Replies: 3 comments 1 reply
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Hi Maksim, First,sorry for the very long delay before answering your message. I am not sure where the coefficient
The gyroscopic torque that is computed by JSBSim is not the gyroscopic torque of the propeller upon itself but instead the gyroscopic torque that the propeller applies to the whole aircraft. In the file
Since the propeller is rotating in its local frame axis |
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The expression Actually, I can formulate a simple question: where did you take this term |
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@msurov here is the relevant snippet in case you don't have access to Aircraft Control and Simulation - 3rd edition by Stevens, Lewis and Johnson. |
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I am looking at the code computing the gyroscopic torque at FGPropeller.cpp:284-295:
and a bit confused. The reason is it's missing the coefficient 0.5 in
Ixx*omega*Sense*Sense_multiplier
term. Actually, the gyroscopic torque depends on the differencesIxx-Iyy
andIxx-Izz
. According to the documentation the valuesIyy,Izz
are not supported. Nevertheless, If the propeller is thought as 4-blades or just a disk, thenIyy = Izz = 0.5 * Ixx
. If the propeller is 2 blades, then vibrations will occur, but the average value of the torque also needs coefficient0.5
.Also, the sign of the resulting torque seems incorrect (upt: sorry, this bug was already fixed).
Where this formula is taken from?
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