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Match each augmentation loop with the derivative it effectively augments.

List I

A. Yaw rate to rudder

B. Sideslip to rudder

C. Roll rate to ailerons

List II

P. Roll damping

Q. Yaw damping

R. Directional stiffness

Select the correct match.

  • A.A-Q, B-P, C-R
  • B.A-P, B-R, C-Q
  • C.A-Q, B-R, C-P
  • D.A-R, B-Q, C-P

Answer: C

Rate feedback augments damping and displacement feedback augments stiffness, on whichever axis the signal and the surface share, so A-Q, B-R, C-P. The rule generalises: measure a rate and you add damping to that axis, measure a displacement and you add stiffness. It is the fastest way to reason about an unfamiliar control law, and it explains why a yaw damper does nothing for the spiral, which needs a bank-angle loop instead.

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