JP2016088348A - Rudder controller, underwater vehicle and rudder control method - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a rudder controller which can obtain a flow force rudder angle more approximate to a target flow force rudder angle even when there exists a rudder getting outside a steerable range out of four rudders that constitute an X type rear rudder, an underwater vehicle and a rudder control method.SOLUTION: A rudder controller 2 that controls the rudder angle of rudders 111-114 of an underwater vehicle 1 comprises: an apart 20, which accepts an input of target flow force rudder angles that the target values of a pitch rudder angle, a yaw rudder angle and a roll rudder angle; a necessary rudder angle specification part 21, which specifies necessary rudder angles that are rudder angles of each of rudders 111-114 necessary to obtain the target flow force rudder angles; a first rudder angle determination part 221, which determines rudder angles of one rudder with a necessary rudder angle out of rudders 111-114 getting outside a steerable range and rudder angles of another rudder capable of rotating around the same axis as the one rudder; and a second rudder angle determination part 222, which determines rudder angles of a rudder other than a rudder the rudder angle of which is determined by the first rudder angle determination part 221.SELECTED DRAWING: Figure 3

Description

  The present invention relates to a rudder control device, an underwater vehicle, and a rudder control method.

  In recent years, in an underwater vehicle, an X-type rear rudder that can obtain a more efficient rudder force has been adopted in place of posture control by a cross-shaped rear rudder composed of a horizontal rudder and a vertical rudder. By adopting the X-type rear rudder, theoretically, the same rudder force as that of the cross-type rear rudder can be obtained with an area 1 / √2 times that of the cross-type rear rudder.

  On the other hand, a rudder control device or the like for controlling each of the four rudders constituting such an X-type rear rudder has been proposed (see, for example, Patent Document 1).

JP 2009-234393 A

  In general, for the control of the rudder constituting the X-type rear rudder, first, a target flow rudder angle (pitch rudder angle, yaw rudder angle and roll rudder angle) based on the cross-shaped rear rudder is calculated, A method of distributing to each rudder angle of the four rudders constituting the rear rudder is adopted. However, each of the four rudders has a predetermined steerable range, and the rudder angle can be changed only within the steerable range. Then, as a result of the distribution, if there is even one rudder that is out of the steerable range, the distribution balance may be lost, and any target flow force steering angle may not be obtained.

  The object of the present invention is to obtain a fluid rudder angle that is closer to the target fluid rudder angle even when there is a rudder that is out of the steerable range among the four rudders constituting the X-type rear rudder. The present invention provides a rudder control device, an underwater vehicle, and a rudder control method.

  One aspect of the present invention includes two rudders which are in a vertical plane of the hull and are rotatable about a first axis inclined at 45 degrees with respect to the horizontal plane of the hull, and the first axis in the vertical plane of the hull. A rudder control apparatus for controlling the rudder angle of the rudder of an underwater vehicle including a total of four rudders, two rudders that are rotatable about a second axis orthogonal to the pitch rudder angle, yaw An input unit for receiving an input of a target flow force steering angle that is a target value of a steering angle and a roll steering angle, and a necessary steering angle that is a steering angle of each of the rudder necessary to obtain the target flow force steering angle A steering angle of one rudder that is out of the steerable range when at least one of the four rudders is out of the steerable range. The limit value of the steerable range is determined, and it can be rotated about the same axis as the one rudder. A first rudder angle determination unit that determines the rudder angle of the rudder as the necessary rudder angle or a limit value of the steerable range, and an undecided rudder other than the rudder for which the first rudder angle determination unit has determined the rudder angle A pitch rudder angle and a yaw rudder angle obtained when the necessary rudder angle is applied to the rudder angle of the undecided rudder are obtained, and the necessary rudder is determined to be the rudder angle of the undecided rudder. A steering control device comprising: a second steering angle determination unit that determines a steering angle at which a roll steering angle closer to the target fluid force steering angle than a roll steering angle obtained when the angle is applied is obtained.

  Further, according to one aspect of the present invention, in the rudder control device described above, the second rudder angle determination unit sets the rudder angle of one rudder among the undecided rudder to the necessary rudder angle of the one rudder. A value obtained by adding a predetermined value is determined, and a rudder angle of another rudder among the undecided rudder is determined by subtracting the predetermined value from the necessary rudder angle of the other rudder. To do.

  Further, according to one aspect of the present invention, in the rudder control device described above, the second rudder angle determination unit may obtain a roll rudder angle obtained when the necessary rudder angle is applied to the undetermined rudder, and the target flow. The predetermined value indicating a difference between the steering angle and the power steering angle is calculated.

  Further, according to one aspect of the present invention, in the above-described rudder control device, the second rudder angle determination unit adds the predetermined value to the required rudder angle of one rudder of the undecided rudder. When the steering angle is out of the steerable range, the rudder angle of the one rudder is determined as the limit value of the steerable range, and the rudder angle of the other rudder among the undecided rudder is changed to the other rudder The required steering angle is determined to be a value obtained by subtracting the difference between the required steering angle of one of the undetermined rudders and the limit value of the steerable range.

  One embodiment of the present invention is an underwater vehicle including the rudder control device described above and the four rudders.

