A method is used to generate an indication value for locking a P flight parameter from an automatic pilot's flight group.

摘要

The present invention relates to a method for generating an instruction value for servo of P flight parameters of an aircraft equipped with an automatic pilot.Between the current value C and the target value T, it includes the stage of determining the increased or decreased PC instruction values of P flight parameters, their time derivatives and/or their integral instruction values. It also includes a usage phase through a servo law of the automatic boot parameter P for each PC instruction value.And/or also includes a stage in which the automatic driver of the T value uses it as the final target value. PC instruction valueAnd/or based on the current value C,Target values T and TAU time constants of TAU parameters.