Computation of the different errors in the ballistic missiles range

DOI10.5402/2011/349737zbMath1238.70008OpenAlexW2132889321WikidataQ58689259 ScholiaQ58689259MaRDI QIDQ420180

S. E. Abd El-Bar, F. A. Abd El-Salam

Publication date: 21 May 2012

Published in: ISRN Applied Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.5402/2011/349737

Mathematics Subject Classification ID

Celestial mechanics (70F15)

Related Items (3)

Analytical and semi-analytical treatment of the satellite motion in a resisting medium ⋮ Air drag effects on the missile trajectories ⋮ An efficient computation of effective ground range using an oblate Earth model

Cites Work

• Ballistic missile trajectory prediction using a state transition matrix
• Orbit determination by solving for gravity parameters with multiple arc data

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