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Air Drag Effects on the Missile Trajectories
Author
Source
Journal of Applied Mathematics
Issue
Vol. 2011, Issue 2011 (31 Dec. 2011), pp.1-19, 19 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2011-10-11
Country of Publication
Egypt
No. of Pages
19
Main Subjects
Abstract EN
The equations of motion of a missile under the air drag effects are constructed.
The modified TD88 is surveyed.
Using Lagrange's planetary equations in Gauss form, the perturbations, due to the air drag in the orbital elements, are computed between the eccentric anomalies of the burn out and the reentry points [Ebo,2π−Ebo], respectively.
The range equation is expressed as an infinite series in terms of the eccentricity e and the eccentric anomaly E.
The different errors in the missile-free range due to the drag perturbations in the missile trajectory are obtained.
American Psychological Association (APA)
Abd El-Salam, F. A.. 2011. Air Drag Effects on the Missile Trajectories. Journal of Applied Mathematics،Vol. 2011, no. 2011, pp.1-19.
https://search.emarefa.net/detail/BIM-505000
Modern Language Association (MLA)
Abd El-Salam, F. A.. Air Drag Effects on the Missile Trajectories. Journal of Applied Mathematics No. 2011 (2011), pp.1-19.
https://search.emarefa.net/detail/BIM-505000
American Medical Association (AMA)
Abd El-Salam, F. A.. Air Drag Effects on the Missile Trajectories. Journal of Applied Mathematics. 2011. Vol. 2011, no. 2011, pp.1-19.
https://search.emarefa.net/detail/BIM-505000
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-505000