Beta
26194

Modified Quasilinearization For Optimal Flight Trajectory

Article

Last updated: 04 Jan 2025

Subjects

-

Tags

-

Abstract

The application of Rontrvaqin's maximum principle to optimal control problems results in a two-point boundary value problem. The quasilinearization method is used to solve the resulting problem and the method is very effective if the final time is fixed. In this paper the modified quasilinearization with time transform is used to find the minimum time flight path in a vertical plane. The method is based on Newton-Raphson combined with long's method in order to solve the problem of unknown final time. The advantage of the method is the fact that it does not need large memary size compared with other methods of trajectory optimization. The minimum time trajectory of climb in a vertical plane is obtained after a few iterations which proves that the method is very efficient in this case.

DOI

10.21608/asat.1987.26194

Authors

First Name

I.

Last Name

Mansour

MiddleName

-

Affiliation

Aeronautical Department, Military Technical College, Cairo, Egypt. Member AIAA.

Email

-

City

-

Orcid

-

First Name

M.

Last Name

abdel Hamid

MiddleName

-

Affiliation

Information Certer of Armed Forces, Egypt.

Email

-

City

-

Orcid

-

First Name

A.

Last Name

Bilal

MiddleName

Y.

Affiliation

Prof., Department of Electrical Engineering, Cairo, University, Giza, Egypt.

Email

-

City

-

Orcid

-

Volume

2

Article Issue

A.S.A.T. CONFERENCE 21-23 April 1987 , CAIRO

Related Issue

4700

Issue Date

1987-04-01

Receive Date

2019-01-30

Publish Date

1987-04-01

Page Start

965

Page End

973

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_26194.html

Detail API

https://asat.journals.ekb.eg/service?article_code=26194

Order

37

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

Modified Quasilinearization For Optimal Flight Trajectory

Details

Type

Article

Created At

22 Jan 2023