Study on a Control Method for Trajectory Correction

Ke Jia Zhang

doi:10.4028/www.scientific.net/AMM.157-158.1042

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 157-158Study on a Control Method for Trajectory...

Study on a Control Method for Trajectory Correction

Abstract:

In order to obtain a two-dimension trajectory correction method based on mature and simple technologies, a simple correction method was proposed. On these basis, spin control, lift and static margin control have been evaluated by identify relevant parameters acting on range and deflection. The correction capability that they offer has been compared by means of a six DOF simulation in the case of a 122mm low spin rocket. The calculation results show that this control method is able to realize the function of two-dimension trajectory correction.

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Periodical:

Applied Mechanics and Materials (Volumes 157-158)

Pages:

1042-1045

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.157-158.1042

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Online since:

February 2012

Authors:

Ke Jia Zhang

Keywords:

Control Methed, Projectile, Trajectory Correction

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References

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