JP2005164868A - Simulation device - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide a simulator control method and a simulation device, wherein excessive revolving motion is not generated and a testee does not feel a sense of incongruity. <P>SOLUTION: The simulation device for reproducing oscillation of a real machine by rotary driving a plurality of shafts consisting of a rotary axis and a plurality of gimbal axes comprises: a means 14 for calculating a motion model of a virtual vehicle based on operation information inputted by a testee pilot 30; a rotation speed calculation means 11 for calculating the rotation speed of the rotary axis based on the motion model; an acceleration/angular velocity calculation means 13 for respectively calculating, from the angle of gimbals, translation acceleration and angular velocity acting on the testee; and an angle calculation means for calculating correction amount of the angle of gimbals according to the deviation of the calculated translation acceleration and angular velocity from the motion model, and the angular velocity of the rotary axis. Based on each of the calculated motion data, a rotary drive mechanism is operated to reproduce the translation acceleration and the rotation angular velocity to act on the testee . <P>COPYRIGHT: (C)2005,JPO&NCIPI

Description

  The present invention relates to a simulation device, and more particularly to a simulation device that simulates the acceleration experienced by a driving operation of a vehicle.

  In a vehicle such as an aircraft or a vehicle, in order to virtually experience the rocking generated by the rider's driving, the vehicle and the surrounding conditions are visually reproduced, and the vehicle accompanying the driving operation of the operator A simulation apparatus is used that allows a subject to experience the exercise in a simulated manner. Such a simulation apparatus is widely used in, for example, a flight simulator for flight training, a driving simulator, or an amusement facility.

Conventionally, simulation of a vehicle in a simulation apparatus is generally performed in such a manner that the magnitude of acceleration, that is, the absolute value of acceleration is regarded as a main sensation factor, and the operator perceives acceleration.
As such a vehicle simulation method, a method of changing the seat angle using gravity is known, and by making the acceleration direction of the simulated virtual vehicle coincide with the vertical direction, The direction of acceleration of the vehicle can be sensed. However, in such a device, the subject always senses a constant gravitational acceleration and cannot feel the situation where the acceleration changes dynamically.

Further, a simulation device is known that uses four to six actuators to move a seat on which a subject is seated. According to such a device, the subject can perceive acceleration greater than gravitational acceleration. This device has a problem that it cannot continuously give a large acceleration to the subject.
Further, Patent Documents 1 and 2 disclose devices that attach a seat to the tip of a turning arm and simulate acceleration by centrifugal force. According to such a device, the subject can continuously feel an acceleration greater than the gravitational acceleration. However, in such a device, when the rotational speed of the arm is rapidly changed in order to change the simulated acceleration, the subject sitting on the seat feels the inertial acceleration other than the centrifugal force and feels uncomfortable. For this reason, such a device cannot simulate rapid changes in acceleration.

JP-A-7-334071 JP-A-7-334072 Japanese Patent Application No. 2003-049205

In the simulation apparatus, in order to make the subject experience the motion of the vehicle, the acceleration acting on the subject is simulated by the centrifugal force due to gravity or rotation so that the subject can feel the motion of the vehicle.
However, even if the acceleration is reproduced only by controlling the gravity and the centrifugal force of the arm, it is difficult to accurately reproduce the actual swing of the vehicle as described above.
In view of this, the present applicant has proposed an acceleration simulation apparatus and an acceleration simulator control apparatus capable of making real acceleration sense in Japanese Patent Application No. 2003-049205 (Patent Document 3).

In such a device, the angular acceleration and angular velocity of the arm rotation axis are adjusted so that the arm tip acceleration matches the size of the translation acceleration vector to be reproduced, and then the gimbal is rotated to determine the direction of the translation acceleration vector of the subject. The gimbal angle is adjusted to match the acceleration vector received by the subject on the vehicle.
In order to match the acceleration acting on the space where the subject is placed to the actual vehicle acceleration, in addition to gravity and centrifugal force, the device further considers tangential acceleration due to rotation, and the three combined accelerations. Is always equal to the combined acceleration of the vehicle, that is, the sum of the acceleration due to gravity and vehicle motion, so that the subject can be given the same acceleration environment as that of a real vehicle.

