading to the upper computer for observation and processing through the relevant interfaces. Test results show that the inertial sensor-based attitude detection system can be used Attitude control of underwater ROV.
作者 裴国栋 温亚楠 朱莉莉 Pei Guodong;Wen Yanan;Zhu Lili(Qingdao Academy for Opto-electronics Engineering, Qingdao266019, Shandong, China)
出处 《船电技术》 2018年第4期56-58,共3页 Marine Electric & Electronic Engineering
关键词 水下ROV 姿态检测 惯性导航 数据融合 ROV attitude detection inertial navigation data fusion
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  • 1高钟毓,牛小骥,郭美凤.Quaternion-Based Kalman Filter for Micro-machined Strapdown Attitude Heading Reference System[J].Chinese Journal of Aeronautics,2002,15(3):171-175. 被引量:18
  • 2[1]Wilson J R.Mini technologies for major impact [J].America Aerospace,1998,36 (5):36-42.
  • 3[2]Geen J.New iMEMS angular-rate-sensing; gyroscope [ R ].Analog Dialogue ,2003:37-03.
  • 4[3]Analog Devices Inc..±300°/s single chip yaw rate gyro with signal conditioning ADXRS300 [Z].29973351ADXRS300_a,2003.
  • 5[4]Waszak M R,Davidson J B.Simulation and flight control of an aeroelastic fixed wing micro aerial vehicle[R].AIAA 2002-4875,2002.
  • 6[5]Bacon B J and Ostroff A J.Reconfigurable flight control using nonlinear dynamic inversion with a special accelerometer implementation [R].AIAA 2000-4565,2000.
  • 7[6]Snell S A,Enns D F,and Garrard W L.Nonlinear control of a super maneuverable aircraft [ R ].AIAA 8-3486,1989.
  • 8[1]Lu G, Cannon M E, Lachapelle G, Kielland P. Attitude determination using dedicated and nondedicated multiantenna GPS Sensors[J]. IEEE Transactions on Aerospace and Electronic Systems, 1994, (30): 1053-1058.
  • 9[2]Yaakov O, Landis M F. Spacecraft attitude/rate estimation using vector-aided GPS observations IEEE Transactions on Aerospace and Electronic Systems, 1999, 35 (3): 1019 - 1032.
  • 10[3]Hayward R, Marchick A, Powell J D. Single baseline GPS based attitude heading reference system (AHRS) for aircraft applications[J]. American Control Conference, 1999, (5): 3655 - 3659.

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