2005
DOI: 10.1088/0957-0233/16/11/024
|View full text |Cite
|
Sign up to set email alerts
|

Earth rotation measurement with micromechanical yaw-rate gyro

Abstract: The direct measurement of the Earth's rotation rate by means of a micromechanical yaw-rate gyroscope is difficult to achieve due to the considerable parameter variations of the current state-of-the-art sensors of this type. This paper outlines and applies a model of the external factors' effect on the sensor measurement via a method for their compensation through a mechanical change in the sensor's orientation. This allows the determination of a value such as the Earth's rotation rate, which is at the limit of… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1

Citation Types

0
15
0

Year Published

2007
2007
2019
2019

Publication Types

Select...
8

Relationship

0
8

Authors

Journals

citations
Cited by 15 publications
(15 citation statements)
references
References 4 publications
0
15
0
Order By: Relevance
“…The scale factor of the prototype IFOG was calculated as 13.83 ( • /h)/mV, corresponding to a sensitivity of 72 µV/( • /h), and the repeatability in scale factor was 0.73%. Considering the earth rotation rate of 4.178074 × 10 −3 ( • /s), corresponding to 15.041 ( • /h) according to WGS84 (World Geodesic System) (Arnaudov and Angelov 2005), the bias stability attained on the prototype IFOG is close to 1 ( • /h) limit of tactical aimed missiles. NE of 0.001 ( • /h)/Hz 1/2 for the designed IFOG prototype in sampling duration of 1 sec was the ultimate rotation rate which can be sensed.…”
Section: Resultsmentioning
confidence: 92%
“…The scale factor of the prototype IFOG was calculated as 13.83 ( • /h)/mV, corresponding to a sensitivity of 72 µV/( • /h), and the repeatability in scale factor was 0.73%. Considering the earth rotation rate of 4.178074 × 10 −3 ( • /s), corresponding to 15.041 ( • /h) according to WGS84 (World Geodesic System) (Arnaudov and Angelov 2005), the bias stability attained on the prototype IFOG is close to 1 ( • /h) limit of tactical aimed missiles. NE of 0.001 ( • /h)/Hz 1/2 for the designed IFOG prototype in sampling duration of 1 sec was the ultimate rotation rate which can be sensed.…”
Section: Resultsmentioning
confidence: 92%
“…It is also commonly referred to as a two-point gyrocompassing [10] since it mitigates additive bias errors through the differential, two position azimuth measurement.…”
Section: B Maytagging For North-findingmentioning
confidence: 99%
“…The common approaches to reduce the effect of bias drift on azimuth measurements include "carouseling" [6] and "maytagging" [10], [11]. We propose to tackle the problem of MEMS gyrocompassing by using the recently developed Quadruple Mass Gyroscope (QMG) [12], with the performance enhanced by Quality (Q) factors of 1.2 million, in drive-and sensemodes, and Allan deviation bias instability of 0.2°/hr [13].…”
mentioning
confidence: 99%
“…Maytagging has been widely applied in various methods of north finding angle detection, such as the two-point method, four-point method, and multiposition method. (6)(7)(8) It is simple to operate and is widely employed in practical applications. However, this method will increase the error caused by the rate random walk (RRW), which conflicts with the angular random walk (ARW).…”
Section: Introductionmentioning
confidence: 99%