However, the simulation apparatus has a problem that excessive rotational motion is generated because it tries to faithfully simulate the acceleration in the three translational directions. When excessive movement occurs, even if the translational acceleration can be completely reproduced, the subject feels uncomfortable, and further, the discomfort continues, causing the subject to get sick, and training itself becomes impossible There is a fear.
Therefore, in view of the problems of the prior art, the present invention provides a simulation device that allows the subject to experience almost the same acceleration environment as a real vehicle and does not cause the subject to feel uncomfortable without causing excessive rotational movement. The purpose is to provide.

Therefore, in order to solve such a problem, the present invention provides a means for calculating a motion model of a virtual vehicle based on operation information input by a subject, and a plurality of axes including a turning axis and a plurality of gimbal axes. In the simulation apparatus provided with means for rotationally driving each based on the model,
A turning speed calculating means for calculating a turning speed of the turning axis based on the motion model, an acceleration angular speed calculating means for calculating a translational acceleration and an angular speed acting on the subject from the gimbal angle, and the calculated translational acceleration, respectively. And an angle calculation means for calculating a correction amount of the gimbal angle based on the angular velocity, the deviation of the motion model, and the angular velocity of the pivot axis,
The rotational driving means is driven based on the calculated motion data, and the rotational angular velocity is reproduced together with the translational acceleration acting on the subject.

According to this invention, the translational acceleration acting on the subject can be reproduced with high accuracy, and further, the gimbal shaft is rotated in consideration of the angular velocity, so that the generation of excessive angular velocity can be suppressed, and the sensory accuracy As a result, simulator sickness can be prevented.
It is preferable that the vehicle motion model includes translational accelerations in three axial directions and angular velocities around the three axes calculated based on the operation information of the subject. The motion data includes the turning axis, the translational acceleration and angular velocity of the gimbal axis, the angle of the gimbal axis, etc., and determines the position, posture and swing of the vehicle.

In addition, there is provided means for calculating a virtual vehicle motion model based on operation information input by the subject, and means for rotationally driving a plurality of axes including a turning axis and a plurality of gimbal axes based on the motion model. In the simulation device,
Acceleration angular velocity calculation means for calculating translational acceleration and angular velocity acting on the subject from the gimbal angle, respectively, and calculating the angular velocity of the turning axis from the motion model, and the calculated translational acceleration and angular velocity and the deviation of the motion model And a turning speed / angle calculating means for calculating a correction amount of the gimbal angle based on the angular speed of the turning axis,
The rotational driving means is driven based on the calculated motion data, and the rotational angular velocity is reproduced together with the translational acceleration acting on the subject.
According to this invention, it is possible to improve the sensation accuracy to the subject and prevent simulator sickness, and since the load is evenly distributed between the turning shaft and the gimbal shaft, simulation accuracy due to torque saturation and speed saturation of the rotating shaft can be achieved. Deterioration can be prevented.

Further, the present invention is characterized by further comprising a reproduction accuracy setting unit that sets a weighting factor that places importance on the reproduction accuracy of either the acceleration or the angular velocity obtained by the acceleration angular velocity calculation unit. According to this, it is possible to set whether to place importance on the reproduction of the translational acceleration or the reproduction of the angular velocity according to the purpose of use of the simulation, thereby improving the simulation accuracy.
Furthermore, it is preferable that the reproduction accuracy setting means sequentially changes the weighting factor based on a vehicle motion model, and according to this, the sensitivity of the human body is the lowest depending on driving conditions such as flight conditions. By concentrating the reproduction errors on the motion axis, it is possible to obtain the best experience reproduction accuracy at that moment.

  Furthermore, it is preferable that the reproduction accuracy designation unit includes an interface unit for the subject to input a weighting coefficient, and thereby the simulation accuracy can be adjusted in accordance with the sense of each individual subject. At this time, the subject himself / herself can finely adjust the simulation accuracy. It is preferable that the interface allows a subject, a maintenance worker, or the like to easily input a weighting coefficient as appropriate with a graph or a mathematical expression.

