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Proceedings ArticleDOI

An historical perspective on inertial navigation systems

Daniel Tazartes
- pp 1-5
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TLDR
In the past fifty years, significant evolutionary and revolutionary changes have taken place in the designs of inertial sensors and systems, including the progression from fluid-filled to dry instruments and the transition from mechanically complex stabilized inertial platforms to computationally intensive strapdown systems.
Abstract
Inertial navigation provides a unique ability to know where one has been, where one is currently, and where one is going, given only a starting position. The laws of physics permit the sensing of dynamic motion without external information, making inertial systems impervious to jamming, masking, or spoofing. Measurements of six degrees of freedom are required - three linear accelerations, and three angular rates - to fully propagate the velocity, position, and orientation of the system. The first inertial sensors are traced to the early 19th century and specialized inertial guidance systems appeared in the 1940s, yet inertial navigation systems did not become commonplace until the 1960s. This is largely due to the fact that requirements for navigation accuracy inertial sensors - accelerometers and gyroscopes - are very challenging. In the past fifty years, significant evolutionary and revolutionary changes have taken place in the designs of inertial sensors and systems. These include the progression from fluid-filled to dry instruments and the transition from mechanically complex stabilized inertial platforms to computationally intensive strapdown systems. Gyroscopes have evolved from large mechanical devices to highly refined precision mechanical sensors. Optical rotation sensors such as the ring laser gyro and the fiber optic gyro have enabled new system designs and capabilities. Coriolis vibratory gyroscopes such as the hemispherical resonator gyro are capable of extreme accuracy and reliability; new opportunities for miniaturizing these types of sensors will lead to new classes of accuracy for inertial navigation systems. Advanced gyroscope technologies such as the nuclear magnetic resonance gyroscope which uses atomic spin to detect rotation have already been demonstrated to achieve navigation accuracy requirements. Cold atom technologies may also provide the opportunity for very high accuracy accelerometers and gyroscopes in the future. Inertial navigation technologies and applications of the past, present, and future are discussed.

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A Self-Calibration Method for Accelerometer Nonlinearity Errors in Triaxis Rotational Inertial Navigation System

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Proceedings ArticleDOI

Trends in inertial sensors and applications

TL;DR: Observations of the historical trends in inertial sensing and devices will be provided and a group of promising future inertial sensor technologies and potentially new applications is discussed.
References
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Journal ArticleDOI

Atomic Sensors – A Review

TL;DR: In this article, the basic physics and instrumentation issues related to high-performance physical and inertial sensors based on atomic spectroscopy are discussed, with a focus on precision sensing of electromagnetic and gravitational fields.
Journal ArticleDOI

Characterization and limits of a cold-atom Sagnac interferometer

TL;DR: In this paper, the authors presented the full evaluation of a cold-atom gyroscope based on atom interferometry and demonstrated that the acceleration noise can be efficiently removed from the rotation signal, allowing them to reach the fundamental limit of the quantum projection noise for short term measurements.
Proceedings ArticleDOI

Nuclear Magnetic Resonance Gyroscope: For DARPA's micro-technology for positioning, navigation and timing program

TL;DR: In this article, the Nuclear Magnetic Resonance Gyro under development by Northrop Grumman Corporation is described and a review of the completed phases is presented, and the current state of development and progress in phase 4 is discussed.
Journal ArticleDOI

Milli-HRG inertial navigation system

TL;DR: The Precision Pointing System (PPS) as mentioned in this paper utilizes a new golf-ball sized milli-HRG (mHRG) that is based on the current HRG 130P production gyro design used in extremely accurate space pointing systems.
Journal ArticleDOI

History of Inertial Navigation

W. Wrigley
- 01 Mar 1977 - 
TL;DR: The development of inertial navigation systems began in the United States in the late 1940's and early 1950's by the M.I.T. Instrumentation Laboratory, Northrop and Autonetics under Air Force sponsorship as mentioned in this paper.
Trending Questions (1)
How does inertial navigation differ from GPS-based navigation systems?

Inertial navigation relies on internal sensors for position, impervious to external interference, while GPS uses satellite signals for positioning, susceptible to jamming.