Cyclic/collective pitch mixing

From Wikipedia, the free encyclopedia
Jump to navigation Jump to search

Cyclic/collective pitch mixing (CCPM) is a control concept employed in collective pitch radio-controlled helicopters.[1] CCPM reduces mechanical complexity and increases precision of control of the helicopter rotor's swashplate.

Conventional operation[edit]

Older model helicopters use three independent servos to manipulate the swashplate. The elevator servo is used to tilt the swashplate forward and aft (longitudinal cyclic), varying the aircraft's pitch. The aileron servo is used to tilt the swashplate left and right (lateral cyclic), varying the aircraft's roll. The collective pitch servo raises and lowers the entire swashplate, varying the collective, and hence the pitch of all the rotor blades collectively. An intermediate mechanical mixing system is used to transfer the control inputs from the servos to the swashplate, therefore the name of mechanical CCPM (mCCPM).[2] This requires an elaborate system of control rods and levers, which often contains many ball bearings.

Electronic mixing[edit]

To reduce the mechanical complexity, newer model helicopters use a software system (usually running on the transmitter) to mix the control inputs of three interdependent servos to control the swashplate.[2] The three servo linkages are arranged around the swashplate at 120° intervals (there is a variation that uses 140° + 140° + 80° intervals). In addition to lower mechanical complexity, the interdependent servos share the workload.

See also[edit]


  1. ^ "What is CCPM and why it's so important". Retrieved 28 October 2014. 
  2. ^ a b "What is the deal with mCCPM and eCCPM?". Retrieved 28 October 2014. 

External links[edit]