  As described above, according to the present invention, the subject can experience a more realistic acceleration, and in the present invention, the gimbal is rotated considering the angular velocity as well as the translational acceleration. It is possible to prevent the subject from feeling uncomfortable.

Hereinafter, exemplary embodiments of the present invention will be described in detail with reference to the drawings. However, the dimensions, materials, shapes, relative arrangements, and the like of the components described in this embodiment are not intended to limit the scope of the present invention unless otherwise specified, but are merely illustrative examples. Not too much.
The simulation device according to the present embodiment is a device that simulates the swing experienced by the subject who controls the vehicle. In the present embodiment, the swing of the airplane is exemplarily reproduced. The present invention is not limited to this, and can be applied to vehicles that generate rocking, such as automobiles and amusement devices.

1 is a block diagram showing an outline of a simulation apparatus according to an embodiment of the present invention, FIG. 2 is a block diagram showing the configuration of a control mechanism and a drive mechanism of the simulation apparatus according to the first embodiment, and FIGS. It is a figure which shows the simulator mechanism which concerns on this embodiment.
As shown in FIG. 1, the simulation apparatus 100 according to the first embodiment includes a simulator control mechanism 101, a simulator drive mechanism 102, and a simulator mechanism 103 as main components, and is connected so as to be able to transmit information to each other. Is provided.
The simulator control mechanism 101 has a function of calculating a body motion model based on operation information input by the test pilot and calculating various motion data. The simulator drive mechanism 102 is based on the various motion data. The simulator mechanism 103 is various devices configured to reproduce an actual machine.

  Here, a specific embodiment of the simulator mechanism 103 will be described with reference to FIGS. The simulator mechanism 103 includes a turning device 43 and a turning arm 44, and the turning device 43 is formed of a turning bearing and a servo motor (not shown). The swivel bearing is joined to one end of the swivel arm 44 and supports the swivel arm 44 so as to be rotatable about the swivel shaft 46 with respect to the ground 45. The turning shaft 46 is provided in the vertical direction. The servo motor rotates the turning arm 44 around the turning shaft 46 in response to an electric signal output from the simulator control mechanism 101.

Further, the simulator mechanism 103 includes a cockpit 51 and a plurality of frames at the other end opposite to one end joined to the turning device 43 of the turning arm 44. The frame is formed of a yaw frame 52 and a pitch frame 53.
A yaw axis rotation device 54 is provided between the turning arm 44 and the yaw frame 52. The yaw shaft rotating device 54 is formed of a bearing and a servo motor (not shown). The bearing supports the yaw frame 52 on the turning arm 44 so that the yaw axis, which is a gimbal axis, can rotate about 55. The yaw axis 55 always passes through point P and is parallel to the pivot axis 46. The servo motor rotates the yaw frame 52 around the yaw axis 55 in response to an electric signal output from the simulator control mechanism 101.

  A pitch axis rotation device 56 is provided between the yaw frame 52 and the pitch frame 53. The pitch shaft rotating device 56 is formed of a bearing and a servo motor (not shown). The bearing supports a pitch frame 53 on a yaw frame 52 so as to be rotatable about a pitch shaft 57 which is a gimbal shaft. The pitch axis 57 always passes through the point P and is perpendicular to the yaw axis 55. The servo motor rotates the pitch frame 53 around the pitch axis 57 in response to an electrical signal output from the simulator control mechanism 101.

  As shown in FIG. 6, a roll shaft rotating device 58 is provided between the pitch frame 53 and the cockpit 51. The roll shaft rotating device 58 is formed of a bearing and a servo motor (not shown). The bearing supports the cockpit 51 on the pitch frame 53 so as to be rotatable about a roll shaft 59 which is a gimbal shaft. The roll axis 59 is always perpendicular to the pitch axis 57 through the point P. The servo motor rotates the cockpit 51 around the roll axis in response to an electrical signal output from the simulator control mechanism 101.

