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- W2100888049 abstract "− Using a synthesis algorithm of a linear state observer one estimates the state vector for longitudinal and lateral move of an aircraft (whose wings are or aren’t affected by elastic deformations). Also one presents the estimation of a flexible aircraft’s state vector. Gain matrix of the observer is calculated using the method of poles’ positioning." @default.
- W2100888049 created "2016-06-24" @default.
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- W2100888049 date "2008-01-01" @default.
- W2100888049 modified "2023-09-26" @default.
- W2100888049 title "AIRCRAFTS' MOVE STABILISATION USING OPTIMAL CRITERIA AND LINEAR STATE OBSERVERS" @default.
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