AN IMPROVED GUIDANCE ALGORITHM FOR SOLID PROPELLENT BALLISTIC MISSILES
GHONIEMY, S., TANTAWY, M., ELLEITHY, M. (1991). AN IMPROVED GUIDANCE ALGORITHM FOR SOLID PROPELLENT BALLISTIC MISSILES. EKB Journal Management System, 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO), 349-361. doi: 10.21608/asat.1991.25811
S. GHONIEMY; M. TANTAWY; M. ELLEITHY. "AN IMPROVED GUIDANCE ALGORITHM FOR SOLID PROPELLENT BALLISTIC MISSILES". EKB Journal Management System, 4, ASAT CONFLENCE 14-16 May 1991 , CAIRO, 1991, 349-361. doi: 10.21608/asat.1991.25811
GHONIEMY, S., TANTAWY, M., ELLEITHY, M. (1991). 'AN IMPROVED GUIDANCE ALGORITHM FOR SOLID PROPELLENT BALLISTIC MISSILES', EKB Journal Management System, 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO), pp. 349-361. doi: 10.21608/asat.1991.25811
GHONIEMY, S., TANTAWY, M., ELLEITHY, M. AN IMPROVED GUIDANCE ALGORITHM FOR SOLID PROPELLENT BALLISTIC MISSILES. EKB Journal Management System, 1991; 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO): 349-361. doi: 10.21608/asat.1991.25811

AN IMPROVED GUIDANCE ALGORITHM FOR SOLID PROPELLENT BALLISTIC MISSILES

International Conference on Aerospace Sciences and Aviation Technology
Article 33, Volume 4, ASAT CONFLENCE 14-16 May 1991 , CAIRO, May 1991, Page 349-361  XML PDF (1.94 MB)
Document Type: Original Article
DOI: 10.21608/asat.1991.25811
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Authors
S. GHONIEMY1; M. TANTAWY2; M. ELLEITHY3
1Asc.Prof. Guid.Dep.M.T.C.
2Asc.Prof. D.S.S.C.
3Ph.D. Air Def.College.
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 in
such a way as to minimize impact errors.
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