JPH11263297A - Automatic maneuvering device - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide an automatic maneuvering device with high operability in conducting shifting between manual maneuver and automatic maneuver. SOLUTION: An actuator 12 displaces the neutral position of a maneuvering rod 11 so that it may agree with a target value Sa. A position detector 13 detects the position of the maneuvering rod 11 and outputs a detected value Sb. A subtracter 14 computes a deviation obtained by subtracting the detected value Sb from the target value Sa. An override detector 15 fixes the target value Sa if the deviation is a threshold value L or higher, and varies the target value Sa if the deviation is less than the threshold value. A limiter 16 outputs the threshold value L if the deviation in a threshold value L or higher and outputs the deviation if the deviation is less than the threshold value L. An adder 17 adds an outputted value from the limiter 16 to the detected value Sb. It is thus possible to conduct switching between manual maneuver and automatic maneuver.

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an automatic control device for automatically controlling a body of an aircraft such as an aircraft when the pilot does not operate the control stick.

[0002]

2. Description of the Related Art An automatic pilot device for an aircraft (autopilot) is a device that gives a plurality of appropriate passing points in the middle of a planned flight path and automatically controls a flight connecting the passing points. It is. Some recent aircraft are equipped with such an autopilot. Autopilots include the following mainly.

As shown in FIG. 3, a helicopter automatic control device 1 having a mechanical or hydraulic control system uses a trim actuator 2 for automatic control input without a pilot. The trim actuator 2 is
It is installed at the base of the control stick 3 and displaces the neutral position of the control stick 3. The control stick 3 is a stabilizing device (SAS; St.
The actuator is mechanically connected to a control surface 6 via a SAS actuator 5 that is displaced by an input from an ability augment system 4.

As shown in FIG. 4, Fly-By-Wire (FB)
The helicopter autopilot having a W) or Fly-By-Light (FBL) control system has no mechanical connection between the control stick 3 and the control surface 6, and An electric signal of the control surface actuator 7 is directly operated by an FBW computer 8 electrically connected therebetween.

US Pat. No. 5,197,697 is a prior art having an FBW control system or an FBL control system, in which a signal obtained by performing a dead band process on a deviation between the position of a control stick and a target value is added to the target value.

[0006]

SUMMARY OF THE INVENTION An object of the present invention is to provide an FB
An object of the present invention is to provide an autopilot having the same performance as an autopilot used in an aircraft having a conventional mechanical or hydraulic control system in an aircraft using a W control system or an FBL control system.

The present invention can solve the above problems only by the present invention, and also has an effect of greatly improving the reliability of the automatic pilot device of the aircraft. That is, the improvement of the reliability by the multi-system configuration is common in aircraft, and the software uses a decimirror technology (multi-system software is independently developed) to improve the reliability. In the conventional case, the software created is based on the same block diagram. The present invention realizes exactly the same function as US Pat. No. 5,197,697 in different blocks. Therefore, the present invention makes it possible to realize a more sophisticated desi mirror by using US Pat. No. 5,197,697, and to obtain higher reliability.

[0008]

SUMMARY OF THE INVENTION The present invention relates to an automatic steering device which takes in a target value output from an automatic steering computer and outputs a steering amount to a steering device of the fuselage. A rod, an actuator for displacing the neutral position of the control stick so as to match the target value, a position detector for detecting the position of the control stick, and subtraction for calculating a deviation obtained by subtracting the detected position value of the control stick from the target value If the deviation is equal to or greater than a predetermined threshold L, it is determined that there is an override, and an instruction is issued to the autopilot computer to fix the target value.
If the difference is less than the threshold L, the override detector outputs a threshold L if the difference is equal to or greater than the threshold L. And an adder that outputs a steering amount obtained by adding an output value from the limiter to a position detection value of the control stick.

According to the present invention, when there is no input from the pilot to the control stick, the actuator causes the neutral position of the control stick to match the target value, and the control stick is arranged at the position of the target value. Is smaller than the threshold value L. At this time, the override detector changes the target value, and the limiter outputs the deviation. Therefore, the variable target value is output from the adder, and the aircraft performs an operation in which the target value is reflected, that is, performs automatic control.

