Computational Algorithm for Gravity Turn Maneuver

Authors

  • L.A.Alaqal

  • Dr. M. A. Sharaf

descent guidance, trajectory optimization, navigation, control

Abstract

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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How to Cite

Computational Algorithm for Gravity Turn Maneuver. (2012). Global Journal of Science Frontier Research, 12(F13), 59-64. https://journalofscience.org/index.php/GJSFR/article/view/683

 

References

I Mehedi, T Kubota (2011) Advanced Guidance Scheme for Lunar Descent and 2. Landing from Orbital Speed Conditions. 54, 98-105.

L Roger (1964) Mars Nonstop Round-Trip Trajectories. 2(2), 368-370.

G Samuel (1965) Dynamic Systems Approach to the Lander Descent Problem. 34(3), 911-915.

W Thomson (1986) Introduction to Space Dynamics. 64.

Computational Algorithm for Gravity Turn Maneuver

Published

2012-11-22

Issue

Vol. 12 No. F13 (2012): GJSFR-F Mathematics: Volume 12 Issue F13

Section

Articles

License

Copyright (c) 2012 Authors and Global Journals Private Limited

Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

How to Cite

Computational Algorithm for Gravity Turn Maneuver. (2012). Global Journal of Science Frontier Research, 12(F13), 59-64. https://journalofscience.org/index.php/GJSFR/article/view/683