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25811

AN IMPROVED GUIDANCE ALGORITHM FOR SOLID PROPELLENT BALLISTIC MISSILES

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Last updated: 04 Jan 2025

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Abstract

Due to production tolerences and off-nominal environmental conditions, the thrust time profile of solid propellant rocket motors suffers from high uncertainties in both magnitude and burn-out time. This behaviour leads to higher uncertainties in the motion parameters of the missile at the shut-off (burn-out) point. Accordingly, the impact point is highly erroneous.
This paper develops a guidance and control strategy for compensating the effects of the above-mentioned uncertainties in
such a way as to minimize impact errors.

DOI

10.21608/asat.1991.25811

Authors

First Name

S.

Last Name

GHONIEMY

MiddleName

-

Affiliation

Asc.Prof. Guid.Dep.M.T.C.

Email

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City

-

Orcid

-

First Name

M.

Last Name

TANTAWY

MiddleName

-

Affiliation

Asc.Prof. D.S.S.C.

Email

-

City

-

Orcid

-

First Name

M.

Last Name

ELLEITHY

MiddleName

-

Affiliation

Ph.D. Air Def.College.

Email

-

City

-

Orcid

-

Volume

4

Article Issue

ASAT CONFLENCE 14-16 May 1991 , CAIRO

Related Issue

4667

Issue Date

1991-05-01

Receive Date

2019-01-23

Publish Date

1991-05-01

Page Start

349

Page End

361

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 4_Issue ASAT CONFLENCE 14-16 May 1991 , CAIRO_Pages 349-361.pdf

PDF . 2.0MB

Link

https://asat.journals.ekb.eg/article_25811.html

Detail API

https://asat.journals.ekb.eg/service?article_code=25811

Order

33

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

AN IMPROVED GUIDANCE ALGORITHM FOR SOLID PROPELLENT BALLISTIC MISSILES

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Article

Created At

22 Jan 2023