OPTIMIZATION OF FLYING VEHICLE DYNAMICS WITH DIFFERENT CRITERI
Anton A. Alexandrov — Post-Graduate Student; Ustinov Baltic State Technical University “Voenmech”, Department of Information Processing Systems and Control; Post-Graduate Student
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Abstract. 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.
Keywords:
flying vehicle, optimal control, Pontriagin principle.
