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Národní úložiště šedé literatury Nalezeno 4 záznamů.  Hledání trvalo 0.00 vteřin. 
LQ-regulator design and its analysis for the aircraft's longitudinal and lateral motion
 Prešinský, Ján ; Zatočilová, Jitka (oponent) ; Nechvátal, Luděk (vedoucí práce)
This diploma thesis is focused on designing and specifying a linear quadratic regulator for longitudinal and lateral motion of the aircraft. The regulator is designed for a linear system obtained from a linearization of our nonlinear dynamic dynamic model of aircraft around the basic reference state (trimmed state-and-level ight). To nd a complete description of this reference state, some optimality problem has to be solved and the solution of this problem is called a trimmed state.
Úplný záznam
Modelling and simulation in aviation
 Prešinský, Ján ; Nechvátal, Luděk (oponent) ; Zatočilová, Jitka (vedoucí práce)
This bachelor thesis is focused on specifying the orientation of aircraft in normal Earth- xed frame. It is devoted to Euler angles representation and quaternions representation. Moreover, it introduces the equations of motion with 3 and 6 degrees of freedom and proposes the numerical method for solving these equations, which are expressed by the set of non-linear diferential equations.
Úplný záznam
LQ-regulator design and its analysis for the aircraft's longitudinal and lateral motion
 Prešinský, Ján ; Zatočilová, Jitka (oponent) ; Nechvátal, Luděk (vedoucí práce)
This diploma thesis is focused on designing and specifying a linear quadratic regulator for longitudinal and lateral motion of the aircraft. The regulator is designed for a linear system obtained from a linearization of our nonlinear dynamic dynamic model of aircraft around the basic reference state (trimmed state-and-level ight). To nd a complete description of this reference state, some optimality problem has to be solved and the solution of this problem is called a trimmed state.
Úplný záznam
Modelling and simulation in aviation
 Prešinský, Ján ; Nechvátal, Luděk (oponent) ; Zatočilová, Jitka (vedoucí práce)
This bachelor thesis is focused on specifying the orientation of aircraft in normal Earth- xed frame. It is devoted to Euler angles representation and quaternions representation. Moreover, it introduces the equations of motion with 3 and 6 degrees of freedom and proposes the numerical method for solving these equations, which are expressed by the set of non-linear diferential equations.
Úplný záznam

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