  The cockpit 51 has a test pilot disposed therein. The cockpit 51 includes a display device, a seat, a control panel, and the like not shown. The display device displays an image created by the simulator control mechanism 101. The seat is installed such that the head of the pilot to be seated overlaps the point P. The control panel outputs operation information indicating the operation content operated by the test pilot to the simulator control mechanism 101 as an electric signal.

FIG. 3 is a diagram for explaining the operation of the simulator mechanism 103 according to the embodiment of the present invention.
In the simulator mechanism 103, a seat of a test pilot is disposed at the tip of a swing arm 44 attached to the swing device 43, and the swing arm 44 is swung to generate centrifugal force, and the test pilot is accelerated by several G. It is designed to let you experience it.
What is effective as the operation amount of the simulation mechanism 103 is the attitude angle of the test pilot composed of the displacement angle ψ of the yaw axis, the displacement angle θ of the pitch axis, and the displacement angle φ of the roll axis, the turning arm rotation angular velocity ω _a , Arm rotation angular acceleration. In order to give the subject the same acceleration α as the actual machine to be reproduced, it is necessary to make the magnitude of the acceleration α _b of the actual arm of the acceleration α _b of the arm tip coincide with the magnitude of the acceleration α _b of the arm tip. In addition to this, in this embodiment, since control is performed in consideration of the rotational angular velocity, the translational acceleration ω _{a of} each of the yaw axis, pitch axis, and roll axis and the gimbal axes ω _x , ω _y , ω _z are centered. The controlled angular velocity is also controlled. At this time, the acceleration sensed by the test pilot is expressed by a coordinate system of three vectors X, Y, and Z as shown in FIG. The X-axis direction indicates the turning tangential direction, the Y-axis direction indicates the turning center direction, and the Z-axis direction indicates the vertical direction, which are in a perpendicular relationship with each other.

FIG. 2 shows a simulator control mechanism 101 and a drive mechanism 102 included in the simulation apparatus 100 according to the first embodiment.
The simulator control mechanism 101 includes an arm turning speed calculation unit 11, a gimbal angle calculation unit 12, a simulator acceleration angular velocity calculation unit 13, and a body motion model calculation unit 14. The body motion model calculating means 14 calculates a body motion model composed of the translational accelerations in the X, Y, and Z three-axis directions and the angular velocities around the three axes shown in FIG. The arm turning speed calculating means 11 calculates the turning speed of the turning arm from the airframe motion model and issues a command to the turning drive means 21 described later by an electrical signal. The simulator acceleration angular velocity calculation means 13 calculates translational acceleration and angular velocity acting on the test pilot from the gimbal angle of the gimbal axis, and the gimbal angle calculation means 12 calculates the aircraft motion model and the calculated acceleration. The gimbal angle is calculated based on the deviation from the angular velocity and the angular velocity of the turning shaft, and a command is issued to the gimbal shaft driving means 22 described later by an electrical signal.

The drive mechanism 102 includes a turning drive means 21 for rotating the turning arm and a gimbal shaft driving means 22, and the gimbal shaft driving means 22 rotates the yaw axis rotating device 54. It comprises means 22a, pitch axis driving means 22b for rotating the pitch axis rotating device 56, and roll axis driving means 22c for rotating the roll axis rotating device 58.
The simulator mechanism 103 operates according to the following flow by the simulator control mechanism 101 and the simulator drive mechanism 102.

First, the airframe motion model calculating means 14 theoretically calculates the operation information input by the test pilot 30, that is, the X, Y and Z axis directions of the seat where the test pilot 30 is located from the amount and direction of the driving operation. The aircraft motion model consisting of translational acceleration and angular velocity is calculated.
Then, the turning speed is calculated by the arm turning speed calculation means 11 so that the acceleration at the arm tip having the magnitude of the translation acceleration vector to be reproduced matches, and the turning drive means 21 is rotated by a necessary amount.
On the other hand, the simulator acceleration angular velocity calculation means 13 performs a process of rotationally converting the respective gimbal angles of the yaw axis 55, the pitch axis 57, and the roll axis 59 and the rotation angular velocity vector of the test pilot, and associates each gimbal angular velocity. The calculation processing is performed to set the translation acceleration and the rotational angular velocity to coincide with each other, and the translation acceleration and the angular velocity are calculated.

