Stuck in Detent Monitors for Collective and Cyclic Sticks

In an embodiment, a rotorcraft includes a control element; a first control sensor connected to the control element, the first control sensor operable to generate position data indicating an actual position of the control element; and a flight control computer (FCC) in signal communication with the first control sensor, the FCC being operable to determine a suggested position for the control element, the FCC including an error monitor, the error monitor being operable to compare the suggested position of the control element with the actual position of the control element and determine whether the second control sensor is functional or defective, the FCC being further operable to provide a first flight management function when the second control sensor is determined to be functional, and the FCC being further operable to provide a second flight management function when the second control sensor is determined to be defective.