Research on Searching Guidance of TV Guided Missile

Hao Peng Wang; Ze Qian Liu

doi:10.4028/www.scientific.net/AMM.404.609

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 404Research on Searching Guidance of TV Guided...

Research on Searching Guidance of TV Guided Missile

Abstract:

The searching phase of TV guided missile is usually divided into three different stages as the navigation, homing and terminal guidance. In this paper, guidance laws in different phases are analyzed. To solve the problem of target acquisition, signal following and navigation precision during the period of navigation, methods of integrated guidance with three geostationary satellites orientation and INS in high dynamic circumstances are put forward. The mathematics models of pre - guiding and searching are established corresponding to the traits of smaller TV seeker instantaneous field, limited shooter reacting velocity, low hunting speed and narrow searching area. The compound guidance methods which integrate the tracking and the proportional in terminal phase are raised in order to increase the guiding precision and to decrease the undershoot value. Experiment shows that the guiding precision is raised by a long way.CLC number: TJ765.4+3 Document Code: B

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Periodical:

Applied Mechanics and Materials (Volume 404)

Pages:

609-617

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.404.609

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Online since:

September 2013

Authors:

Hao Peng Wang, Ze Qian Liu

Keywords:

Searching Guidance, Terminal Guidance, Three Geostationary Satellites Orientation, TV Guidance Missile

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