Novel rotation scheme for dual-axis rotational inertial navigation system based on body diagonal rotation of inertial measurement unit

نویسندگان

چکیده

Abstract Traditional rotational inertial navigation systems are based on rotation around one or two sensitive axes of sensors. However, as the and sensors lie along same direction, it is difficult to modulate relative error sensor in axial direction. This paper proposes a dual-axis scheme diagonal measurement unit (IMU) body. The selects body three orthogonal IMU horizontal axis, sets vertical axis this axis. As oriented different directions, at any moment rotation, errors directions can all be modulated, especially installation error. First, mathematical model established. On basis, coordinate transformation relationship equations derived, propagation characteristics obtained. Finally, comprehensive system tested. Under conditions, latitude reduced from 0.1089 nautical miles/72 h traditional 0.0368 h, longitude 0.3587 0.1332 h. These results verify effectiveness proposed scheme. method rotating also exhibits certain advantages when applied other schemes.

برای دانلود رایگان متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Precision and Reliability Incensement of Inertial Navigation System with Rotation and Redundancy

Precision and reliability are two main performance characteristic in low-cost Inertial Navigation System(INS). Increase of precision in low-cost INS without auxiliary sensors is main challenge. Bias instability leads to position drift error in inertial navigation system. In addition, fault occurrence makes the sensor reliability is decreased. Rotation of Inertial Measurement Unit(RIMU) and use ...

متن کامل

Accurate Compensation of Attitude Angle Error in a Dual-Axis Rotation Inertial Navigation System

In the dual-axis rotation inertial navigation system (INS), besides the gyro error, accelerometer error, rolling misalignment angle error, and the gimbal angle error, the shaft swing angle and the axis non-orthogonal angle also affect the attitude accuracy. Through the analysis of the structure, we can see that the shaft swing angle and axis non-orthogonal angle will produce coning errors which...

متن کامل

Attitude Heading Reference System Using MEMS Inertial Sensors with Dual-Axis Rotation

This paper proposes a low cost and small size attitude and heading reference system based on MEMS inertial sensors. A dual-axis rotation structure with a proper rotary scheme according to the design principles is applied in the system to compensate for the attitude and heading drift caused by the large gyroscope biases. An optimization algorithm is applied to compensate for the installation ang...

متن کامل

Adaptive Fusion of Inertial Navigation System and Tracking Radar Data

Against the range-dependent accuracy of the tracking radar measurements including range, elevation and bearing angles, a new hybrid adaptive Kalman filter is proposed to enhance the performance of the radar aided strapdown inertial navigation system (INS/Radar). This filter involves the concept of residual-based adaptive estimation and adaptive fading Kalman filter and tunes dynamically the fil...

متن کامل

Intelligent Calibration Method of low cost MEMS Inertial Measurement Unit for an FPGA-based Navigation System

Based on a small, lightweight, low-cost high performance inertial Measurement Units(IMU), an effective calibration method is implemented to evaluate the performance of Micro-Electro-Mechanical Systems(MEMS) sensors suffering from various errors to get acceptable navigation results. A prototype development board based on FPGA, dual core processor’s configuration for INS/GPS integrated navigation...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

ژورنال

عنوان ژورنال: Measurement Science and Technology

سال: 2022

ISSN: ['0957-0233', '1361-6501']

DOI: https://doi.org/10.1088/1361-6501/ac6e2c