Here, an example of the calculation in the arm turning speed calculation unit 11 and the calculation in the simulator acceleration angular velocity calculation unit 13 will be described.
First, the calculation in the simulator acceleration angular velocity calculation means 13 is performed. In the calculation, first, the degree of freedom of movement in the simulator mechanism 103 is selected. Since the degree of freedom of motion of the simulator mechanism 103 is smaller than the degree of freedom of motion 6 of the aircraft, a control method that focuses on reproducing translational degrees of freedom (x, y, z degrees of freedom) will be examined here. The G vector is originally a 6xl column vector having six elements, but in this embodiment, which focuses only on the degree of translational freedom, for the sake of simplicity, the G vector has only elements corresponding to three degrees of freedom of translation. Expressed as a 3xl vector.

α_ｂが与えられた時、被験パイロットをｘ、ｙ、ｚ軸について、それぞれ角度φ、θ、ψだけ回転すると、被験パイロットに作用するＧベクトルは次式（１）となる。関数Ｅ_αｂはｘ軸に関する回転と、ｙ軸に関する回転と、さらにｚ軸に関する回転を連続的に行なうことを一括して示している。

このように、上記式（１）について、収束演算によりα＝α_ｍとするジンバル角度φ、θ、ψの数値解を得ることができる。 As shown in FIG. 3, the G vector of the tip of the swing arm 44 and alpha _b, x-axis turning tangentially, y-axis turning center direction, the upward direction is defined as z-axis.
Given α _b , if ‖α _b ‖ = ‖α _m ‖, α = α _m should be able to be obtained by appropriately changing the attitude angle of the pilot. The attitude angle search method at this time is as follows.
That is, the transformation that rotates by the angles φ, θ, and ψ with respect to the x, y, and z axes, respectively, is expressed by

When α _b is given and the subject pilot is rotated about the x, y, and z axes by angles φ, θ, and ψ, respectively, the G vector acting on the subject pilot is expressed by the following equation (1). The function E _αb collectively indicates that rotation about the x axis, rotation about the y axis, and rotation about the z axis are continuously performed.

As described above, numerical solutions of the gimbal angles φ, θ, and ψ with α = α _m can be obtained for the above formula (1).

Next, a calculation in the arm turning speed calculation means 11 is performed. As described above, it is assumed that ‖α _b ‖ = ‖α _mに て in the calculation by the simulator acceleration angular velocity calculation means 13, but it is difficult to actually do this. Therefore, the arm turning speed calculation means 11 adjusts the turning speed and acceleration of the arm so that ‖α _b ‖ = ‖α _m確 実 is established. When the length of the arm and L _a, the acceleration of the tip becomes the following equation. The coordinate system is a right-handed system according to the custom of an aircraft, with the vertical downward direction being positive of z. FIG. 4 shows each component of the arm tip acceleration.

上式は、ωについての微分方程式であるので、実装時には離散化して数値積分してω_ａの解軌道を求めるようにする。 Therefore, in order to establish ‖α _b ‖ = ‖α _m ‖, the angular acceleration of the arm may be determined as in the following equation (2).

Above expression, since it is the differential equation for omega, and numerical integration and discretization so as solving trajectory omega _a during mounting.

  When the solution is obtained by the calculation in the arm turning speed calculating means 11 and the simulator acceleration angular velocity calculating means 13 in this way, the airframe motion model derived by the airframe motion model calculating means 14 and the acceleration angular velocity calculating means 13 are obtained. The gimbal angle calculation means 12 calculates the gimbal angle correction amount based on the translational acceleration and angular velocity deviation calculated by the above and the angular speed of the turning axis, and issues a command to the gimbal shaft drive means 22 by an electrical signal.

