Research on Missile System with Strapdown Guidance Technology

Abstract:

This paper presents a project of missile guidance system based on the strapdown guidance technology. The project is composed of strapdown seeker and inertial measurement unit. The integrated guidance and control technology have been adopted. The project raise accuracy of missiles on the premise that the low cost should be guaranteed. According to simulation experiment, this paper proves the feasiblity of the scheme, and it has good ballistic missile.

• Periodical: Advanced Materials Research (Volumes 785-786)
• Pages: 1560-1563
• DOI: https://doi.org/10.4028/www.scientific.net/AMR.785-786.1560
• Online since: September 2013
• Authors: De Long Feng, Suo Chang Yang, Ying Xi Liu
• Keywords: Guided Missile, Proportional Guidance Law, Seeker, Strapdown

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