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Comparison of selected criteria of flight characteristcs on an airplane simulator
Melich, Peter ; Zikmund, Pavel (referee) ; Matějů, Jiří (advisor)
As of today, we might consider PC technologies as very progressive and advanced. Due to this fact, we have numerous commercial flight simulators available on the market nowadays. However, each flight simulator has it’s own specific characteristics and behaviour and that’s why I’m going to compare selected flight characteristics in the chosen flight simulator on a chosen aircraft type (Cessna 172SP in my case) and it’s comparison with measured data from real-life environment in this thesis. Data comparison will show us how accurately simulator responds to inputs from the user and if the simulation is similar in relation to real conditions.
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Load calculation and design of control system
Lontras, Martin ; Bartoněk, Jaroslav (referee) ; Jebáček, Ivo (advisor)
This thesis deals with the control system of two-seater aircraft corresponding to CS-23 Level 2. First load calculations of each control surface are performed using the proses described in previous CS-23 regulation. This load is calculated trought the steering mechanism to control elements in cockpit. The resulting forces on the control elements are compared with the requi-rements in CS-23. Because the steering forces meets requirements is not necessary to propose changes in steering kinematics. However, there are further suggested ways of adjusting the control in case the external load would increase during further development of the airplane. At the end, the strength calculation of entire mechanism is preformed.
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Comparison of selected criteria of flight characteristcs on an airplane simulator
Melich, Peter ; Zikmund, Pavel (referee) ; Matějů, Jiří (advisor)
As of today, we might consider PC technologies as very progressive and advanced. Due to this fact, we have numerous commercial flight simulators available on the market nowadays. However, each flight simulator has it’s own specific characteristics and behaviour and that’s why I’m going to compare selected flight characteristics in the chosen flight simulator on a chosen aircraft type (Cessna 172SP in my case) and it’s comparison with measured data from real-life environment in this thesis. Data comparison will show us how accurately simulator responds to inputs from the user and if the simulation is similar in relation to real conditions.
|
|
|
Load calculation and design of control system
Lontras, Martin ; Bartoněk, Jaroslav (referee) ; Jebáček, Ivo (advisor)
This thesis deals with the control system of two-seater aircraft corresponding to CS-23 Level 2. First load calculations of each control surface are performed using the proses described in previous CS-23 regulation. This load is calculated trought the steering mechanism to control elements in cockpit. The resulting forces on the control elements are compared with the requi-rements in CS-23. Because the steering forces meets requirements is not necessary to propose changes in steering kinematics. However, there are further suggested ways of adjusting the control in case the external load would increase during further development of the airplane. At the end, the strength calculation of entire mechanism is preformed.
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