Here, an example of calculation in the gimbal angle calculation means 12 will be described.
In order to make the translational acceleration and the rotational angular velocity acting on the simulator mechanism 103 completely coincide with each other, the above formula (1) relating to the translational acceleration and the following formula (3) relating to the rotational angular velocity are simultaneously calculated in total of six formulas (4). Must be met.
Equation (3) relating to the rotational angular velocity is expressed as follows from the rotational angular velocity vector of the test pilot and the rotational angular velocity of the gimbal.

Moreover, Formula (4) is as follows.

However, since the above equation (4) is a nonlinear simultaneous equation for the gimbal angle, it is difficult to derive an analytical solution. Therefore, we will solve numerically by the following procedure.
The simulator control mechanism 101 only needs to be able to calculate the numerical value of the gimbal angle output at the next time step. Assuming that the current time is t and the time step of the calculation of the simulation control mechanism 101 is dt, the gimbal angle is corrected so that the above equation (4) is satisfied at time t + dt. The value of the gimbal angle at time t, the translational acceleration and the rotational angular velocity of the actual cockpit are represented by perturbation δ around the origin.

When the above equation (4) is discretized at time t and time t + dt, the following equation (5) is obtained. The derivative is a numerical derivative.

補足すると、αはアーム先端の並進加速度ベクトルα_ｂを被験パイロットの並進加速度ベクトルに変換した値で、Ｒ_gimはジンバルの回転角速度を被験パイロットの回転角速度に変換する行列で、Ｘは次の行列を簡略表記したものである。

Here, the symbols α and R _gim are simplified expressions of the right side of the above equation (4), and are the following equations.

Supplementally, α is a value obtained by converting the translation acceleration vector α _b of the arm tip into the translation acceleration vector of the test pilot, R _gim is a matrix for converting the rotation angular velocity of the gimbal into the rotation angular velocity of the test pilot, and X is the following matrix: Is abbreviated notation.

In the above equation (5), if δα and δω are the difference between the acceleration / angular velocity of the actual cockpit at time t + dt and the reproduced acceleration / angular velocity of the simulation apparatus 100 at the current time t, the inverse of equation (5) The correction amount of the gimbal angle is obtained from the calculation. That is, the gimbal angle correction amount from time t to time t + dt is formally expressed as the following equation (6).

However, since the size of the matrix X is 6 × 3, X has no inverse matrix and cannot be implemented in this form. The reason why X does not have an inverse matrix is that although there are a total of five accelerations and angular velocities, the simulation apparatus 100 has only three gimbals that can be operated, and the number of operation amounts is insufficient. When the number of manipulated variables is insufficient, the least square method is generally applied, and this is also used in this embodiment.
When the above equation (6) is solved by the method of least squares, the gimbal angle command is obtained by the following equation (7).

  According to such a flow, not only can the translation pilot be faithfully sensed as in the past, but also control that performs simulation in consideration of the angular velocity, such as simulator sickness given to the pilot Discomfort can be removed.

FIG. 7 is a diagram showing a second embodiment according to the present invention. Similar to the first embodiment, the simulation apparatus 100 includes a simulator control mechanism 101, a simulator drive mechanism 102, and a simulator mechanism 103. Since the simulator drive mechanism 102 and the simulator mechanism 103 have the same configuration as that of the first embodiment, description thereof is omitted.
In the second embodiment, the simulator control mechanism 101 includes a simulator acceleration angular velocity calculation means 13, a body motion model calculation means 14, and a 4-axis command calculation means 15.

  The body motion model calculating means 14 calculates a body motion model composed of translational acceleration in three axial directions and an angular velocity about three axes from the operation information input by the test pilot, and the simulator acceleration angular velocity calculating means 13 includes the gimbal The translational acceleration and angular velocity acting on the test pilot 30 are calculated from the gimbal angle of the shaft. The four-axis command calculating means 15 calculates the angular velocity of the turning axis from the airframe motion model, and gives a gimbal based on the calculated translational acceleration and angular velocity, the deviation of the motion model, and the angular velocity of the turning axis. Calculate the amount of angle correction. That is, the pivot axis and the gimbal axis are rotationally driven by fully coordinating the total four axes of the pivot axis and the gimbal axis.