  One aspect of the present invention includes two rudders that are in a vertical plane of the hull and are rotatable about a first axis that is inclined at 45 degrees with respect to a horizontal plane of the hull, and the first rudder that is in the vertical plane of the hull. A rudder control method for controlling a rudder angle of the rudder of an underwater vehicle including a total of four rudders, two rudders capable of rotating around a second axis perpendicular to one axis, the pitch An input step for receiving an input of a target fluid force steering angle that is a target value of a steering angle, a yaw steering angle, and a roll steering angle, and each steering angle of the rudder necessary to obtain the target fluid power steering angle A required rudder angle identifying step for identifying a rudder angle, and one rudder that is out of the steerable range when at least one of the four rudder is out of the steerable range Is determined to be the limit value of the steerable range, and the same axis as the one rudder A rudder angle is determined by a first rudder angle determining step for determining a rudder angle of another rudder that can rotate about the required rudder angle or a limit value of the steerable range, and the first rudder angle determining step. The pitch rudder angle and yaw rudder angle obtained when the required rudder angle is applied to the rudder angle of the undecided rudder, and the necessary rudder angle other than the rudder rudder are obtained. A second rudder angle determining step for determining a rudder angle at which a roll rudder angle closer to the target fluid force rudder angle than a roll rudder angle obtained when the required rudder angle is applied to the rudder angle of the determined rudder; This is a rudder control method.

  According to the rudder control device, the underwater vehicle, and the rudder control method described above, even if there is a rudder that is out of the steerable range among the four rudder constituting the X-type rear rudder, the target flow can be further increased. A fluid steering angle close to the steering angle can be obtained.

It is a figure which shows the outline | summary of the underwater vehicle which concerns on 1st Embodiment. It is a figure which shows the structure of the X-type rear rudder which concerns on 1st Embodiment. It is a figure which shows the function structure of the underwater vehicle which concerns on 1st Embodiment. It is a 1st figure explaining the function of the required steering angle specific | specification part which concerns on 1st Embodiment. It is a 2nd figure explaining the function of the required steering angle specific | specification part which concerns on 1st Embodiment. It is a figure which shows the processing flow of the rudder control apparatus which concerns on 1st Embodiment. It is a 1st figure which shows the processing flow of the reallocation calculating part which concerns on 1st Embodiment. It is a 2nd figure which shows the processing flow of the reallocation calculating part which concerns on 1st Embodiment. It is a 3rd figure which shows the processing flow of the reallocation calculating part which concerns on 1st Embodiment. It is a 4th figure which shows the processing flow of the reallocation calculating part which concerns on 1st Embodiment. It is a figure explaining the effect of the rudder control device concerning a 1st embodiment.

<First Embodiment>
Hereinafter, the rudder control apparatus according to the first embodiment will be described in detail with reference to FIGS.

FIG. 1 is a diagram showing an outline of an underwater vehicle according to the first embodiment.
As shown in FIG. 1, the underwater vehicle 1 according to the first embodiment includes a hull 10 and an X-type rear rudder 11 provided on the rear side in the traveling direction of the hull 10.
The underwater vehicle 1 can change the course of the hull 10 by appropriately changing the rudder angle of the X-type rear rudder 11.

FIG. 2 is a diagram illustrating a structure of an X-type rear rudder according to the first embodiment.
FIG. 2 schematically shows the structures of the hull 10 and the X-type rear rudder 11 when the underwater vehicle 1 is viewed from the rear side in the traveling direction. In FIG. 2, a horizontal plane and a vertical plane along the traveling direction of the underwater vehicle 1 are shown as a hull horizontal plane H and a hull vertical plane V.
As shown in FIG. 2, the X-type rear rudder 11 is provided with two rudders that are rotatable around a first axis O <b> 1 that is in a vertical plane of the hull orthogonal to the traveling direction and that is inclined at 45 degrees with respect to the horizontal plane H of the hull. 111, 114. The X-type rear rudder 11 has two rudders 112 and 113 that are rotatable around a second axis O2 that is in the vertical plane of the hull and orthogonal to the first axis O1. As described above, the X-type rear rudder 11 has a total of four rudders 111 and 112 extending from the center side of the hull 10 to the outside in the upper left, lower left, upper right, and lower right when the underwater vehicle 1 is viewed backward. , 113, 114.
As shown in FIG. 1, when a right-handed coordinate system with the hull center as the origin is considered, the attachment position x coordinates of the rudders 111, 112, 113, 114 are assumed to be equal. Further, it is assumed that the attachment position y coordinate of the rudder 111 and 112 and the attachment position y coordinate of the rudder 113 and 114 are equal. In addition, it is assumed that the attachment position z coordinates of the rudders 111 and 113 and the attachment position z coordinates of the rudders 112 and 114 are equal. Further, the fluid characteristics of the rudder 111, 112, 113, 114 are assumed to be equal.

In FIG. 2, the rudder angles of the rudder 111, 112, 113, 114 are indicated by rudder angles f1, f2, f3, f4. The rudder angles f1 and f4 are numerical values representing the degree of driving of each rudder 111 and 114 in the counterclockwise direction as a positive value and the degree of driving in the clockwise direction as a negative value when viewed from the rudder 111 side. is there. The rudder angles f2 and f3 represent, as viewed from the rudder 112, the degree of driving of each rudder 112 and 113 in the clockwise direction as a positive value, and the degree of driving in the counterclockwise direction as a negative value. It is a numerical value.
Further, although details will be described later, each of the rudder 111, 112, 113, 114 has a steerable range in advance (limit values of the steering angles f1, f2, f3, f4 (upper limit value and lower limit value)) due to mechanical restrictions or the like. The steering angles f1, f2, f3, and f4 can only take values from the upper limit value lim, which is the steerable range, to the lower limit value -lim (lim> 0), respectively.

  In addition, in the following description, the words indicating up, down, left, right, clockwise, and counterclockwise are directions or rotational directions when the underwater vehicle 1 is viewed backward as shown in FIG. 2 unless otherwise specified. Means.

