Outer-loop monitor for aircraft automatic flight control system

Claim 1

A monitor for providing a fault signal indicative of a failure in a position control system having an inner-loop actuator positionable in response to an inner-loop error signal over a limited range of positions which is a fraction of a full range of control system positions, means for providing the inner-loop error signal as a function of the difference between the actual inner-loop actuator position and a dictated inner-loop actuator position, means for providing an outer-loop command signal, which is a pulse, when the inner-loop error signal is indicative of at least a substantial portion of the limited range of inner-loop actuator positions, and an outer-loop actuator, positionable over the full range of control system positions and connected to the inner-loop actuator for adjusting the limited range of the inner-loop actuator in response to the outer-loop command signal pulses within the full range so that the inner-loop actuator is positionable over the full range of positions, said monitor comprising: means (46) for providing an intermediate fault signal when the sense of the outer-loop command signal (D,E) disagrees with the sense of the inner-loop error signal (A,B); means (38) for providing a limited time signal at the onset of an outer-loop command signal pulse and for a predetermined limited time thereafter, said limited time being of duration less than that of the pulse; and means (42) for providing the fault signal (C) in response to the intermediate fault signal when the limited time signal is also present.