Integrated upsampler and filtering for multi-rate controller for electromechanical flight actuation system

Patent metadata

Field	Value
Publication number	US-9405277-B2
Application number	US-201414182151-A
Country	US
Kind code	B2
Filing date	Feb 17, 2014
Priority date	Sep 28, 2010
Publication date	Aug 2, 2016
Grant date	Aug 2, 2016

Abstract

A multi-rate system for controlling an actuator may include an incremental command limiter that receives a command from a first control system and outputs a limited incremental command; a feed-forward that receives the limited incremental command from the incremental command limiter and outputs a feed forward rate command; a first differentiator that limits the limited incremental command to a maximum allowable command; an upsampler state that outputs a current state back to the differentiator; a first summer that receives the limited incremental command and the current state from the upsampler state, and outputs an incremental position command; and a second summer that combines the incremental position command and the feed forward rate command to produce a rate error output signal.

First claim

What is claimed is:

1. A multi-rate system for controlling an actuator, the system comprising:
an incremental command limiter that receives a command from a first control system and outputs a limited incremental command;
a feed-forward that receives the limited incremental command from the incremental command limiter and outputs a feed forward rate command;
a first differentiator that limits the limited incremental command to a maximum allowable command;
state of position command that outputs a current state back to the differentiator;
a first summer that receives the limited incremental command and the current state and outputs an incremental position command; and
a second summer that combines the incremental position command and the feed forward rate command to output a rate error output signal.

2. The multi-rate system of claim 1 , further comprising a lead-lag filter that receives the limited incremental command from the incremental command limiter, and filters the limited incremental command to the feed forward.

3. The multi-rate system of claim 2 , wherein the lead-lag filter filters the limited incremental command to the first summer.

4. The multi-rate system of claim 1 , further comprising a second differentiator that receives and compares the incremental position command from the first summer to a position feedback signal to derive a position error signal.

5. The multi-rate system of claim 4 , wherein the second summer receives the position error signal as a rate command, the feed forward rate command, and a rate feedback to produce the rate error output signal.

6. The multi-rate system of claim 5 , further comprising a first amplifier that receives the position error signal from the second differentiator and produces the rate command received by the second summer.

7. The multi-rate system of claim 1 , further comprising a second amplifier that receives the rate error output and converts the rate error output to a torque command.

8. The multi-rate system of claim 7 , further comprising an actuator that receives the torque command.

9. The multi-rate system of claim 1 , wherein the incremental command limiter differences a one time-step delayed position command from a last received position command from the first control system to produce a signed difference signal.

10. The multi-rate system of claim 9 , wherein the incremental command limiter includes a first function that depolarizes the signed difference signal to generate an unsigned difference signal whose value is an unpolarized absolute value limited to an increment no larger than an intended rate command from the first control system.

11. The multi-rate system of claim 10 , wherein the incremental command limiter includes a bias that is added to the unsigned difference signal prevent sluggish motion.

12. The multi-rate system of claim 10 , wherein the incremental command limiter includes a second function that receives the unsigned difference signal and updates the output of the second function when the unsigned difference signal has a positive change.

13. The multi-rate system of claim 12 , wherein the incremental command limiter includes a third function that divides a conditionally updated signal from the second function into smaller incremental changes according to a ratio of the sample rate of the first control system and a second control system having a greater sample rate than the first control system.

14. An aircraft comprising:
an actuator;
a position/rate feedback sensor that is connected to the actuator;
a flight control system having master computer and a flight actuator controller, the master computer connected to send a command signal to the flight actuator controller, and the flight actuator controller connected to send an actuation signal to cause the actuator to reposition the flight control surface, wherein the master computer sends the command signal at a first sample rate, and the flight actuator operates at a second, different sample rate; and
an integrated upsampler associated with the flight actuator controller and connected to receive the command signal from the master computer and produce a command to the actuator, the integrated upsampler including
an incremental command limiter that receives a command from the master computer and outputs a limited incremental command;
a feed-forward that receives the limited incremental command from the incremental command limiter and outputs a feed forward rate command;
a first differentiator that limits the limited incremental command to a maximum allowable command;
an upsampler state that outputs a current state back to the differentiator;
a first summer that receives the limited incremental command and the current state from the upsampler state, and outputs an incremental position command; and
a second summer that combines the incremental position command and the feed forward rate command to produce a rate error output signal.

15. The aircraft of claim 14 , further comprising a lead-lag filter that receives the limited incremental command from the incremental command limiter, and filters the limited incremental command to the feed forward and to the first summer.

16. The aircraft of claim 15 , further comprising a second differentiator that receives and compares the incremental position command from the first summer to a position feedback signal to derive a position error signal, and wherein the second summer receives the position error signal as a rate command, the feed forward rate command, and a rate feedback to produce the rate error output signal.

17. The aircraft of claim 16 , further comprising a first amplifier that receives the position error signal from the second differentiator and produces the rate command received by the second summer; and a second amplifier that receives the rate error output and converts the rate error output to the actuation signal.

18. The aircraft of claim 14 , further comprising a flight control surface that is connected to be controller by the actuator.

19. The aircraft of claim 14 , wherein the second sample rate is greater than the first sample rate.

20. A method for integrating multi-rate control systems having different sample rates, the method comprising:
receiving by an incremental command limiter a command from a first control system, and outputting a limited incremental command;
receiving the limited incremental command by a feed-forward, and outputting a feed forward rate command;
a first differentiator that limits the limited incremental command to a maximum allowable command;
outputting by an upsampler state a current state back to the differentiator;
receiving by a first summer the limited incremental command and the current state from the upsampler state, and outputting an incremental position command; and
combining by a second summer the incremental position command and the feed forward rate command to produce a rate error output signal.

21. A multi-rate system for controlling an actuator, the system comprising:
an upsampler that receives a position command from a first control system, rate limits and filters the position command to output a feed forward rate command and a limited incremental command;
the upsampler including a state of position command that receives the limited incremental command and a current state of position command, and outputs an incremental position command; and
a processing network that receives the incremental position command and the feed forward rate command from the

Assignees

• Boeing Co

Inventors

• Cameron Douglas C

Classifications

• B64C19/00

  Aircraft control not otherwise provided for · CPC title

• G05B6/02 Primary

  electric · CPC title

• G05B2219/41427

  Feedforward of position · CPC title

• G05B11/01 Primary

  electric · CPC title