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Section 12.2

Flight Control Systems

The swashplate, collective/cyclic/pedal control, hydraulic servos, mixing and stability augmentation.

Notes

Flight control systems — summary notes

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Main ideas
  • The SWASHPLATE is the heart of helicopter control: a non-rotating (lower) plate and a rotating (upper) plate. The pilot's collective and cyclic move the non-rotating plate; the rotating plate turns with the shaft and drives the blade pitch links.
  • COLLECTIVE raises or lowers the whole swashplate, changing all blades' pitch equally (total thrust). CYCLIC tilts the swashplate, so each blade's pitch changes cyclically once per revolution — tilting the rotor disc to move the aircraft (the input is applied ~90° ahead because of precession).
  • The PEDALS change the tail-rotor blade pitch for anti-torque and yaw; a mixing unit combines collective, cyclic and pedal inputs mechanically before the servos.
  • Powered helicopters use IRREVERSIBLE hydraulic servos (the pilot cannot feel or be back-driven by rotor loads); loss of hydraulic power makes the controls heavy and may limit manoeuvring, so dual/independent hydraulic systems are common.
  • The helicopter is inherently unstable, so a STABILITY AUGMENTATION SYSTEM (SAS/SCAS) and/or autopilot continuously damps and stabilises it; rotor RPM is held by a governor coordinating collective and throttle.
  • ⚠ Exam trap: the SWASHPLATE (stationary + rotating halves) converts fixed collective/cyclic inputs into rotating blade-pitch changes; cyclic changes each blade's pitch ONCE PER REVOLUTION to tilt the disc, and the input leads the desired result by ~90° (precession).
Solved examples
  1. How does moving the cyclic forward cause the helicopter to pitch forward and accelerate?

    Forward cyclic tilts the (non-rotating) swashplate, which cyclically varies each blade's pitch once per revolution. Because of gyroscopic precession the maximum pitch change is applied about 90° before the point where the disc should drop, so the rotor disc tilts forward. The tilted total-rotor-thrust vector now has a forward component, pulling the helicopter forward.

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Flight Control Systems

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