Journal
Scientific and technical journal «Priborostroenie»
UDK517.977.5
Issue:12 (52)
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OPTIMIZATION OF FLYING VEHICLE DYNAMICS WITH DIFFERENT CRITERI
Annotation
The problem of optimal control over a flying vehicle regarded as a hard body is considered. Flying object dynamics is described by Euler and Poisson equations. The optimal solution to the problem is obtained on the base of Pontriagin principle with Lagrange criterion as a goal functional.
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