Flugzeug-Regelsystem für vertikale Position
Aircraft input signals of selected altitude (hs), selected vertical speed (h/s), current altitude (h), current vertical speed (h/), current pitch attitude ( ), current normal acceleration (Nz) and current pitch rate (Q) are processed to produce an elevator command ( delta e) that will result in a sm...
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| Zusammenfassung: | Aircraft input signals of selected altitude (hs), selected vertical speed (h/s), current altitude (h), current vertical speed (h/), current pitch attitude ( ), current normal acceleration (Nz) and current pitch rate (Q) are processed to produce an elevator command ( delta e) that will result in a smooth vertical transition of the aircraft for various autopilot vertical maneuvers, including altitude capture and hold, glideslope capture and hold, and flare control. |
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