System and method for monitoring aircraft pilot control position and providing a retrim prompt

1. A rotorcraft, comprising:

a pilot control having a sensor configured to generate pilot control position data indicating a pilot control position;

a flight control configured to control a flight characteristic of the rotorcraft;

a trim system connected to the pilot control and configured to move the pilot control; and

a flight control computer (FCC) configured to receive the pilot control position data from the sensor, wherein the FCC is configured to execute a first flight control process, wherein the first flight control process comprises generating first flight control commands and sending the first flight control commands to the flight control to cause the rotorcraft to operate according to the first flight control process, wherein the flight control computer is further configured to generate, according to the first flight control commands, a trim signal indicating a target position for the pilot control and to send the trim signal to the trim system to cause the trim system to attempt to move the pilot control to the target position to reflect a position of the flight control, and wherein the flight control computer is further configured to monitor a working state of the trim system and execute a retrim process in response to determining that the trim system has failed.

2. The rotorcraft of claim 1 , wherein the FCC is further configured to execute the retrim process by terminating the first flight control process and further by executing a second flight control process different from the first flight control process.

3. The rotorcraft of claim 2 , wherein the FCC is further configured to execute the retrim process by providing a retrim prompt.

4. The rotorcraft of Claim 3 , wherein the FCC is further configured to execute the retrim process by terminating the first flight control process in response to a pilot retrim command provided by a pilot after the retrim prompt is provided.

5. The rotorcraft of claim 1 , wherein the FCC is further configured to implement an integrator that determines an error value associated with a difference between the pilot control position and the target position for the pilot control; and

wherein the FCC is further configured to determine the working state of the trim system according to the error value.

6. The rotorcraft of Claim 5 , wherein the FCC is further configured to determine that the trim system has failed in response to the error value exceeding a retrim threshold for a predetermined time.

7. The rotorcraft of claim 6 , wherein the FCC is further configured to determine that the trim system has failed further in response to determining that a pilot has released manual control of the pilot control and that the pilot control is in-detent.

8. A flight control computer (FCC), comprising:

a processor; and

a non-transitory computer-readable storage medium storing a program to be executed by the processor, the program including instructions for:

receiving pilot control position data from a pilot control sensor of a rotorcraft, the pilot control position data indicating a pilot control position of a pilot control associated with the pilot control sensor;

providing a first flight control process by generating first flight control commands according to the first flight control process and operating the rotorcraft according to the first flight control process by sending the first flight control commands to a flight control of the rotorcraft;

generating, according to the first flight control commands, a trim signal indicating a target position for the pilot control associated with a position of the flight control;

sending the trim signals to a trim system to cause the trim system to attempt to move the pilot control to the target position;

determining an operating state of the trim system according to the target position of the pilot control; and

providing a retrim process in response to the determining the operating state of the trim system indicating that the trim system has failed.

9. The FCC of claim 8 , wherein the instructions for providing the retrim process include instructions for:

terminating the first flight control process; and

providing a second flight control process different from the first flight control process.

10. The FCC of Claim 9 , wherein the instructions for providing the retrim process include instructions for providing a retrim prompt.

11. The FCC of claim 10 , wherein the instructions for providing the retrim process include instructions for:

receiving a pilot retrim command provided by a pilot after the retrim prompt is provided; and

terminating the first flight control process in response to the pilot retrim command.

12. The FCC of claim 8 , wherein the program further includes instructions for implementing an integrator that determines an error value associated with a difference between the pilot control position indicated by the pilot control position data and the target position for the pilot control; and

wherein the instructions for determining the operating state of the trim system include instructions to determine the operating state of the trim system according to the error value.

13. The FCC of claim 12 , wherein the instructions for determining the operating state of the trim system include instructions for determining that the trim system has failed in response to the error value exceeding a retrim threshold for a predetermined time.

14. The FCC of claim 13 , wherein the instructions for determining the operating state of the trim system include instructions for determining that the trim system has failed further in response to determining that a pilot has released manual control of the pilot control and that the pilot control is in-detent.

15. A method of operating a rotorcraft, comprising:

receiving, by a flight control computer (FCC), pilot control position data from a pilot control sensor of the rotorcraft, the pilot control position data indicating a pilot control position of a pilot control associated with the pilot control sensor;

providing, by the FCC, a first flight control process by generating first flight control commands according to the first flight control process and operating the rotorcraft according to the first flight control process by sending the first flight control commands to a flight control of the rotorcraft;

generating, by the FCC and according to the first flight control commands, a trim signal indicating a target position for the pilot control associated with a position of the flight control;

sending the trim signals by the FCC to a trim system to cause the trim system to attempt to move the pilot control to the target position;

determining an operating state of the trim system by the FCC and according to the target position of the pilot control; and

providing, by the FCC, a retrim process in response to the determining the operating state of the trim system indicating that the trim system has failed.

16. The method of claim 15 , wherein the providing the retrim process comprises:

terminating the first flight control process; and

providing a second flight control process different from the first flight control process.

17. The method of claim 16 , wherein the providing the retrim process further comprises providing a retrim prompt.

18. The method of claim 17 , wherein the providing the retrim process further comprises:

receiving a pilot retrim command provided by a pilot after the providing the retrim prompt; and

terminating the first flight control process in response to the pilot retrim command.

19. The method of claim 15 , further comprising:

determining an error value associated with a difference between pilot control position indicated by the pilot control position data and the target position for the pilot control; and

wherein the determining the operating state of the trim system comprises determining the operating state of the trim system according to the error value.

20. The method of claim 19 , wherein the determining the operating state of the trim system further comprises determining that the trim system has failed in response to the error value exceeding a retrim threshold for a predetermined time.