Simulation based on MEMS INS performance analyses in flying mission

Wenling Liu; Pei Chen; Chao Han

doi:10.1109/PCSPA.2010.296

Simulation based on MEMS INS performance analyses in flying mission

Wenling Liu^*
, Pei Chen
, Chao Han

^*Corresponding author for this work

School of Astronautics

Beihang University

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

1 Scopus citations

Abstract

This paper describes the principle and implementation of a simulator based on Inertial Navigation System (INS) using Micro Electro Mechanical System (MEMS) The MEMS is composed of Micro Inertial Measurement Unit (MIMU). The gyroscope and accelerometer error models are established according to the characteristics of the MEMS. The principle of INS is described and an INS model is established to simulate and analyze the influence of the MEMS performance on navigation precision. An example of a sounding rocket is presented in the paper to analyze the INS performance using MEMS in flying mission.

Original language	English
Title of host publication	Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010
Pages	1205-1208
Number of pages	4
DOIs	https://doi.org/10.1109/PCSPA.2010.296
State	Published - 2010
Event	1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010 - Harbin, China Duration: 17 Sep 2010 → 19 Sep 2010

Publication series

Name	Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010

Conference

Conference	1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010
Country/Territory	China
City	Harbin
Period	17/09/10 → 19/09/10

Keywords

Error model
INS
MEMS
Navigation precision

Access to Document

10.1109/PCSPA.2010.296

Cite this

Liu, W., Chen, P., & Han, C. (2010). Simulation based on MEMS INS performance analyses in flying mission. In Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010 (pp. 1205-1208). Article 5636013 (Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010). https://doi.org/10.1109/PCSPA.2010.296

Liu, Wenling ; Chen, Pei ; Han, Chao. / Simulation based on MEMS INS performance analyses in flying mission. Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010. 2010. pp. 1205-1208 (Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010).

@inproceedings{f3d4d64ce4244627a15d78d8e4b21bd4,

title = "Simulation based on MEMS INS performance analyses in flying mission",

abstract = "This paper describes the principle and implementation of a simulator based on Inertial Navigation System (INS) using Micro Electro Mechanical System (MEMS) The MEMS is composed of Micro Inertial Measurement Unit (MIMU). The gyroscope and accelerometer error models are established according to the characteristics of the MEMS. The principle of INS is described and an INS model is established to simulate and analyze the influence of the MEMS performance on navigation precision. An example of a sounding rocket is presented in the paper to analyze the INS performance using MEMS in flying mission.",

keywords = "Error model, INS, MEMS, Navigation precision",

author = "Wenling Liu and Pei Chen and Chao Han",

year = "2010",

doi = "10.1109/PCSPA.2010.296",

language = "英语",

isbn = "9780769541808",

series = "Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010",

pages = "1205--1208",

booktitle = "Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010",

note = "1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010 ; Conference date: 17-09-2010 Through 19-09-2010",

}

Liu, W, Chen, P & Han, C 2010, Simulation based on MEMS INS performance analyses in flying mission. in Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010., 5636013, Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010, pp. 1205-1208, 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010, Harbin, China, 17/09/10. https://doi.org/10.1109/PCSPA.2010.296

Simulation based on MEMS INS performance analyses in flying mission. / Liu, Wenling; Chen, Pei; Han, Chao.
Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010. 2010. p. 1205-1208 5636013 (Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010).

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

TY - GEN

T1 - Simulation based on MEMS INS performance analyses in flying mission

AU - Liu, Wenling

AU - Chen, Pei

AU - Han, Chao

PY - 2010

Y1 - 2010

N2 - This paper describes the principle and implementation of a simulator based on Inertial Navigation System (INS) using Micro Electro Mechanical System (MEMS) The MEMS is composed of Micro Inertial Measurement Unit (MIMU). The gyroscope and accelerometer error models are established according to the characteristics of the MEMS. The principle of INS is described and an INS model is established to simulate and analyze the influence of the MEMS performance on navigation precision. An example of a sounding rocket is presented in the paper to analyze the INS performance using MEMS in flying mission.

AB - This paper describes the principle and implementation of a simulator based on Inertial Navigation System (INS) using Micro Electro Mechanical System (MEMS) The MEMS is composed of Micro Inertial Measurement Unit (MIMU). The gyroscope and accelerometer error models are established according to the characteristics of the MEMS. The principle of INS is described and an INS model is established to simulate and analyze the influence of the MEMS performance on navigation precision. An example of a sounding rocket is presented in the paper to analyze the INS performance using MEMS in flying mission.

KW - Error model

KW - INS

KW - MEMS

KW - Navigation precision

UR - https://www.scopus.com/pages/publications/78650443084

U2 - 10.1109/PCSPA.2010.296

DO - 10.1109/PCSPA.2010.296

M3 - 会议稿件

AN - SCOPUS:78650443084

SN - 9780769541808

T3 - Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010

SP - 1205

EP - 1208

BT - Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010

T2 - 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010

Y2 - 17 September 2010 through 19 September 2010

ER -

Liu W, Chen P, Han C. Simulation based on MEMS INS performance analyses in flying mission. In Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010. 2010. p. 1205-1208. 5636013. (Proceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010). doi: 10.1109/PCSPA.2010.296

Simulation based on MEMS INS performance analyses in flying mission

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