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Numerical simulation of optimal explicit guidance algorithm for satellite launch vehicle(slv)

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Material type: Text

TextPublication details: Department of Mathematics IslamabadDescription: 68 pSubject(s):

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Holdings
Item type	Current library	Collection	Call number	Status	Barcode
Thesis	Air University Central Library Thesis Repository (5th Floor) Mathematics	Mathematics	510 RAF-MS (Browse shelf(Opens below))	Available	TH1335

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