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Inertial reference unit

About: Inertial reference unit is a research topic. Over the lifetime, 1306 publications have been published within this topic receiving 22068 citations. The topic is also known as: IRU.


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Journal ArticleDOI
01 Mar 1958
TL;DR: By measuring forces and moments that constrain a body of known inertial characteristics to move with a vehicle it is possible to determine acceleration in a set of specified axes and hence change in velocity and position.
Abstract: By measuring forces and moments that constrain a body of known inertial characteristics to move with a vehicle it is possible to determine acceleration in a set of specified axes and hence change in velocity and position. The principles of this method of navigation, known as inertial navigation, are outlined, and it is shown that the many possibilities of a practical realization can all be expressed in terms of a single block schematic of a computer which corrects for the expected variations in the specific force of gravity as a function of position and time.The magnitude of the problem of designing suitable gyroscopes and accelerometers is discussed, and the effect is calculated of certain errors in the components. Means for combining inertial navigation with radio navigation aids are outlined, and it is shown that these give an effective memory over periods in which the radio aid may be inoperative, a heavy filtering of the radio-aid output without introducing lag and loss of information, and interpolation between outputs of a low-data-rate system. The performance requirements for gyroscopes and accelerometers to obtain this can be much less stringent than for pure inertial navigation.

4 citations

DOI
01 Oct 1985
TL;DR: The performance requirements of a gyro for one nautical mile per hour aircraft IN system are derived and the difference between `gimballed?
Abstract: A simple explanation of inertial navigation is presented. The difference between `gimballed? and `strapdown? systems is explained. The performance requirements of a gyro for one nautical mile per hour aircraft IN system are derived.

4 citations

Proceedings ArticleDOI
21 Dec 2013
TL;DR: A motion capture system based on inertial sensors mainly composed of the inertial sensor unit and real-time monitoring unit on PC and adaptive Kalman Filter algorithm is used to estimate the body gesture.
Abstract: The motion capture technologies have been widely used in the following areas: human movement science, human-computer interaction and control, medical analysis, film, game production, and etc. This paper presented a motion capture system based on inertial sensors. The system is mainly composed of the inertial sensor unit and real-time monitoring unit on PC. Meanwhile, Sensor units exchange data with PC through BSN (body sensor network). One sensor measurement unit contains a three-axis gyroscope, a three-axis accelerometer, a three-axis magnetometer and a network communication unit. The inertial sensor units are installed on the different parts of body. In the system, the inertial sensor data are collected, and then adaptive Kalman Filter algorithm is used to estimate the body gesture. The Experiments show that this way have some advantages such as: high precision, dynamic, and almost no drift. Furthermore, the data can be changed smoothly.

4 citations

Patent
29 Nov 1963

4 citations


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Performance
Metrics
No. of papers in the topic in previous years
YearPapers
202314
202221
20211
20202
20193
20189