RANGE ESTIMATION FOR IR HOMING MISSILES

Q: How can I download an article?

To download an article from SID, first log in to the site, search for the article title, and click on the 'Download Article' option.

Q: How can I download an ISI article?

To download an ISI article on SID, enter the keyword or article title in the search bar, view the relevant results, click on the desired article, and select the 'Download Article' option.

Q: How can I access the SID database?

To access the SID database, visit SID.ir, create an account, and log in to access scientific resources.

Q: Is downloading articles from SID free?

Some articles on SID are available for free, while others require payment. Details are specified on the article's page.

MOHARAMPOUR A.; POSHTAN J.; KHAKI SEDIGH A.

Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Journal Paper

Paper Information

Journal: Journal of Aerospace Mechanics Year:2009 | Volume:4 | Issue:4 (14) Page(s): 55-69

Download Full-Text

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Verion

View:

1,404

Download:

Cites:

Information Journal Paper

Title

RANGE ESTIMATION FOR IR HOMING MISSILES

Author(s)

MOHARAMPOUR A. | POSHTAN J. | KHAKI SEDIGH A. | Issue Writer Certificate

Keywords

RANGE ESTIMATIONQ3

NEUTRAL KALMAN FILTERQ2

PARTICLE FILTERQ3

CRAMER-RAO LOWER BOUNDQ3

PURE PROPORTIONAL GUIDANCEQ3

Abstract

In this paper, PURE PROPORTIONAL GUIDANCE in 3-D space is first explained with a new perception. The main idea is based upon the distinction between angular rate vector and rotation vector conceptions. In this innovation, the emphasis is based upon the selection of line of sight coordinates and comparison between the two available views for choosing this system. Then, using an additional term, an improvement to this law is made. This term compromises a cross range compensator, which is used to provide first fluctuations for obtaining convergent estimates of state variables. Then, a state-space description within the improved spherical coordinate system has been offered. The available measurements in this system have been chosen with regard to the considered practical points. Then, the issue of range-to-target estimation is proposed and some non-linear filters, such as extended Kalman filter, unscented Kalman filter, PARTICLE FILTER, EKF PARTICLE FILTER, and UKF PARTICLE FILTER in the modified spherical coordinates have been used. Simulations indicate that the proposed tracking filters in conjunction with the dual guidance law are able to provide the convergence of the RANGE ESTIMATION for both maneuvering and non-maneuvering targets.

Cites

No record.

References

No record.

Cite

APA: Copy

MOHARAMPOUR, A., POSHTAN, J., & KHAKI SEDIGH, A.. (2009). RANGE ESTIMATION FOR IR HOMING MISSILES. AEROSPACE MECHANICS JOURNAL, 4(4 (14)), 55-69. SID. https://sid.ir/paper/101848/en

Vancouver: Copy

MOHARAMPOUR A., POSHTAN J., KHAKI SEDIGH A.. RANGE ESTIMATION FOR IR HOMING MISSILES. AEROSPACE MECHANICS JOURNAL[Internet]. 2009;4(4 (14)):55-69. Available from: https://sid.ir/paper/101848/en

IEEE: Copy

A. MOHARAMPOUR, J. POSHTAN, and A. KHAKI SEDIGH, “RANGE ESTIMATION FOR IR HOMING MISSILES,” AEROSPACE MECHANICS JOURNAL, vol. 4, no. 4 (14), pp. 55–69, 2009, [Online]. Available: https://sid.ir/paper/101848/en

Related Journal Papers