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32994

On-line Control Technique for Missile Autopilot

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Last updated: 24 Dec 2024

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Abstract

In this paper a new learning strategy is used for on-line tuning the control system of the ballistic missile. The gradient descent method technique is utilized to derive the on-line tuning laws of the robust controller, so that the robust performance of the system can be yielded. As the result of using this method, the old technique “gain schedule" that normally used in ballistic missile is replaced. The simulation result shows a good settling time, less or no overshoot and higher robustness were achieved. Moreover, the new tuning process is successful in the presence of high noise.

DOI

10.21608/iceeng.2010.32994

Keywords

PID tuning, Missile control system and Gradient descent

Authors

First Name

Magdy

Last Name

Abo-Elela

MiddleName

-

Affiliation

College of Engineering, Cairo University, Cairo, Egypt.

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Orcid

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First Name

Ayman

Last Name

El-Shabrawy

MiddleName

-

Affiliation

Egyptian Armed Forces.

Email

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City

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Orcid

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First Name

Ibrahim

Last Name

Hassan

MiddleName

-

Affiliation

Egyptian Armed Forces.

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-

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Orcid

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Volume

7

Article Issue

7th International Conference on Electrical Engineering ICEENG 2010

Related Issue

5537

Issue Date

2010-05-01

Receive Date

2019-05-23

Publish Date

2010-05-01

Page Start

1

Page End

8

Print ISSN

2636-4433

Online ISSN

2636-4441

Article File

ICEENG_Volume 7_Issue 7th International Conference on Electrical Engineering ICE….pdf

PDF . 254.8kB

Link

https://iceeng.journals.ekb.eg/article_32994.html

Detail API

https://iceeng.journals.ekb.eg/service?article_code=32994

Order

41

Type

Original Article

Type Code

833

Publication Type

Journal

Publication Title

The International Conference on Electrical Engineering

Publication Link

https://iceeng.journals.ekb.eg/

MainTitle

On-line Control Technique for Missile Autopilot

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Article

Created At

22 Jan 2023