As will be described later, when the underwater vehicle 1 according to the present embodiment determines the rudder angles of the rudders 111 to 114 of the X-type rear rudder 11, the flow force applied to the steering for the conventional cross-shaped rear rudder. A target fluid force steering angle that is a target value of the steering angle (pitch steering angle e, yaw steering angle r, and roll steering angle d) is calculated.
Here, the pitch rudder angle e is a numerical value representing the degree of turning of the underwater vehicle 1 in the vertical direction along the hull vertical plane V. In FIG. 2, the pitch rudder angle e represents a degree of turning in which the traveling direction of the underwater vehicle 1 moves upward, and a negative value indicates a degree of turning in which the traveling direction of the underwater vehicle 1 moves downward. Represented by the value of.
The yaw rudder angle r is a numerical value representing the degree of turning of the underwater vehicle 1 in the left-right direction along the hull horizontal plane H. In FIG. 2, the yaw rudder angle r represents the degree of turning in which the traveling direction of the underwater vehicle 1 moves to the right side as a positive value, and the degree of turning in which the traveling direction of the underwater vehicle 1 moves to the left is negative. Expressed by value.
Further, the roll rudder angle d is a numerical value representing the degree of rotation of the underwater vehicle 1 around the traveling direction axis. In FIG. 2, the roll rudder angle d represents the degree of clockwise rotation of the underwater vehicle 1 as a positive value, and represents the degree of counterclockwise rotation of the underwater vehicle 1 as a negative value. .
The pitch rudder angle e and the yaw rudder angle r are used to direct the traveling direction of the underwater vehicle 1 to a target direction (any direction, up, down, left, and right). In order to keep the inclination of the vehicle horizontal, it is adjusted by the steering of the operator or automatic control.

The fluid rudder angle (pitch rudder angle e, yaw rudder angle r, and roll rudder angle d) is achieved by the combined moment of each rudder 111-114. That is, the progress of the underwater vehicle 1 is determined by the combination of the rudder angles f1 to f4 of the rudder 111 to 114 corresponding to the hydrodynamic rudder angles (e, r, d).
For example, consider a case where the steering angles f1 to f4 of the rudders 111 to 114 are in the state shown in FIG. 2 (f1 = δ> 0, f2 = δ> 0, f3 = δ> 0, f4 = δ> 0). In this case, the rudder 111 and the rudder 114 both generate a lower left moment, and the rudder 112 and the rudder 113 both generate a left upper moment. Further, as described above, since the absolute value of the attachment position y coordinate of the rudder 111, 112, 113, 114 and the flow force characteristic of each rudder are equal and the rudder angles f1-f4 are equal, the rudder 111-114 is generated. Moments are equal. Therefore, a leftward force is applied to the stern side of the hull 10 by these combined moments. As a result, since the stern side of the hull 10 moves to the left, the underwater vehicle 1 turns to the right (pitch rudder angle e = 0, yaw rudder angle r> 0, roll rudder angle d = 0).
When the mechanism as described above is generalized, the steering angles f1 to f4 of the rudders 111 to 114 in the X-type rear rudder 11 are based on the correspondence relationship such as the equation (1), and the pitch rudder angle e, yaw rudder angle r, and It is converted into each of the roll steering angles d.

  When a target fluid steering angle (a target pitch steering angle et, a target yaw steering angle rt, and a target roll steering angle dt, which will be described later) is given as a target fluid steering angle, A method of calculating the steering angles f1 to f4 (necessary steering angles fn1 to fn4 described later) required for each of 111 to 114 will be described later.

FIG. 3 is a diagram illustrating a functional configuration of the underwater vehicle according to the first embodiment.
As shown in FIG. 3, the hull 10 includes a steering reception unit 12, a rudder drive unit 13, and a rudder control device 2.
The steering reception unit 12 is a steering device that receives an input of a target direction, a target pitch angle, and a target roll angle for steering or automatic control by a driver. The steering reception unit 12 includes a target fluid force steering angle calculation unit 120 that calculates a target fluid steering angle (target pitch steering angle et, target yaw steering angle rt, and target roll steering angle dt) according to the received steering. I have. The target hydrodynamic steering angle calculation unit 120 immediately calculates a target hydrodynamic steering angle that achieves the traveling direction and posture specified by the steering or automatic control target azimuth, target pitch angle, and target roll angle. And output to the rudder control device 2.
The rudder drive unit 13 includes a drive mechanism such as a motor, and the rudder angles f1 to f4 of the rudder 111 to 114 according to control signals (determined rudder angles ff1, ff2, ff3, and ff4 described later) received from the rudder control device 2. Adjust.

  The rudder control device 2 according to the present embodiment includes each of the target fluid power steering angles (pitch steering angle e, yaw steering angle r, and roll steering angle d) received from the steering receiving unit 12 (target fluid steering angle calculation unit 120). Optimal steering angles f1 to f4 (determined steering angles ff1 to ff4) are calculated based on the target pitch steering angle et, target yaw steering angle rt, and target roll steering angle dt). Hereinafter, the functional configuration of the rudder control device 2 will be described in detail.

As shown in FIG. 2, the rudder control device 2 includes an input unit 20, a necessary rudder angle specifying unit 21, and a redistribution calculation unit 22.
The input unit 20 receives an input of a target fluid force steering angle (a target pitch steering angle et, a target yaw steering angle rt, and a target roll steering angle dt) from the steering reception unit 12.
The necessary rudder angle identifying unit 21 identifies the necessary rudder angles fn1, fn2, fn3, and fn4, which are the respective rudder angles of the rudder 111 to 114 necessary for obtaining the target flow force rudder angle.
The redistribution calculation unit 22 determines the actual steering angle (e, r, d) that is obtained when at least one of the necessary steering angles fn1, fn2, fn3, fn4 is outside the steerable range. In order to bring the force steering angle (et, rt, dt) as close as possible, a process of redistributing the steering angles f1 to f4 so as to be an optimum steering angle within the steerable range is performed. The redistribution calculation unit 22 includes a first rudder angle determination unit 221 and a second rudder angle determination unit 222, and the final determined rudder angles ff1 to ff4 with respect to the rudder angles f1 to f4 by the respective functions. Is determined.

