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A curve setting example is shown below.
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Use the hovering system and set this curve to
match take off and landing and vertical climb at a
constant speed.
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Use this curve in 540
º
stall turn, loop, and rolling stall
turn, and adjust it so the fuselage is facing straight
ahead when heading into the wind.
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This function is set so that the fuselage is facing
straight ahead at straight line auto rotation. The
pitch of the tail rotor becomes nearly 0
º
.
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7KURWWOH FXW SURYLGHV DQ HDV\ ZD\ WR VWRS WKH
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at idle. The action is not functional at high throttle
WR DYRLG DFFLGHQWDO GHDG VWLFNV 7KH VZLWFK¶V
ORFDWLRQDQGGLUHFWLRQPXVWEHFKRVHQDVLWGHIDXOWV
WR18//
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HQJLQH FRQVLVWHQWO\ VKXWV RII EXW WKURWWOH OLQNDJH LV QRW
binding.
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7KHVZDVKPL[IXQFWLRQLVXVHGWRFRUUHFWWKH
VZDVK SODWH LQ WKH DLOHURQ /HIW5LJKW &\FOLF
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corresponding to each operation of each condition.
6. D/R function
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RSHUDWLRQFXUYHRIDLOHURQHOHYDWRUDQGUXGGHUIRU
each condition.
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mentioned "Throttle/Pitch curve setting"
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*\URVHQVLWLYLW\DQGPRGHVZLWFKLQJ
7KH J\UR VHQVLWLYLW\ DQG PRGH VZLWFKLQJ
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PRGHODQGFDQEHVHWIRUHDFKFRQGLWLRQ
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maximum
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sensitivity minimum
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driven helicopter, this function may not have
any effect on the high gyro sensitivity.
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Note: When using a GY601, GY502, GY520,
GY401, or other heading hold gyro, this
Pitch to RUD mixing should not be used. The
reaction torque is corrected by the gyro.
When operating the gyro in the AVCS mode,
the mixed signal will cause neutral deviation
symptoms and the gyro will not operate
normally.
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WKHWRUTXHJHQHUDWHGE\WKHFKDQJHVLQWKHSLWFK
and speed of the main rotor during pitch operation.
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UXGGHUGLRZHYHUZKHQXVLQJDKHDGLQJ
KROGJ\UROLNHWKRVHVKRZQDERYHGRQRWXVH3LWFK
to rudder mixing.
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IXQFWLRQIURPWKH0RGHO0HQXDQGVHWWKHFXUYH
* niet vertaald *
