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- Rudder, ailerons, elevators, spoilers and canards for aircraft. - Canards and fins for missiles.
- E.g. the canard angles are usually 'c, etc. - The guidance law will generate a required acceleration, and a linearised airframe transfer function will be used to convert this acceleration into a value for the various control surface angles.
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Electronic engine control systems : Advances in gas turbine technology have demanded more precise control of engine parameters than can be provided by hydromechanical fuel cont
THE PITCH CHANGE MECHANISM : The cylinder backplate . The disc shaped backplate provides a mounting for the pitch change cylinder. This backplate fits in front of the propel
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