The computers of the electrical flight controls system comply with programs defined by attitude control laws such as: on the longitudinal axis, the law may combine the load factor and the changes in the pitch rate as control data sources the trimming is automatic and ensures neutral stability the protections apply to pitch and bank attitudes depending on the speed these laws do not apply to the whole flight envelope The combination regrouping all the correct statements is: A. 1, 2, 3, 4. B. 2, 3. C. 1, 2, 3. D. 1, 3, 4.

 

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