On the other hand, when the pilot gives an override input to the control stick, the actuator causes the neutral position of the control stick to match the target value, but since the control stick is disposed at a position having a deviation L or more from the target value, the target The deviation between the value and the position detection value is equal to or greater than the threshold L. At this time, the override detector fixes the target value and the limiter outputs the threshold value L.
The sum of the position detection value and the threshold value L is output from the adder, and the aircraft executes an operation reflecting the variable position detection value, that is, a manual operation. The fixed target value when the override input is detected becomes variable again when the deviation between the position detection value and the fixed target value becomes smaller than L, and the variable target value is output from the adder. Output, that is, the autopilot is restarted.

As described above, the pilot can automatically control the aircraft by not inputting to the control stick, and can manually control the aircraft by inputting the override to the control stick. Therefore, in an aircraft using the FBW control system or the FBL control system, it is possible to realize the same performance as an automatic pilot device used in an aircraft having a conventional mechanical or hydraulic control system.

In the present invention, similar functions are realized by blocks different from those in US Pat. No. 5,197,697.
Therefore, by using the present invention in combination with U.S. Pat. No. 5,197,697, it is possible to realize a more sophisticated desi-mirror, and to obtain higher reliability.

[0013]

FIG. 1 is a diagram showing an electric configuration of an embodiment of the present invention. The autopilot 10 includes a control stick 11, an actuator 12, a position detector 13, and a subtractor 1.
4. An apparatus that includes an override detector 15, a limiter 16, and an adder 17, and automatically controls an aircraft. The target value generator 21 calculates and generates a neutral position as a target of the control stick 11, that is, a target value, and inputs the target value to the autopilot device 11.

The control stick 11 is provided in the cockpit of the aircraft, and can be operated by a pilot. The actuator 12 displaces the neutral position of the control stick 11 so as to match the target value. The position detector 13 is
The sensor detects the absolute position of the control stick 11. The subtractor 14 calculates a deviation obtained by subtracting the position detection value of the control stick 11 from the target value. If the deviation is equal to or greater than the predetermined threshold L, the override detector 15 determines that there is an override and gives a command to fix the target value to the target value generation unit 21. An instruction to change the target value is given to the value generation unit 21. The limiter 16 outputs the threshold L if the deviation is equal to or larger than the threshold L, and outputs the deviation if the deviation is smaller than the threshold L. The adder 17 adds the output value from the limiter 16 to the position detection value of the control stick 11, and uses the result as the steering amount of the aircraft.
Output to 2.

The control section 22 outputs the steering amount directly to a steering device such as a control surface actuator of the aircraft to control the steering device. Note that the target value generation unit 21 and the control unit 22
May be configured by a single circuit, respectively, or may be configured as a part of a function of a computer that performs a general operation of flight control.

FIG. 2 shows the control stick 11 and the actuator 12. The control stick 11 is a rod-shaped member, one end 31 of which is swingably supported, and has a grip 32 at the other end for a pilot to grip. One end of the actuator 12 is supported by the base of the control stick 11, and swings the control stick 11 around the end 31. The absolute position of the control stick 11 is represented by the angle of the control stick 11, and the neutral position of the control stick 11 is represented by a position at which the control stick 11 does not receive a force from the actuator 12.

Next, the flow of signals in the autopilot 10 will be described below. First, the target value generated by the target value generation unit 21 is defined as Sa. The target value Sa is sequentially generated by the target value generation unit 21 and varies with time. Target value Sa
Is output to the actuator 12 and the subtractor 14. It is assumed that the position detector 13 outputs a detection value Sb of the absolute position of the control stick 11. The detected value Sb is sent to the subtractor 14 and the adder 17. The difference (Sa−Sb) is output from the subtractor 14 and sent to the override detector 15 and the limiter 16.

In the override detector 15, the absolute value | Sa−Sb | of the deviation is compared with a threshold value L, and the absolute value | Sa−
If Sb | is equal to or greater than the threshold L, the target value Sa generated by the target value generator 21 is fixed at the current target value SA, and if the absolute value | Sa-Sb | Sa is kept as it is, and time is freely changed. In the limiter 16, the absolute value | Sa-Sb | of the deviation is compared with a threshold value L. If the absolute value | Sa-Sb | is equal to or larger than the threshold value L, sgn (Sa-Sb) · L is output, and the absolute value | Sa−Sb | ｜ S
If a−Sb | is smaller than the threshold value L, the deviation (Sa−S
b) is output as it is. Where sgn (X) is
This function is 1 when X is equal to or greater than zero and -1 when X is less than zero. From the adder 17, Sa or Sb + s
gn (Sa−Sb) · L is output.

