Single-axis accelerometer-based range correction method for the rocket-assisted projectile and precision analysis

Shen Qiang; Dongguang Li

doi:10.1109/KAMW.2008.4810556

Single-axis accelerometer-based range correction method for the rocket-assisted projectile and precision analysis

Shen Qiang^*, Dongguang Li

^*Corresponding author for this work

School of Mechatronical Engineering

Beijing Institute of Technology

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

2 Citations (Scopus)

Abstract

This paper proposes a single-axis accelerometer-based range correction method for rocket-assisted projectile, which is applicable to the low-cost autonomous correction for the rangeextended projectile with the range being mainly influenced by the deviation of the rocket thrust force. Based on the proposal of the basic principle of the method, it performs analysis and calculation on various elements that influence the precision of the system. The results show that the relative circular error probable of the range, which cannot be eliminated by the correction system, is 0.28%, the relative circular error probable of the range, which is caused by the sensor system, shall be less than 0.18%, and the null-drift error of the sensor is required to be at least less than 0.04% of the full range.

Original language	English
Title of host publication	2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008
Pages	586-588
Number of pages	3
DOIs	https://doi.org/10.1109/KAMW.2008.4810556
Publication status	Published - 2008
Event	2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop, KAM 2008 - Wuhan, China Duration: 21 Dec 2008 → 22 Dec 2008

Publication series

Name	2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008

Conference

Conference	2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop, KAM 2008
Country/Territory	China
City	Wuhan
Period	21/12/08 → 22/12/08

Keywords

Accelerometer
Correction
Precision
Rocket-assisted projectile

Access to Document

10.1109/KAMW.2008.4810556

Cite this

Qiang, S., & Li, D. (2008). Single-axis accelerometer-based range correction method for the rocket-assisted projectile and precision analysis. In 2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008 (pp. 586-588). Article 4810556 (2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008). https://doi.org/10.1109/KAMW.2008.4810556

Qiang, Shen ; Li, Dongguang. / Single-axis accelerometer-based range correction method for the rocket-assisted projectile and precision analysis. 2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008. 2008. pp. 586-588 (2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008).

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title = "Single-axis accelerometer-based range correction method for the rocket-assisted projectile and precision analysis",

abstract = "This paper proposes a single-axis accelerometer-based range correction method for rocket-assisted projectile, which is applicable to the low-cost autonomous correction for the rangeextended projectile with the range being mainly influenced by the deviation of the rocket thrust force. Based on the proposal of the basic principle of the method, it performs analysis and calculation on various elements that influence the precision of the system. The results show that the relative circular error probable of the range, which cannot be eliminated by the correction system, is 0.28%, the relative circular error probable of the range, which is caused by the sensor system, shall be less than 0.18%, and the null-drift error of the sensor is required to be at least less than 0.04% of the full range.",

keywords = "Accelerometer, Correction, Precision, Rocket-assisted projectile",

author = "Shen Qiang and Dongguang Li",

year = "2008",

doi = "10.1109/KAMW.2008.4810556",

language = "English",

isbn = "9781424435296",

series = "2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008",

pages = "586--588",

booktitle = "2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008",

note = "2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop, KAM 2008 ; Conference date: 21-12-2008 Through 22-12-2008",

}

Qiang, S & Li, D 2008, Single-axis accelerometer-based range correction method for the rocket-assisted projectile and precision analysis. in 2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008., 4810556, 2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008, pp. 586-588, 2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop, KAM 2008, Wuhan, China, 21/12/08. https://doi.org/10.1109/KAMW.2008.4810556

Single-axis accelerometer-based range correction method for the rocket-assisted projectile and precision analysis. / Qiang, Shen; Li, Dongguang.
2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008. 2008. p. 586-588 4810556 (2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008).

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

TY - GEN

T1 - Single-axis accelerometer-based range correction method for the rocket-assisted projectile and precision analysis

AU - Qiang, Shen

AU - Li, Dongguang

PY - 2008

Y1 - 2008

N2 - This paper proposes a single-axis accelerometer-based range correction method for rocket-assisted projectile, which is applicable to the low-cost autonomous correction for the rangeextended projectile with the range being mainly influenced by the deviation of the rocket thrust force. Based on the proposal of the basic principle of the method, it performs analysis and calculation on various elements that influence the precision of the system. The results show that the relative circular error probable of the range, which cannot be eliminated by the correction system, is 0.28%, the relative circular error probable of the range, which is caused by the sensor system, shall be less than 0.18%, and the null-drift error of the sensor is required to be at least less than 0.04% of the full range.

AB - This paper proposes a single-axis accelerometer-based range correction method for rocket-assisted projectile, which is applicable to the low-cost autonomous correction for the rangeextended projectile with the range being mainly influenced by the deviation of the rocket thrust force. Based on the proposal of the basic principle of the method, it performs analysis and calculation on various elements that influence the precision of the system. The results show that the relative circular error probable of the range, which cannot be eliminated by the correction system, is 0.28%, the relative circular error probable of the range, which is caused by the sensor system, shall be less than 0.18%, and the null-drift error of the sensor is required to be at least less than 0.04% of the full range.

KW - Accelerometer

KW - Correction

KW - Precision

KW - Rocket-assisted projectile

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T3 - 2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008

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Qiang S, Li D. Single-axis accelerometer-based range correction method for the rocket-assisted projectile and precision analysis. In 2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008. 2008. p. 586-588. 4810556. (2008 IEEE International Symposium on Knowledge Acquisition and Modeling Workshop Proceedings, KAM 2008). doi: 10.1109/KAMW.2008.4810556

Single-axis accelerometer-based range correction method for the rocket-assisted projectile and precision analysis

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