FIG. 4 is a first diagram illustrating the function of the necessary steering angle specifying unit according to the first embodiment.
FIG. 5 is a second diagram illustrating the function of the necessary steering angle specifying unit according to the first embodiment.
Next, the function of the required steering angle specifying unit 21 will be described in detail with reference to FIGS. 4 and 5.

The necessary rudder angle identifying unit 21 identifies the necessary rudder angles fn1 to fn4 of the rudder 111 to 114 according to the target pitch rudder angle et, the target yaw rudder angle rt, and the target roll rudder angle dt input through the input unit 20. .
Specifically, the necessary rudder angle specifying unit 21 performs the calculation of Expression (2) for the target pitch rudder angle et, the target yaw rudder angle rt, and the target roll rudder angle dt.

  Here, the equation (2) indicates that the target pitch rudder angle et, the target yaw rudder angle rt, the target roll rudder angle dt, and the necessary rudder angles fn1 to fn4 of the rudders 111 to 114 have the relationship of the equation (1). It is prescribed to satisfy. That is, the target pitch rudder angle et, the target yaw rudder angle rt, and the target roll rudder angle dt are achieved when the rudder angles f1 to f4 of the rudders 111 to 114 become the required rudder angles fn1 to fn4.

  According to equation (2), the relationship between the target fluid steering angle (target pitch steering angle et, target yaw steering angle rt and target roll steering angle dt) and the required steering angles fn1, fn2, fn3, fn4 is shown in FIG. The correspondence is as shown in (a). According to such a correspondence relationship, for example, as shown in FIG. 5B, the target pitch rudder angle et = 20 °, the target yaw rudder angle rt = 20 °, and the target roll rudder angle dt as the target fluid force rudder angle. = 5 ° is input, the required steering angle fn1 to fn4 are specified as fn1 = 35 °, fn2 = 5 °, fn3 = −5 °, and fn4 = 45 ° by the calculation of the required steering angle specifying unit 21. The

However, as described above, the rudder angles f1 to f4 of the rudders 111 to 114 are driven only from the upper limit value lim that is a preliminarily steerable range to the lower limit value −lim (lim> 0). Here, for example, a case is considered in which the limit values (upper limit value, lower limit value) of the steerable range are defined in advance as the upper limit value lim = 30 ° and the lower limit value −lim = −30 °.
In this case, among the necessary steering angles fn1 to fn4 corresponding to the target fluid power steering angle (et = 20 °, rt = 20 °, dt = 5 °), the required steering angles fn1 (= 35 °) and fn4 (= 45 °). ) Is out of the steerable range (see FIG. 5B). On the other hand, among the necessary steering angles fn1 to fn4, the necessary steering angles fn2 (= 5 °) and fn3 (= −5 °) are within the steerable range.
Here, suppose that the steering angles f1 and f4 corresponding to the necessary steering angles fn1 and fn4 exceeding the upper limit value lim (= 30 °) are determined as the upper limit value lim, and the required steering is within the steerable range. It is assumed that the steering angles f2 and f3 corresponding to the angles fn2 and fn3 are processed as the necessary steering angles fn2 and fn3. According to such processing, as shown in FIG. 5C, the final determined rudder angles ff1 to ff4 corresponding to the rudders 111 to 114 are ff1 = 30 °, ff2 = 5 °, ff3 = −5. °, ff4 = 30 °. As a result of applying the determined rudder angles ff1 to ff4 to the rudder angles f1 to f4 of the rudders 111 to 114, the actually obtained fluid rudder angle is based on the formula (1), and the pitch rudder angle e = 15. °, yaw steering angle r = 15 °, and roll steering angle d = 2.5 °.
Then, any of the actually obtained fluid power steering angles (pitch steering angle e, yaw steering angle r, and roll steering angle d) is the target fluid power steering angle (target pitch steering angle et, target yaw steering angle rt, and target steering angle rt). It deviates from each of the roll rudder angles dt).

  Therefore, in the rudder control device 2 according to the present embodiment, the fluid steering angle (e, r, d) actually obtained by the redistribution calculation unit 22 described above is the target fluid steering angle (et, rt, dt). The steering angle f1 to f4 is redistributed within each steerable range so as to be as close as possible.

FIG. 6 is a diagram illustrating a processing flow of the rudder control device according to the first embodiment.
Next, the processing flow of the entire rudder control device 2 will be described in order with reference to FIG.

First, the input unit 20 of the rudder control device 2 obtains the target fluid rudder angle (target pitch rudder angle et, target yaw rudder angle rt and target roll rudder angle dt) from the target fluid rudder angle calculating unit 120 (FIG. 3). Input (step S01).
Next, the required rudder angle specifying unit 21 of the rudder control device 2 specifies the required rudder angles fn1 to fn4 of the rudder 111 to 114 based on the calculation of the equation (2) (step S02) (FIG. 5). (Refer to (a) and (b)).
Next, the redistribution calculation unit 22 of the rudder control device 2 performs a predetermined redistribution calculation for the necessary rudder angles fn1 to fn4 obtained in step S02, and calculates final determined rudder angles ff1 to ff4 ( Step S03). Details of the process of step S03 by the redistribution calculation unit 22 will be described later.
Further, the redistribution calculation unit 22 outputs the calculated determined rudder angles ff1 to ff4 toward the rudder driving unit 13 (FIG. 3) (step S04). Thereby, the rudder angles f1 to f4 of the rudders 111 to 114 become optimum rudder angles (determined rudder angles ff1 to ff4) according to the target fluid force rudder angle.

7 to 10 are first to fourth diagrams showing a processing flow of the redistribution calculation unit according to the first embodiment.
Next, the processing flow of the redistribution calculation unit 22 executed in step S03 (FIG. 6) will be described in detail.

