Computation of the Different Errors in the Ballistic Missiles Range
Joint Authors
Abd El-Bar, S. E.
Abd El-Salam, F. A.
Source
Issue
Vol. 2011, Issue 2011 (31 Dec. 2011), pp.1-16, 16 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2011-10-12
Country of Publication
Egypt
No. of Pages
16
Main Subjects
Abstract EN
The ranges of the ballistic missile trajectories are very sensitive to any kind of errors.
Most of the missile trajectory is a part of an elliptical orbit.
In this work, the missile problem is stated.
The variations in the orbital elements are derived using Lagrange planetary equations.
Explicit expressions for the errors in the missile range due to the in-orbit plane changes are derived.
Explicit expressions for the errors in the missile range due to the out-of-orbit plane changes are derived when the burnout point is assumed on the equator.
American Psychological Association (APA)
Abd El-Salam, F. A.& Abd El-Bar, S. E.. 2011. Computation of the Different Errors in the Ballistic Missiles Range. ISRN Applied Mathematics،Vol. 2011, no. 2011, pp.1-16.
https://search.emarefa.net/detail/BIM-464863
Modern Language Association (MLA)
Abd El-Salam, F. A.& Abd El-Bar, S. E.. Computation of the Different Errors in the Ballistic Missiles Range. ISRN Applied Mathematics No. 2011 (2011), pp.1-16.
https://search.emarefa.net/detail/BIM-464863
American Medical Association (AMA)
Abd El-Salam, F. A.& Abd El-Bar, S. E.. Computation of the Different Errors in the Ballistic Missiles Range. ISRN Applied Mathematics. 2011. Vol. 2011, no. 2011, pp.1-16.
https://search.emarefa.net/detail/BIM-464863
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-464863