Paper Title:
Guidance Law Design for Space-Based Anti-Missile Boost Phase Intercept
  Abstract

Guidance law The optimal direct-impact guidance law for space-based anti-missile of ballistic missile in boost phase is considered. First the relative motion equation between missile and target is built, then the optimal guidance law based on terminal miss distance is designed. using minimum energy as the optimum index. The simulation results show the effectiveness of our guidance law.

  Info
Periodical
Advanced Materials Research (Volumes 301-303)
Chapter
Chapter 3: Mechanical, Electronic and Material Engineering
Edited by
Riza Esa and Yanwen Wu
Pages
1749-1753
DOI
10.4028/www.scientific.net/AMR.301-303.1749
Citation
H. Huang, Z. F. Zhu, "Guidance Law Design for Space-Based Anti-Missile Boost Phase Intercept", Advanced Materials Research, Vols. 301-303, pp. 1749-1753, 2011
Online since
July 2011
Authors
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Price
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