Computational Algorithm for Gravity Turn Maneuver

Computational Algorithm for Gravity Turn Maneuver

L.A.Alaqal

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Dr. M. A. Sharaf

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1 King AbdulAziz University, Jeddah, Saudi Arabia.

2 King Abdul Aziz University

GJSFR Volume 12 Issue F13

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In this paper, computational algorithm for gravity turn maneuver is established for variable thrust-to-weight ratio. The applications of the algorithm was illustrated graphically.

4 Cites in Articles

References

I Mehedi,T Kubota (2011). Advanced Guidance Scheme for Lunar Descent and 2. Landing from Orbital Speed Conditions.
L Roger (1964). Mars Nonstop Round-Trip Trajectories.
G Samuel (1965). Dynamic Systems Approach to the Lander Descent Problem.
W Thomson (1986). Introduction to Space Dynamics.

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Funding

No external funding was declared for this work.

Conflict of Interest

The authors declare no conflict of interest.

Ethical Approval

No ethics committee approval was required for this article type.

Data Availability

Not applicable for this article.

L.A.Alaqal. 2012. \u201cComputational Algorithm for Gravity Turn Maneuver\u201d. Global Journal of Science Frontier Research - F: Mathematics & Decision GJSFR-F Volume 12 (GJSFR Volume 12 Issue F13): .

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GJSFR Volume 12 Issue F13
Pg. 59- 64

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Journal Specifications

Crossref Journal DOI 10.17406/GJSFR

Print ISSN 0975-5896

e-ISSN 2249-4626

Keywords

control descent guidance navigation trajectory optimization

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Submission ReceivedOctober 9, 2012
RevisedOctober 9, 2012
Peer Review Double Blind
Handling Editor
Accepted October 29, 2012
Published November 8, 2012

Version of record

v1.2

Issue date

November 22, 2012

Language

English

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Article Matrices

Total Score: 127

Country: Saudi Arabia

Subject: Global Journal of Science Frontier Research - F: Mathematics & Decision

Authors: Dr. M. A. Sharaf, L.A.Alaqal (PhD/Dr. count: 1)

View Count (all-time): 144

Total Views (Real + Logic): 5085

Total Downloads (simulated): 2723

Publish Date: 2012 11, Thu

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Total Views: 5085

Total Downloads: 2723

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In this paper, computational algorithm for gravity turn maneuver is established for variable thrust-to-weight ratio. The applications of the algorithm was illustrated graphically.

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