Feasibility Study of Multi Inertial Measurement Unit
نویسندگان
چکیده
منابع مشابه
Study of Inertial Measurement Unit Sensor
This paper contains the study about the inertial measurement unit (IMU) sensor. The study is about the types available in markets and also some research on IMU. In this paper also included the uncertainty of some IMU been used and comparison between some IMU manufacturers. Then the combination of IMU with GPS can provide more effective result for navigation, guidance and controlling system for ...
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During the last few years microminiaturized inertial sensors were introduced in many applications. Their small size, low power consumption, rugged construction open doors to many areas of implementation. The main drawback of these sensors is the influence of different type of errors, leading to an unavoidable wrong position and orientation estimation. In the paper a simulator of Inertial Measur...
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The Department of Mechanical Engineering and Avionics Engineering Center at Ohio University are developing an electromechanical system for the calibration of an inertial measurement unit (IMU) using global positioning system (GPS) antennas. The GPS antennas and IMU are mounted to a common platform to be oriented in the angular roll, pitch, and yaw motions. Vertical motion is also included to te...
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We have developed a compact, six degree-of-freedom inertial measurement unit for user interfaces. The system uses three axes each of gyroscopes and accelerometers for full 6-axis inertial sensing, and transmits data wirelessly to an external basestation, providing full state updates at 75 Hz. Circuitry for proximity sensing and ID transmission through capacitive coupling was also constructed. W...
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Unmanned Aerial Vehicles (UAVs) are being deployed in a vast variety of military, civilian, industrial and agricultural applications. Dynamics modeling is an essential step towards designing autonomous controllers for UAV systems. The dynamics modeling on the other hand requires accurate records of the UAVs motion states during real flight tests, this is usually achieved using Inertial Measurem...
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ژورنال
عنوان ژورنال: Proceedings
سال: 2019
ISSN: 2504-3900
DOI: 10.3390/ecsa-6-06582