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- The algorithm can meet the precision requirement in application,and is effective and feasible in error compensation of strapdown inertial measurement system. 该算法能够满足应用的精度要求,对捷联惯性测量系统的误差补偿有一定的有效性和可行性。
- An Algorithm of Inertial Measurement System 惯性测量系统的一种算法
- Replacement Inertial Measurement System 替换惯性测量系统
- Three-Axis Inertial Measurement System 三轴惯性测量系统
- A system which only uses accelerometers but has not gyro is called Gyroscope Free Strap-down Inertial Measure System (GFSIM). 无陀螺捷联惯性测量系统是把加速度计直接安装在载体上，舍弃陀螺仪的捷联惯性测量系统。
- Advanced Inertial Measurement System 高级惯性测量系统
- Evaluation of Test Valid Period of Inertial Measurement System 惯性测量系统测试有效期评估方法研究
- Design of an Inertial Measurement System Based on Accelerometers and Gyro-Free 基于加速度计的无陀螺惯性测量系统设计
- rate strapdown inertial measurement system 速率捷联惯性测量系统
- The Design and Experiment of A Gyro-free Inertial Measurement System 无陀螺惯性测量系统的设计与实验
- The Error Compensation Investigation of Strapdown Inertial Measurement System 捷联惯性测量系统的误差补偿研究
- Micro Inertial Measurement System and its Application 微型惯性测量系统及其应用
- Hardware Design for Cannon Shell Inertial Measurement System Based on Accelerometers 基于加速度计的炮弹惯性测量硬件系统设计
- An Intelligent Solvent Mass Measurement System. 智能溶剂质量测量系统。
- Nanospec Film Thickness Measurement System. 薄膜测厚仪,用于测量薄膜厚度。
- Error analysis of the measurement system is given. 给出了次测量系统的误差分析。
- The errors of Inertial Measurement Unit(IMU) affect the accuracy of the system a lot and also determine the impact point error of missiles directly. 弹上惯测组件(IMU)的误差是影响系统导航精度的重要因素,并直接决定导弹的落点偏差。
- A new nine-accelerometer configuration of non-gyro inertial measurement unit(NGIMU) is presented,with its experiment system built. 提出了九加速度计无陀螺惯性测量组合(NGIMU)配置方案,并建立了其实验系统。
- Verify the veracity and reliability of measurement system. 确认测量系统的准确性和可靠性。
- The errors of Inertial Measurement Unit (IMU) affect the accuracy of the system a lot and also determine the impact point error of missiles directly. 摘要弹上惯测组件(IMU)的误差是影响系统导航精度的重要因素，并直接决定导弹的落点偏差。
