Balancing inputs to the swashplate to equilise torsional loads on the blades
Hello, fellow rotorheads!
I've been going trough the syllabus for Aircraft general knowledge and stumbled upon a learning objective at Helicopter: Flight Controls and it goes like this:
"Describe the swashplate or azimuth star control system including the following:
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- balancing of pitch/roll/collective inputs to the swashplate to equilise torsional loads on the blades"
If someone could please explain what's up with this question or at least point me in the direction where I could find an explanation for it.
Thank you!