Study on attitude measurement in gyro-free inertial navigation system

Xiaoli Wang; Xun Zhou

doi:10.1109/MACE.2011.5987989

Study on attitude measurement in gyro-free inertial navigation system

Xiaoli Wang^*, Xun Zhou

^*Corresponding author for this work

Academy of Armored Force Engineering China

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

2 Citations (Scopus)

Abstract

Through analysing the measurement priniple of the accelerometer-based gyro-free inertial navigation system, this paper designed a kind of easy to engineering realization of 9 accelerometer configuration scheme, studied attitude measurement principle based on this configuration.Through analysing the acceleration in the carrier movement, obtained angular velocity and linear acceleration.

Original language	English
Title of host publication	2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Proceedings
Pages	4432-4434
Number of pages	3
DOIs	https://doi.org/10.1109/MACE.2011.5987989
Publication status	Published - 2011
Externally published	Yes
Event	2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Inner Mongolia, China Duration: 15 Jul 2011 → 17 Jul 2011

Publication series

Name	2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Proceedings

Conference

Conference	2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011
Country/Territory	China
City	Inner Mongolia
Period	15/07/11 → 17/07/11

Keywords

Acceleromete
Attitude measurement
GFSINS

Access to Document

10.1109/MACE.2011.5987989

Cite this

Wang, X., & Zhou, X. (2011). Study on attitude measurement in gyro-free inertial navigation system. In 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Proceedings (pp. 4432-4434). Article 5987989 (2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Proceedings). https://doi.org/10.1109/MACE.2011.5987989

@inproceedings{149c29c724cb4633b15d752d1250513f,

title = "Study on attitude measurement in gyro-free inertial navigation system",

abstract = "Through analysing the measurement priniple of the accelerometer-based gyro-free inertial navigation system, this paper designed a kind of easy to engineering realization of 9 accelerometer configuration scheme, studied attitude measurement principle based on this configuration.Through analysing the acceleration in the carrier movement, obtained angular velocity and linear acceleration.",

keywords = "Acceleromete, Attitude measurement, GFSINS",

author = "Xiaoli Wang and Xun Zhou",

year = "2011",

doi = "10.1109/MACE.2011.5987989",

language = "English",

isbn = "9781424494392",

series = "2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Proceedings",

pages = "4432--4434",

booktitle = "2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Proceedings",

note = "2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 ; Conference date: 15-07-2011 Through 17-07-2011",

}

Wang, X & Zhou, X 2011, Study on attitude measurement in gyro-free inertial navigation system. in 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Proceedings., 5987989, 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Proceedings, pp. 4432-4434, 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, Inner Mongolia, China, 15/07/11. https://doi.org/10.1109/MACE.2011.5987989

Study on attitude measurement in gyro-free inertial navigation system. / Wang, Xiaoli; Zhou, Xun.
2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Proceedings. 2011. p. 4432-4434 5987989 (2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Proceedings).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Study on attitude measurement in gyro-free inertial navigation system

AU - Wang, Xiaoli

AU - Zhou, Xun

PY - 2011

Y1 - 2011

N2 - Through analysing the measurement priniple of the accelerometer-based gyro-free inertial navigation system, this paper designed a kind of easy to engineering realization of 9 accelerometer configuration scheme, studied attitude measurement principle based on this configuration.Through analysing the acceleration in the carrier movement, obtained angular velocity and linear acceleration.

AB - Through analysing the measurement priniple of the accelerometer-based gyro-free inertial navigation system, this paper designed a kind of easy to engineering realization of 9 accelerometer configuration scheme, studied attitude measurement principle based on this configuration.Through analysing the acceleration in the carrier movement, obtained angular velocity and linear acceleration.

KW - Acceleromete

KW - Attitude measurement

KW - GFSINS

UR - http://www.scopus.com/inward/record.url?scp=80054812889&partnerID=8YFLogxK

U2 - 10.1109/MACE.2011.5987989

DO - 10.1109/MACE.2011.5987989

M3 - Conference contribution

AN - SCOPUS:80054812889

SN - 9781424494392

T3 - 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Proceedings

SP - 4432

EP - 4434

BT - 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Proceedings

T2 - 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011

Y2 - 15 July 2011 through 17 July 2011

ER -

Study on attitude measurement in gyro-free inertial navigation system

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Cite this