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- W2912755446 abstract "Due to production tolerences and off-nominal environmental conditions, the thrust time profile of solid propellant rocket motors suffers from high uncertainties in both magnitude and burn-out time. This behaviour leads to higher uncertainties in the motion parameters of the missile at the shut-off (burn-out) point. Accordingly, the impact point is highly erroneous.This paper develops a guidance and control strategy for compensating the effects of the above-mentioned uncertainties insuch a way as to minimize impact errors." @default.
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- W2912755446 date "1991-05-01" @default.
- W2912755446 modified "2023-09-25" @default.
- W2912755446 title "AN IMPROVED GUIDANCE ALGORITHM FOR SOLID PROPELLENT BALLISTIC MISSILES" @default.
- W2912755446 doi "https://doi.org/10.21608/asat.1991.25811" @default.
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