Manual Graupner GR-24 PRO (page 36 of 51) (English)

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S1019_S1034_S1035_33579_33583_FW2_DE_V1.0sh

Expert mode "Yes"

Base sett control

Tail servo 1,5ms

Tail frequency 333Hz

Tail mid +0

Tail limit B +50

4.Swp servo mid +0

Logging +3

Expert mode Yes

As soon as the "Expert mode" opon on the last line of the display

page "Basic seng control" is set to "Yes", further opons are avail-

able on the display pages "Swash seng" and "Tail rotor sengs".

Regardless of "yes / no", however, the associated sengs are always

eﬀecve. Switching to "no" thus does not switch oﬀ these opons,

but only fades them out again.

P tail

I tail +70

P tail +80

D tail +15

Tail dynamic +65

Vivration damping No

Stop damping R +5

Stop damping L +5

Tail rotor settin

Tail sensitivity 65

Tail rate +85

Tail expo +40

Pitch- Tail +25

Swp- Tail +4

The "P tail" opon is responsible for eﬀecng a harder stop with the

tail. Higher values result in a faster stop. If the P values are too high,

the tail will start to "oscillate". In such cases, the value must be

reduced again.

Adjustment range: +40 … +125

I tail

The I-factor ensures constant piroueng. Start with low values and

only increase them unl the pirouees are constant. If the values are

too high, this will cause the tail to oscillate slowly.

Adjustment range: +20 … +100

D tail

The D-factor inﬂuences how the tail is stopped. If the tail bounces

somewhat when the tail is stopped, this parameter should ﬁrst be

increased in 5-degree increments to test the tail stop.

Adjustment range: 0 … +50

Note on "P / I / D tail"

The control is based on the PID principle, where the "P" stands for

"proporonal", the "I" for "integral" and the

"D" for "digital". In short

...

... the deviaon from the setpoint proporonal to the manipulated

variable has an eﬀect at the P value.

... the exisng control deviaon is connuously summed up at the I

value and then acts on the manipulated variable via the I value.

... the diﬀerenal component only takes into account the speed of

the control deviaon and then acts on the control accordingly via the

D component.

Pitch => Tail and Swp => Tail

Torque compensaon for pitch and tail is opmal when the two

opons are adjusted together.

• Pitch => Tail

With rapid successive pitch changes (pitch pumping) and the

resulng swashplate movements, the tail should remain stable

also during the load. If the tail swings out shortly, "Pitch => Tail"

should be increased unl the tail is sll.

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Graupner GR-24 PRO Manual

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