GRAUPNER Alpha 150Q, Manual

Page: 35 / 48

35 / 48
16571.GPS_Alpha150Q_V2.0sh.en
ALTITUDE HOLD I
This parameter determines the behaviour of the copter in the case
of deviations from the nominal height due to external influences as
a function of the size of the deviation.
This value must be set so that deviations are compensated as well as
possible without the copter oscillating around the desired height.
Otherwise the value must be reduced.
ALTITUDE HOLD D
This parameter determines the behaviour of the copter in the event
of deviations from the nominal height due to external influences as
a function of the acceleration caused by the external influence.
This value must be set so that deviations are compensated as well as
possible without the copter oscillating around the desired height.
Otherwise the value must be reduced.
ALTITUDE HOLD II
This parameter compensates for the time-integrated height differ-
ence.
This value must be set so that the desired height is kept as good as
possible.
This parameter does not usually have to be adjusted.
POS HOLD P
MULTIC. AUTOPILOT
ALT HOLD I 20
ALT HOLD D 30
ALT HOLD II 5
POS HOLD P 50
ALT HOLD P 50
POS HOLD I 20
POS HOLD D 10
POS HOLD II 50
ALT COMING HOME 25
GPS YES 50
This parameter determines the behaviour of the copter in the
case of deviations from the nominal position due to external
influences as a function of the speed of the deviation.
This value must be set so that deviations are compensated as well
as possible without the copter oscillating around the desired
position. Otherwise the value must be reduced.
POS HOLD I
This parameter determines the behaviour of the copter in the case
of deviations from the nominal position due to external influences
as a function of the size of the deviation.
This value must be set so that the copter does not swing around the
set position for a longer time. Otherwise the value must be reduced
or the compass calibration and voltage calibration have to be
repeated.
POS HOLD D
This parameter determines the behaviour of the copter in the event
of deviations from the nominal position due to external influences
as a function of the acceleration caused by the external influence.
This value must be set so that deviations are compensated as well as
possible without the copter oscillating around the desired position.
Otherwise the value must be reduced.