First, the first rudder angle determination unit 221 of the redistribution calculation unit 22 substitutes the necessary rudder angles fn1 to fn4 identified in step S02 (FIG. 6) for each of the determined rudder angles ff1 to ff4 (step S11). .
Next, the first rudder angle determination unit 221 refers to the determined rudder angles ff1 and ff4 corresponding to each of the rudder 111 and the rudder 114 that are rotatable about the same axis O1, and determines the determined rudder angles ff1 and ff4. It is determined whether or not at least one is out of the steerable range (ff1, ff4 <-lim, or ff1, ff4> lim) (step S12).

When one of the determined rudder angles ff1 and ff4 is outside the steerable range (step S12: YES), the first rudder angle determining unit 221 is out of the steerable range among the determined rudder angles ff1 and ff4. For one (or both), the upper limit value lim or the lower limit value -lim is determined. Further, the first rudder angle determining unit 221 determines the other of the determined rudder angles ff1 and ff4 within the steerable range by adopting the necessary rudder angles fn1 and fn4 that are initially set in step S11. (Step S13).
For example, when the determined rudder angle ff1 = 35 ° and ff4 = −5 ° in step S11, the determined rudder angle ff1 = lim = 30 ° and ff4 = −5 ° are determined in step S13. For example, when the determined rudder angle ff1 = 35 ° and ff4 = −45 ° in step S11, the determined rudder angle ff1 = lim = 30 ° and ff4 = −lim = −30 ° are determined in step S13.

After step S13, the first rudder angle determination unit 221 is an undecided rudder at this time (the rudder other than the rudder whose rudder angle has been determined in step S13), and the rudder that can rotate about the same axis O2. It is determined whether or not the determined rudder angles ff2 and ff3 corresponding to each of 112 and 113 are within the steerable range (step S14).
When the determined rudder angles ff2 and ff3 are both within the steerable range (step S14: YES), the second rudder angle determining unit 222 sets the determined rudder angles ff2 and ff3 corresponding to the undecided rudder (the rudder 112 and 113). Processing to determine is performed (step S15). The process flow of the second steering angle determination unit 222 executed in step S15 will be described later.

  Further, when one of the determined rudder angles ff2 and ff3 is outside the steerable range (step S14: NO), the first rudder angle determining unit 221 determines that the determined rudder angles ff2 and ff3 are out of the steerable range. For one (or both), the upper limit value lim or the lower limit value -lim is determined. Further, the first rudder angle determining unit 221 determines the other of the determined rudder angles ff2 and ff3 that are within the steerable range by adopting the necessary rudder angles fn2 and fn3 that are initially set in step S11. (Step S16).

  On the other hand, when the determined rudder angles ff1 and ff4 are both within the steerable range in step S12 (step S12: NO), the first rudder angle determination unit 221 then sets the rudder 112 and the rudder 113 to each. The corresponding determined rudder angles ff2, ff3 are referred to. Then, the first rudder angle determination unit 221 determines whether or not at least one of the determined rudder angles ff2 and ff3 is outside the steerable range (step S17).

  When one of the determined rudder angles ff2 and ff3 is outside the steerable range (step S17: YES), the first rudder angle determining unit 221 is out of the steerable range among the determined rudder angles ff2 and ff3. For one (or both), the upper limit value lim or the lower limit value -lim is determined. Further, the first rudder angle determining unit 221 determines the other of the determined rudder angles ff2 and ff3 that are within the steerable range by adopting the necessary rudder angles fn2 and fn3 that are initially set in step S11. (Step S18).

  The determined rudder angles ff1 and ff4 corresponding to each of the rudders 111 and 114 that are undecided rudder at this time (the rudder other than the rudder whose rudder angle has been determined in step S17) are both within the steerable range in step S12. It turns out that there is. Therefore, in this case, the second rudder angle determination unit 222 immediately performs a process of determining the determined rudder angles ff1 and ff4 corresponding to the undecided rudder (the rudders 111 and 114) (step S19).

  When the determined rudder angles ff2 and ff3 are both within the steerable range in step S17 (step S17: NO), the determined rudder angles ff1 to ff4 are both within the steerable range. Then, since each rudder 111 to 114 can be steered to the necessary rudder angles fn1 to fn4 at which the target fluid force rudder angle is achieved, the first rudder angle determination unit 221 determines the determined rudder angle initially set in step S11. ff1 to ff4 are employed as they are, and the processing is terminated.

  Next, a processing flow of the second steering angle determination unit 222 executed in step S15 and step S19 (FIG. 7) will be described with reference to FIGS. 8 to 10 exemplify the processing flow executed in step S15, the processing flow executed in step S19 is also the same as that shown in FIGS.

  First, the second rudder angle determination unit 222 of the redistribution calculation unit 22 performs a calculation shown in Expression (3) using a predetermined value (calculated value a) (step S31).

Here, the determined rudder angles ff1 and ff4 determined by the first rudder angle determining unit 221 (step S13 (FIG. 7)) are determined to be within the steerable range. Then, since at least one of the determined rudder angles ff1 and ff4 is less than the necessary rudder angles fn1 and fn4, the roll rudder angle d actually obtained when the determined rudder angles ff1 and ff4 are employed as they are. Is less than the target roll rudder angle dt (see the relational expression for the roll rudder angle d in equation (1)).
As the calculated value a, the determined rudder angles ff1 and ff4 determined so as to be within the steerable range are applied to the rudder angles f1 and f4 of the rudder 111 and 114, and the undecided rudder (the rudder 112 and 113). The difference between the roll steering angle d obtained when the required steering angles fn1 and fn2 are applied as they are to the steering angles f2 and f3 and the target roll steering angle dt that was originally targeted is shown.