In such an automatic control device 10, when there is no input from the pilot to the control stick 11, the actuator 12 makes the neutral position of the control stick 11 coincide with the target value Sa, and the control stick 11 sets the target value Sa to the target value Sa. Placed in the position. Deviation between target value Sa and detected value Sb (Sa-Sb)
Is smaller than the threshold value L, the override detector 15 changes the target value Sa. The limiter 16 determines the deviation (Sa
-Sb) is output. Therefore, the adder 17 finally outputs a variable target value Sa, and the aircraft outputs the target value Sa.
Perform a flight that reflects.

On the other hand, when the pilot gives an override input to the control stick 11, the actuator 12
1 is adjusted to the target value Sa, but the control stick 11
Is arranged at a position that is at least a deviation L from the target value Sa. Absolute value of deviation between target value Sa and detection value Sb | Sa-Sb |
Is greater than or equal to the threshold L, the override detector 15 fixes the target value Sa to the current target value SA. Limiter 1
6 outputs the threshold value L. The sum (Sb + L) of the detection value Sb and the threshold value L is finally output from the adder 17, and the aircraft performs a flight reflecting the detection value Sb.

The target value SA fixed when there is an override input returns to the variable target value Sa again when the deviation between the detected value Sb and the fixed target value SA becomes less than L, The adder 17 outputs a variable target value Sa.

[0022]

As described above, according to the present invention, in an aircraft using an FBW control system or an FBL control system, an automatic pilot device used in an aircraft having a conventional mechanical or hydraulic control system is provided. Equivalent performance can be achieved.

Further, by using the present invention in combination with US Pat. No. 5,197,697, it is possible to realize a more sophisticated desi-mirror and obtain higher reliability.

[Brief description of the drawings]

FIG. 1 is a block diagram showing an electrical configuration of an embodiment of the present invention.

FIG. 2 is a view showing a control stick 11 and an actuator 12;

FIG. 3 is a view showing a conventional mechanical autopilot 1;

FIG. 4 is a diagram showing a conventional FBW automatic steering device.

[Explanation of symbols]

 Reference Signs List 10 autopilot device 11 control stick 12 actuator 13 position detector 14 subtractor 15 override detector 16 limiter 17 adder 21 target value generation unit 22 control unit Sa target value Sb detection value L threshold

[Procedure amendment]

[Submission date] March 12, 1999

[Procedure amendment 1]

[Document name to be amended] Statement

[Correction target item name] Claims

[Correction method] Change

[Correction contents]

[Claims]

[Procedure amendment 2]

[Document name to be amended] Statement

[Correction target item name] 0008

[Correction method] Change

[Correction contents]

[0008]

SUMMARY OF THE INVENTION The present invention relates to an automatic steering device which takes in a target value output from an automatic steering target value generation section and outputs a steering amount to a steering device of an airframe. A possible control stick, an actuator that displaces the neutral position of the control stick to match the target value, a position detector that detects the position of the control stick, and a deviation obtained by subtracting the detected value of the control stick position from the target value If the subtractor to be calculated and the deviation is equal to or greater than a predetermined threshold L, an instruction to fix the target value is given to the autopilot target value generation unit by regarding that there is an override,
If the deviation is less than the threshold L, an override detector that gives an instruction to make the target value variable to the autopilot target value generation unit assuming that there is no override, and if the deviation is greater than or equal to the threshold L,
A limiter that outputs a threshold L and outputs a deviation if the deviation is less than the threshold L; and an adder that outputs a steering amount obtained by adding an output value from the limiter to a position detection value of the control stick. It is an automatic pilot device.

Claims (1)

[Claims] 1. An automatic steering device which takes in a target value output from an automatic steering computer and outputs a steering amount to a steering device of an airframe, wherein a control rod operable by a pilot and the target value coincide with each other. An actuator for displacing the neutral position of the control stick, a position detector for detecting the position of the control stick, a subtractor for calculating a deviation obtained by subtracting the position detected value of the control stick from a target value, and a predetermined threshold for the deviation. If L is greater than or equal to L, an instruction is given to fix the target value to the autopilot computer assuming that there is an override. A detector, if the deviation is greater than or equal to the threshold L, a threshold L is output; if the deviation is less than the threshold L, a limiter that outputs the deviation; and a control bar position detection value output from the limiter. Autopilot, characterized in that it comprises an adder which outputs a steering amount obtained by adding the.