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ISSN:2394-3661 | Crossref DOI | SJIF: 5.138 | PIF: 3.854

International Journal of Engineering and Applied Sciences

(An ISO 9001:2008 Certified Online and Print Journal)

Missile Guidance Law Design via Backstepping Technique

( Volume 3 Issue 4,April 2016 ) OPEN ACCESS
Author(s):

Hamza Zaidi, Panlong Wu, Ali Bellahcene

Abstract:

In this paper a Back-stepping Control technique is proposed for command to line-of-sight missile guidance law design. In this design, the three-dimensional (3-D) CLOS guidance problem is formulated as a tracking problem of a time-varying nonlinear system. Simulation results for different engagement scenarios illustrate the validity of the proposed Backstepping-based Guidance Law.

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