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Back to: "P"pitch control
- Fonte1
- INTERNATIONAL CIVIL AVIATION ORGANIATION. Annex 8 to the Convention on International Civil Aviation. Airworthiness of aircraft. 11th ed. Montreal, 2010.
- Nota adicional1
- The cyclic pitch control system is designed so that the rotor disc tilts slightly opposite tail rotor thrust when in a hover.
- Contexto
- The cyclic pitch control changes the pitch of each blade as a function of where it is in the plane of rotation. This allows for trimming the helicopter in pitch and roll during forward flight and for maneuvering in all flight conditions.
- Subárea
- Aerodynamics
- Related Term
- collective pitch control
- cyclic pitch control
- nose down pitch control
- pitch control effect
- pitch effect
- Spanish
- control de cabeceo