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25465

MICROPROCESSOR IMPLEMENTATION OF AN ON-LINE OPTIMAL ESTIMATOR OF GUIDANCE STATES FOR A SHORT-RANGE HOMING SYSTEM

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Last updated: 04 Jan 2025

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Abstract

An optimal online pp-based estimator for the guidance states of a short range homing system is presented, taking into account : the horning head measurement errors, autopilot measurement errors, launch initial heading errors, and wind disturbances. A powerful 16-bit microprocessor system is used. The obtained results illustrate the potential improvement of both the missdistance and normal acceleration as well as the overall system performance. Moreover, the system allows for further modifications through more powerful algorithms.

DOI

10.21608/asat.1995.25465

Authors

First Name

M.

Last Name

Fahmy

MiddleName

A.

Affiliation

Guidance Dept., M.T.C. Cairo, Egypt.

Email

-

City

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Orcid

-

First Name

S.

Last Name

Bahgat

MiddleName

F.

Affiliation

Guidance Dept., M.T.C. Cairo, Egypt.

Email

-

City

-

Orcid

-

First Name

S.

Last Name

Ghoniemy

MiddleName

-

Affiliation

Guidance Dept., M.T.C. Cairo, Egypt.

Email

-

City

-

Orcid

-

Volume

6

Article Issue

ASAT CONFERENCE 2 — 4 May 1995, CAIRO

Related Issue

4647

Issue Date

1995-05-01

Receive Date

2019-01-20

Publish Date

1995-05-01

Page Start

1

Page End

10

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 6_Issue ASAT CONFERENCE 2 — 4 May 1995, CAIRO_Pages 1-10.pdf

PDF . 1.7MB

Link

https://asat.journals.ekb.eg/article_25465.html

Detail API

https://asat.journals.ekb.eg/service?article_code=25465

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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

MICROPROCESSOR IMPLEMENTATION OF AN ON-LINE OPTIMAL ESTIMATOR OF GUIDANCE STATES FOR A SHORT-RANGE HOMING SYSTEM

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Article

Created At

22 Jan 2023