117
<Functions of Model Menu (Helicopter Functions)>
S1
button
EDIT
button
EDIT
dial
ŏ3XVKWKH
S1
EXWWRQIRU
VHFRQGWRUHWXUQWRWKH
KRPHVFUHHQ
ŏ7XUQ WKH
E D I T
GLDO WR
PRYHRQWKHVFUHHQ
ŏ6 H O H F W W K H I X Q F W L R Q
QDPH DQG UHWXUQ WR WKH
S U H F H G L Q J V F U H H Q E \
SXVKLQJWKH
EDIT
EXWWRQ
PIT to RUD mixing (Revolution mixing)
Use this mix when you want to suppress the
reaction torque generated by main rotor pitch and
speed changes during pitch operation. Adjust so
that the nose does not move in the rudder direction.
An acceleration function which temporarily
increases the correction rate at throttle stick
acceleration/deceleration operation can be set. The
mixing rate at acceleration/deceleration can be set.
Setting method
ŏ:KHQXVLQJWKLVIXQFWLRQPRYHWKHFXUVRUWR
WKH >$&7@ LWHP DQG SXVK WKH (',7 EXWWRQ WR
VZLWFKWRWKHGDWDLQSXWPRGH7XUQWKH(',7
GLDOWRWKHOHIWDQGSXVKWKH(',7EXWWRQ21
LVGLVSOD\HG
ŏ:KHQ\RXZDQWWRVHWWKHVDPHFRQWHQWVDWRWKHU
FRQGLWLRQVVHOHFWWKHJURXSPRGH
:KHQ\RXZDQWWRVHWWKHVHOHFWHGFRQGLWLRQRQO\
VHOHFWWKHVLQJOHPRGHLQLWLDOVHWWLQJ
ŏ$PL[LQJFXUYHLVVHW
<Normal condition mixing curve>
7KH PL[LQJ FXUYH UDWH VWDUWV IURP D VPDOO
YDOXH
)RU D URWRU ZLWK D FORFNZLVH RSHUDWLRQ
GL U H FWL RQ SR O D U L W\ ZK H Q S L WFK ZD V
RSHUDWHGDWWKHSOXVVLGHVHWVRWKDWPL[LQJ
LV LQ WKH FORFNZLVH GLUHFWLRQ )LUVW WULP DW
KRYHULQJ DQG WKHQ DGMXVW WKH QHXWUDO
SRVLWLRQ
$GMXVWPHQWEHWZHHQVORZDQGKRYHULQJ
5HSHDWHGO\ KRYHU IURP WDNH RII DQG ODQG
IURPKRYHULQJDWDFRQVWDQWUDWHPDWFKHG
WR\RXURZQUK\WKPDQGDGMXVWWKHSLWFKVR
WKHQRVHGRHVQRWGHÁHFWZKHQWKHWKURWWOH
LVUDLVHGDQGORZHUHG
7KURWWOHKLJKVLGHFOLPELQJDQGGLYLQJIURP
KRYHULQJ
5HSHDW FOLPELQJ DQG GLYLQJ IURP KRYHULQJ
DW D FRQVWDQW UDWH PDWFKHG WR \RXU RZQ
UK\WKPDQGDGMXVWWKHSLWFKVRWKDWWKHQRVH
GRHVQRWGHIOHFWZKHQWKHWKURWWOHLVUDLVHG
DQGORZHUHG
However, when a GY Series or other heading
hold gyro is used, since correction is performed
by the gyro, this mix is not used. If this function
is used when the gyro operation mode is the
AVCS mode, the neutral position will change.
<Idle up condition mixing curve>
6HWWKHPL[LQJUDWHVRWKDWWKHUXGGHUGLUHFWLRQ
DWKLJKVSHHGÁLJKWLVVWUDLJKWDKHDG$GMXVWIRU
HDFKFRQGLWLRQXVHG
<Acceleration function setting>
ŏ$FFHOHUDWLRQRSHUDWLRQFDQEHSHUIRUPHG
IRUERWKVHWWLQJDWDFFHOLJKDQG
VHWWLQJDWGHFHOHUDWLRQ/RZ
ŏ$FFHOHUDWLRQUDWHVHWWLQJ5DWH
ŏ7KHUHWXUQWLPHDIWHURSHUDWLRQ'XPSLQJ
FDQEHVHW
ŏ $ Q R S H U D W L R Q S R L Q W $ F W 3 R V D W
DFFHOHUDWLRQDQGGHFHOHUDWLRQFDQEHVHW
LQGHSHQGHQWO\ :KHQ DQ RSHUDWLRQ SRLQW
ZDV H[FHHGHG DFFHOHUDWLRQ RSHUDWLRQ LV
SHUIRUPHG
ŏ1RUPDOO\XVH>32,17@W\SH
ŏ6HOHFW>3,7WR58'@DWWKHPRGHOPHQXDQGFDOOWKH
VHWXS VFUHHQ VKRZQ EHORZ E\ SXVKLQJ WKH (',7
EXWWRQ
(Currently selected condition name)
ŏ3XVK WKH
S1
EXWWRQ WR
FDOOQH[WSDJH
ŏ$FFHOHUDWLRQVHWWLQJV
