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Flight guidance vertical level
Ing. Pavel Hospodář, Czech technical university in Prague, Faculty of electrical engineering , Department of control engineering October , 2009
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select see level preasure mode/range of EFIS display air speed setup
Cockpit – FCU Navigation Air speed stabilization Vertical speed Altitude control select see level preasure mode/range of EFIS display air speed setup heading select altitude select vertical speed select
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Vv – vertical speed Vt – total speed H – altitude (differencial form)
Cockpit – FCU Navigation Air speed stabilization Vertical speed Altitude control Vv – vertical speed Vt – total speed H – altitude (differencial form)
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Control element: elevator – UAV – control a critical air speed thrust of engine – classical method
Cockpit – FCU Navigation Air speed stabilization Vertical speed Altitude control
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Change of flight level – elemetary flight mode – flight level at 100 ft
Cockpit – FCU Navigation Air speed stabilization Vertical speed Altitude control
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Root locus method - zero control deviation -> PI reg
Cockpit – FCU Navigation Air speed stabilization Vertical speed Altitude control Root locus method - zero control deviation -> PI reg
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Control equations: Low stability area Cockpit – FCU Navigation
Air speed stabilization Vertical speed Altitude control Low stability area
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Cockpit – FCU Navigation Air speed stabilization Vertical speed Altitude control
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Cockpit – FCU Navigation Air speed stabilization Vertical speed Altitude control
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MPC regulátor Cockpit – FCU Navigation Air speed stabilization
Vertical speed Altitude control MPC regulátor
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Cockpit – FCU Navigation Air speed stabilization Vertical speed Altitude control
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