  The second rudder angle determination unit 222 uses the determined rudder angle ff2 of one rudder (the rudder 112) of the undecided rudder (the rudder 112, 113) as shown in the equation (3). A value obtained by adding a half value (a / 2) of the operation value a to fn2 is determined. Further, the second rudder angle determination unit 222 sets the determined rudder angle ff3 of the other rudder (rudder 113) of the undecided rudder (rudder 112, 113) to a predetermined value a from the necessary rudder angle fn3 of the rudder 113. A value obtained by subtracting the half value (a / 2) is determined.

The determined rudder angles ff1 and ff4 stored in the steerable range in step S13 (FIG. 7) and the newly determined rudder angles ff2 and ff3 determined in step S31 are related to the roll rudder angle d (formulas) When the steering angles f1 to f4 in (1) are respectively substituted, the actually obtained roll steering angle d coincides with the target roll steering angle dt.
Similarly, the determined rudder angles ff1 and ff4 within the steerable range in step S13 (FIG. 7) and the determined rudder angles ff2 and ff3 determined in step S31 are the pitch rudder angle e and yaw rudder angle. If the values are substituted for the steering angles f1 to f4 in the relational expression (formula (1)) for r, the calculated value a is canceled in any case. That is, by applying the determined rudder angles ff2 and ff3 determined in step S31 to the rudder angles f2 and f3 of the undecided rudder (the rudder 112 and 113), the original necessity for the rudder angles f2 and f3 is applied. The same pitch steering angle e and yaw steering angle r as the pitch steering angle e and yaw steering angle r obtained when the steering angles fn2 and fn3 are applied can be obtained.

  As described above, the second rudder angle determination unit 222 determines the roll rudder angle d and the target roll rudder angle dt obtained when the necessary rudder angles fn2 and fn3 are applied to the undecided rudder (the rudder 112 and 113). By calculating the calculation value a indicating the difference between the roll steering angle d, the roll steering angle d actually obtained can be matched with the target roll steering angle dt.

  In step S19 (FIG. 7), the processing corresponding to step S31 can be executed by performing the calculation shown in equation (4) using the calculated value a.

Next, the second rudder angle determination unit 222 checks whether each of the determined rudder angles ff2 and ff3 determined in step S31 is outside the steerable range.
Specifically, first, the second rudder angle determination unit 222 performs initialization by substituting “zero” into predetermined calculation values b2 and b3 (step S32).

Next, the second steering angle determination unit 222 determines whether or not the determined steering angle ff2 determined in step S31 is outside the steerable range (step S33).
When the determined rudder angle ff2 determined in step S31 is outside the steerable range (step S33: YES), the second rudder angle determining unit 222 uses a predetermined function F to limit the limit value (upper limit lim or The difference from the lower limit value -lim) to the required steering angle fn2 is obtained, and this is set as the calculated value b2 (step S34).

Here, the predetermined function F will be described with reference to the flowchart shown in FIG.
The function F first determines whether or not the variable x (the required steering angle fn2 in step S34) is greater than or equal to zero (x ≧ 0) (step S50).
When the variable x (required steering angle fn2) is equal to or greater than zero (step S50: YES), the function F calculates the difference y (y = lim−x> 0) between the upper limit value lim and the variable x (required steering angle fn2). Output (step S51).
On the other hand, when the variable x (required steering angle fn2) is less than zero (step S50: NO), the function F is the difference y (y = −lim−x) between the lower limit value −lim and the variable x (required steering angle fn2). <0) is output (step S52).
In this way, the function F takes into account the sign of the input variable x (required steering angle fn2), the variable x, and the limit values closer to the variable x (upper limit lim, lower limit -lim) and The difference between and is output.

  On the other hand, in step S33 of FIG. 8, when the determined rudder angle ff2 determined in step S31 is within the steerable range (step S33: NO), the second rudder angle determining unit 222 executes step S34 described above. do not do. That is, the second rudder angle determination unit 222 keeps the calculated value b2 as zero.

Next, the second steering angle determination unit 222 determines whether or not the determined steering angle ff3 determined in step S31 is outside the steerable range (step S35).
When the determined rudder angle ff3 determined in step S31 is outside the steerable range (step S35: YES), the second rudder angle determining unit 222 uses the function F (FIG. 10) to set a limit value (upper limit value). lim or lower limit value−lim) to the required steering angle fn3 is obtained and set as a calculated value b3 (step S36).

  In FIG. 9, the second steering angle determination unit 222 further determines whether or not both the calculated value b2 and the calculated value b3 that have passed through Steps S31 to S36 are not zero (b2 ≠ 0 and b3 ≠ 0) ( Step S37).

When both the calculated value b2 and the calculated value b3 are not zero (step S37: YES), this means that both the determined rudder angles ff2 and ff3 determined in step S31 are outside the steerable range. doing.
In this case, the second rudder angle determination unit 222 substitutes the smaller one of the calculated values b2 and b3 for the predetermined calculated value m. Then, the second rudder angle determination unit 222 determines the determined rudder angle ff2 of the rudder 112 to a value obtained by adding the calculated value m to the required rudder angle fn2 of the rudder 112, and sets the determined rudder angle ff3 of the rudder 113. Then, a value obtained by subtracting the predetermined value m from the required steering angle fn3 of the rudder 113 is determined (step S38).

  Then, the determined rudder angles ff2 and ff3 are added (or subtracted) to the necessary rudder angles fn2 and fn3, respectively, with the calculated value m corresponding to the difference from either one of the necessary rudder angles fn2 and fn3 to the limit value. Obtained. Therefore, one of the determined rudder angles ff2 and ff3 coincides with a limit value (upper limit lim or lower limit -lim). Further, since the calculated value m is the smaller of the calculated values b2 and b3, the other of the determined rudder angles ff2 and ff3 is always within the steerable range.

