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- W2381569510 abstract "To appropriately correct trajectory error,an approach of estimating terminal trajectory correction was proposed.The effect of the impulsive force and moment on the velocity deflection angle was studied by swing theory,and a fast estimation approach of the correction of each impulse was proposed based on the relationship between terminal correction and velocity deflection angle.The numerical simulation of the 6DOF trajectory was carried out.The actual impact point correction computed by numerical simulation was compared with the estimated correction by the approach.The results show that the chosen impulse azimuth is exact,and the fast estimation approach of the correction of each impulse is effective,and the effect of multi-impulses can be superposed if the time interval of impulse is set appropriately." @default.
- W2381569510 created "2016-06-24" @default.
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- W2381569510 date "2010-01-01" @default.
- W2381569510 modified "2023-09-23" @default.
- W2381569510 title "Correction Estimation of Low-Rolling Terminal Trajectory Correction Projectile" @default.
- W2381569510 hasPublicationYear "2010" @default.
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