Automatic flight control systems (AE) Flashcards
At missed approach og þú “depressar” TOGA switch, hvað gerist? (tveir þættir)
1) Autothrottle selects go around power.
2) Autopilot flies the GA maneouver.
Ef þú ert með FDC í ALT HOLD mode, hvaða faktorum fylgist hún með (tveir þættir)?
1) altitude deviation
2) pitch attitude
In a flight director (FD) (command bar type), the vertical bar is associated with the roll/pitch channel and why?
Associated with the roll channel.
Getur hugsað þetta þannig að ef þú rollar vélinni þá færist vertical bar. (Þetta er fjólublái krossinn, ef þú rollar t.d. á rétta átt þá er fjólubláa vertical línan komin í miðjuna).
Hvað er roll-out mode að gera í autoland?
Gerir vélinni kleyft að halda centerline á braut eftir lendingu.
Hvaða græja fylgist með í hvaða phase autoland þú ert í?
Radio altimeter
Notar autopilot m.a. inputs frá:
1) ADC
2) Attitude reference system
3) ILS receiver
4) Mode control panel
allt
Flight director er í LOC mode og certical command bar er deviating to the left, þetta þýðir að aircraft:
a) must be rolled to the left
b) is right of the LOC axis
a) must be rolled to the left
Málið er að vertical command er ekki að segja þér NEITT um hvar þú ert, bara hvað þú þarft að GERA.
The guidance functions of a autopilot consists in:
a) stabilizing and monitoring the movements around the centre of gravity
b) monitoring the movements of the centre of gravity in the three dimensions of space.
b) monitoring the movements of the centre of gravity in the three dimensions of space.
Í “command bars” type of flight director the
a) vertical bar may be associated with the pitch channel
b) horizontal bar is associated with the pitch channel
b) horizontal bar is associated with the pitch channel
To allow the coupling of a duel channel flight director.. both autopilot channels must be selecten ON/OFF?
(PS þetta er bara memory item því þessi spurning er víst alveg rugluð)
ON
The horizontal command bar of a flight director gives information about the direction and the amplitude of the corrections to be applied on the ____ of the aircraft.
pitch
Varðandi fail-passive flight control system; In case of failure there is /is not significant deviation of flight path or attitude.
Landing is not/is not completed automatically
no significant deviation but landing is not completed automatically.
Vertical flight path mode of an autopilot system are:
a) pitch attitude hold
b) altitude hold
c) track hold
d) glide slope intercept and track
b) altitude hold
d) glide slope intercept and track
A semi-automatic landing system disconnects itself automatically when?
at decision height.
during an automatic landing, the autopilot maintains a vertical speed depending on the radio altimeter height, with a constant vertical speed about __ feet/second during the last phase of the flare manoeuvre.
2