  On the other hand, when one of the calculated value b2 and the calculated value b3 is zero (step S37: NO), the second steering angle determination unit 222 continues with only the calculated value b3 being zero (b2 ≠ 0 and b3). = 0) or not (step S39).

When only the calculated value b3 is zero (step S39: YES), this means that only the determined rudder angle ff2 is out of the steerable range among the determined rudder angles ff2 and ff3 determined in step S31. doing.
In this case, the second rudder angle determination unit 222 determines the determined rudder angle ff2 of the rudder 112 to a value obtained by adding the calculated value b2 to the necessary rudder angle fn2 of the rudder 112, and the determined rudder angle ff3 of the rudder 113 Is determined by subtracting the predetermined value b2 from the required steering angle fn3 of the rudder 113 (step S40).

  Then, the determined steering angle ff2 is obtained by adding the calculated value b2 corresponding to the difference from the required steering angle fn2 to the limit value to the required steering angle fn2. Accordingly, the determined rudder angle ff2 matches the limit value (upper limit lim or lower limit -lim).

  When only the calculated value b3 is not zero (step S39: NO), the second steering angle determining unit 222 subsequently determines whether only the calculated value b2 is zero (b2 = 0 and b3 ≠ 0). Is determined (step S41).

When only the calculated value b2 is zero (step S41: YES), this means that only the determined rudder angle ff3 is out of the steerable range among the determined rudder angles ff2 and ff3 determined in step S31. doing.
In this case, the second rudder angle determination unit 222 determines the determined rudder angle ff3 of the rudder 113 to a value obtained by subtracting the calculated value b3 from the required rudder angle fn3 of the rudder 113, and the determined rudder angle ff2 of the rudder 112 Is determined to be a value obtained by adding the predetermined value b3 to the required steering angle fn2 of the rudder 112 (step S42).

  Then, the determined steering angle ff3 is obtained by adding the calculated value b3 corresponding to the difference from the required steering angle fn3 to the limit value to the required steering angle fn3. Therefore, the determined rudder angle ff3 matches the limit value (upper limit lim or lower limit -lim).

  If both the calculated values b2 and b3 are zero (step S41: NO), this means that both the determined rudder angles ff2 and ff3 determined in step S31 are within the steerable range. doing. Therefore, in this case, the determined rudder angles ff2 and ff3 determined in step S31 are employed as they are.

According to the process of step S32 to step S42 described above, the second rudder angle determination unit 222 has not yet been determined when one of the determined rudder angles ff2 and ff3 determined in step S31 is outside the steerable range. The rudder angles f2, f3 of the rudder (the rudder 112, 113) are determined as limit values (upper limit lim, lower limit-lim) of the steerable range. By doing so, it is possible to control the roll rudder angle d as close as possible to the target roll rudder angle dt within the steerable range.
Further, the second rudder angle determination unit 222 sets the determined rudder angles ff2 and ff3 within the steerable range, and further adds a value (m, b2 or b3) to the necessary rudder angle fn2 and the necessary rudder angle fn3. Control so that the value to be subtracted is equal. By doing in this way, the pitch rudder angle e and yaw rudder angle r obtained when the original necessary rudder angles fn2 and fn3 are applied to the rudder angles f2 and f3 of the undetermined rudder (the rudder 112 and 113). The same pitch rudder angle e and yaw rudder angle r can be obtained.

FIG. 11 is a diagram for explaining the effect of the rudder control device according to the first embodiment.
Here, in the case illustrated in FIG. 5B, a case is considered in which the processes of the first steering angle determination unit 221 and the second steering angle determination unit 222 described above are performed.
In this case, the determined rudder angles ff1 and ff4 are both outside the steerable range (ff1 = 35 °> 30 °, ff4 = 45 °> 30 °). Accordingly, the first rudder angle determination unit 221 determines that the determined rudder angle ff1 = 30 ° and the determined rudder angle ff4 = 30 ° in step S13 (FIG. 7). At this time, the determined rudder angles ff2, ff3 (initial setting values fn2, fn3) of the undecided rudder (the rudder 112, 113) are both within the steerable range (step S14: YES). The second steering angle determination unit 222 executes the steering angle determination process (step S15).

  In step S31 (FIG. 8), the second rudder angle determination unit 222 calculates the calculated value a (a = 10 °), and further determines that the rudder angle ff2 = 10 ° and the rudder angle ff3 = −10 °. To do. In this case, since the determined rudder angles ff2 and ff3 are both within the steerable range, the determined rudder angle ff2 = 10 ° and the determined rudder angle ff3 = −10 ° determined in step S31 are employed as they are (step S32). -Step S42).

  As a result, as shown in FIG. 11, the actually obtained fluid power steering angle is pitch steering angle e = 15 °, yaw steering angle r = 15 °, and roll steering angle d = 5 °. Therefore, by the control of the rudder control device 2, the same pitch rudder angle e and yaw rudder angle r as the pitch rudder angle e and yaw rudder angle r obtained in the case shown in FIG. The same roll steering angle d (= 5 °) as the angle dt can be obtained.

As described above, according to the second rudder angle determining unit 222 according to the first embodiment, the rudder angles f2 and f3 of the undecided rudder (the rudder 112 and 113) are required to be the rudder angles f2 and f3. Than the roll steering angle d obtained when the required steering angles fn2 and fn3 are applied to the steering angles f2 and f3. The rudder angle d that is close to the target roll rudder angle dt is determined to be a rudder angle.
Therefore, according to the rudder control device 2 according to the first embodiment, even if there is a rudder that is out of the steerable range among the four rudders 111 to 114 constituting the X-type rear rudder 11, A fluid steering angle closer to the target fluid steering angle can be obtained.

