| 1. | Research on inertial measurement unit of high rotation vehicle
高转速载体惯性测量组合研究 |
| 2. | Precision - calibration for low cost inertial measurement units
一种低精度惯性测量单元的精确标定技术 |
| 3. | The acceleration sensor is the key basic component for imu ( inertial measurement unit ) to sense and analysis the motion information
加速度传感器是一种十分重要的力学量传感器，是惯性测量组合（ imu ）系统的基础元件之一。 |
| 4. | Through the correlative theoretic analysis and simulation , this algorithm can be used to finish the initial alignment of the low cost inertial measurement unit
理论分析和仿真计算表明，这种算法仅受组合系统自身硬件条件的约束，可以较好地应用于组合系统中低成本惯性单元的初始对准。 |
| 5. | The kinematic model of inertial measurement unit ( imu ) with mdrlg has been analyzed theoretically , the coning drift caused by dithering has been calculated , and some problems including the assembly of inertial sensors have been discussed
本文对机抖激光陀螺捷联惯导系统惯性测量单元的运动模型进行了理论分析,对抖动作用下的圆锥漂移进行了理论计算,对仪表安装形式等问题进行了探讨。 |
| 6. | The cox report says , " china great wall industry corp . determined that the root cause of the failure was a deterioration in the gold - aluminum wiring connections within a power amplifier for the follow - up frame torque motor in the inertial measurement unit
《考克斯报告》称， “中国长城工业总公司确定失败的根本原因，是惯性测量装置中，随动架转矩电动机功率放大器内部金铝合金线路连接处破损。 |
| 7. | The micro inertial acceleration sensor is the key basic component for mimu ( micro inertial measurement unit ) , which will be more and more applied in future . the research of mems inertial accelerometer is of great scientific significance
Mems惯导加速度传感器是微惯性测量组合( mimu )的核心部件,在军用航空和民用相关领域有重要的发展前景,研究高性能的mems惯导加速度计已成为世界各国的研究热点。 |
| 8. | 2 . the necessity and difficulty are discussed for the in - place calibration of inertial measurement unit being subjected to the vibration , shock and acceleration induced by the host vehicles . a new in - place calibration method based on the fixed axe rotation constraint is presented
2 、讨论了载体经受振动、冲击和加速度的情况下，惯性测量组合参数现场标定的必要性和技术难点，提出了基于定轴转动约束的现场标定算法。 |
| 9. | Based on gyro - free inertial navigation theory while revolve about mems accelerometer and dsp , this dissertation mainly focuses on the research of gyro - free inertial measurement unit for shell flight path measurement - the first step for guidance
本文以无陀螺惯性导航理论为基础,以微机械加速度传感器、高性能dsp处理器为核心,研制应用于某型炮弹的无陀螺惯性测量系统,该系统将用于炮弹飞行轨迹的测量,是实现炮弹制导的第一步。 |
| 10. | ( 4 ) applying measurement noise automatic weighting kalman filter to the guidance of line - guidance torpedo , we compromised target information and torpedo information , which in turn come from sonar of guidance station and inertial measurement units of torpedo
( 4 )将多传感器量测噪声自动加权卡尔曼滤波应用在线导鱼雷制导中，融合来自制导站声纳测量到的目标信息和来自鱼雷惯性测量组件的鱼雷位置和姿态等信息进行了仿真研究。 |