As mentioned above, although the rudder control apparatus 2 which concerns on 1st Embodiment was demonstrated in detail, the specific aspect of the rudder control apparatus 2 is not limited to the above-mentioned thing, In the range which does not deviate from a summary, it is various. It is possible to add design changes.
For example, in the first embodiment, the rudder control device 2 preferentially approaches the target flow force rudder angle with respect to the roll rudder angle d among the pitch rudder angle e, yaw rudder angle r, and roll rudder angle d. It was described as performing control. However, in other embodiments, the present invention is not limited to this aspect, and control may be performed so that the pitch steering angle e or the yaw steering angle r is preferentially brought close to the target fluid steering angle.

In the above-described embodiment, a program for realizing the function of the rudder control device 2 is recorded on a computer-readable recording medium, and the program recorded on the recording medium is read by the computer system and executed. Each procedure is to be performed. Here, each process of the rudder control device 2 described above is stored in a computer-readable recording medium in the form of a program, and the above-described various processes are performed by the computer reading and executing the program. Here, the computer-readable recording medium refers to a magnetic disk, a magneto-optical disk, a CD-ROM, a DVD-ROM, a semiconductor memory, and the like. Alternatively, the computer program may be distributed to the computer via a communication line, and the computer that has received the distribution may execute the program.
Moreover, the aspect with which each function of the rudder control apparatus 2 is comprised over the some apparatus connected with a network may be sufficient.

  As mentioned above, although some embodiment of this invention was described, these embodiment is shown as an example and is not intending limiting the range of invention. These embodiments can be implemented in various other forms, and various omissions, replacements, and changes can be made without departing from the scope of the invention. These embodiments and modifications thereof are included in the invention described in the claims and equivalents thereof, as long as they are included in the scope and gist of the invention.

DESCRIPTION OF SYMBOLS 1 Underwater vehicle 10 Hull 11 X-type rear rudder 111,112,113,114 Rudder 12 Steering reception part 120 Target flow force rudder angle calculating part 13 Rudder drive part 2 Rudder control apparatus 20 Input part 21 Necessary rudder angle specific part 22 Redistribution calculation unit 221 First steering angle determination unit 222 Second steering angle determination unit

Claims (6)

Two rudders in the hull vertical plane that are rotatable about a first axis inclined at 45 degrees with respect to the horizontal plane of the hull, and a second axis that is in the hull vertical plane and orthogonal to the first axis A rudder control device for controlling a rudder angle of the rudder of an underwater vehicle including a total of four rudders,
An input unit for receiving an input of a target hydrodynamic steering angle that is a target value of a pitch steering angle, a yaw steering angle, and a roll steering angle;
A required rudder angle identifying unit for identifying a necessary rudder angle that is a rudder angle of each of the rudder necessary for obtaining the target fluid power rudder angle;
When at least one of the four required rudder angles is outside the steerable range, the rudder angle of one rudder outside the steerable range is set as the limit value of the steerable range. A first rudder angle determination unit that determines and determines a rudder angle of another rudder that is rotatable about the same axis as the one rudder as the required rudder angle or a limit value of the steerable range;
The pitch rudder angle obtained when the necessary rudder angle is applied to the rudder angle of the undecided rudder which is a rudder other than the rudder whose rudder angle has been determined by the first rudder angle determining unit. And a yaw rudder angle, and a roll rudder angle closer to the target hydrodynamic rudder angle than the roll rudder angle obtained when the required rudder angle is applied to the undetermined rudder angle. A second rudder angle determination unit that determines the angle;
Rudder control device comprising: The second rudder angle determination unit
The rudder angle of one rudder of the undecided rudder is determined to be a value obtained by adding a predetermined value to the required rudder angle of the one rudder, and the rudder angle of another rudder of the undecided rudder The rudder control device according to claim 1, wherein the rudder control device is determined to be a value obtained by subtracting the predetermined value from the necessary rudder angle of the other rudder. The second rudder angle determination unit
The predetermined value indicating a difference between a roll rudder angle obtained when the required rudder angle is applied to the undetermined rudder and the target flow rudder angle is calculated. Rudder control device. The second rudder angle determination unit
When the value obtained by adding the predetermined value to the required rudder angle of one rudder among the undecided rudders is outside the steerable range, the rudder angle of the one rudder is limited to the limit of the steerable range. And determining the rudder angle of the other rudder of the undecided rudder from the necessary rudder angle of the other rudder and the necessary rudder angle of the rudder of the undecided rudder and the steering The rudder control apparatus according to claim 2 or 3, wherein the rudder control apparatus determines a value obtained by subtracting a difference from a limit value of a possible range. The rudder control device according to any one of claims 1 to 4,
An underwater vehicle including the four rudders. Two rudders in the hull vertical plane that are rotatable about a first axis inclined at 45 degrees with respect to the horizontal plane of the hull, and a second axis that is in the hull vertical plane and orthogonal to the first axis A rudder control method for controlling a rudder angle of the rudder of an underwater vehicle including a total of four rudders,
An input step for receiving an input of a target hydrodynamic steering angle which is a target value of a pitch steering angle, a yaw steering angle, and a roll steering angle;
A necessary rudder angle identifying step for identifying a necessary rudder angle that is a rudder angle of each of the rudder necessary to obtain the target flow force rudder angle;
When at least one of the four required rudder angles is outside the steerable range, the rudder angle of one rudder outside the steerable range is set as the limit value of the steerable range. A first rudder angle determining step for determining and determining a rudder angle of another rudder that is rotatable about the same axis as the one rudder as the required rudder angle or a limit value of the steerable range;
The pitch rudder obtained when the necessary rudder angle is applied to the rudder angle of the undecided rudder which is a rudder other than the rudder whose rudder angle has been determined in the first rudder angle determining step. A roll rudder angle closer to the target flow force rudder angle than a roll rudder angle obtained when the required rudder angle is applied to the rudder rudder angle is obtained. A second rudder angle determining step for determining the rudder angle;
Rudder control method comprising:

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