Here, an example of calculation in the four-axis command calculation means 15 will be described.
In the first embodiment described above, control is performed so that the swivel arm is the main and the gimbal follows this, such as rotational conversion by the biaxial gimbal after the angular velocity of the swivel arm is determined. In this embodiment, for the purpose of avoiding an excessive burden on the actuator used for the swing arm, control is performed in which the total of the four axes including the swing arm and the three gimbal axes are completely coordinated.
In this embodiment, the acceleration and angular velocity of the simulator mechanism 103 are expressed by the following equation (8).

The above equation (7) is linearly approximated for minute changes around various quantities at time t.
In order to simplify the notation, the column vectors of the 3 × 3 transformation matrix R _gim are represented as g ₁ , g ₂ , and g ₃ . That is, [g ₁ g ₂ g ₃ ]: = R _gim .
If δα and δω are taken as the difference between the acceleration / angular velocity of the actual cockpit at time t + dt and the reproduced acceleration / angular velocity of the simulation mechanism 103 at the current time t, the correction amount of the cymbal angle can be calculated from the inverse calculation of the following equation (9). Desired.

That is, the four-axis angle correction amount from time t to time t + dt is formally expressed as the following equation (10).

かかる実施例によれば、駆動装置への負荷の均等配分が可能となり、回転軸のトルク飽和や速度飽和による模擬精度の劣化を防止することができる。 Further, as in the first embodiment, a coefficient matrix W for designating reproduction accuracy for each degree of freedom is introduced, and further, the origin of the perturbation on the left side is arranged as a 4-axis angle or angular velocity at time t. The following equation (11) is obtained as a command value for the four axes of t + dt.

According to this embodiment, it is possible to evenly distribute the load to the drive device, and to prevent deterioration in simulation accuracy due to torque saturation and speed saturation of the rotating shaft.

FIG. 8 shows a third embodiment of the simulation apparatus according to the present invention. In FIG. 8, the description of the same configuration as in FIG. 1 is omitted.
The simulation apparatus 100 according to the third embodiment includes a simulator control mechanism 101, a simulator drive mechanism 102, and a simulator mechanism 103 (see FIG. 1). The simulator control mechanism 101 includes an arm turning speed calculation means 11 and The weighted gimbal angle calculating means 12, the simulator acceleration angular velocity calculating means 13, the body motion model calculating means 14, and the reproduction accuracy setting means 16 are configured.
The simulator driving mechanism 102 includes a turning driving means 21 and a gimbal shaft driving means 22. The gimbal shaft driving means 22 includes a yaw axis driving means 22a, a pitch axis driving means 22b, and a roll axis driving means 22c. .

In this embodiment, the reproduction accuracy setting means 16 is incorporated in the first embodiment, and the reproduction accuracy setting means 16 is for specifying the reproduction accuracy of acceleration and angular velocity according to the purpose of use of the simulation. It has a function of outputting a weighting coefficient. One weighting factor is set for each of the five degrees of freedom of three translational accelerations and three rotational angular velocities.
As an example of the weighting factor setting method, for example, when calculating the correction amount of the gimbal angle in the first embodiment, when accurately reproducing the translational acceleration, the weighting factor of the translational acceleration is set to 1 and the weighting factor of the rotational angular velocity. If the rotational angular velocity is accurately reproduced, the rotational angular velocity weighting factor is 1 and the translational acceleration weighting factor is 0, or all degrees of freedom are reproduced with equal accuracy. A weighting coefficient is assigned such that the weighting coefficient is 1.

Based on this weighting factor, the weighted gimbal angle calculation means 12 ′ calculates a gimbal angle command. An embodiment of calculation of the weighted gimbal angle calculation means 12 ′ will be described. The calculation of the weighted gimbal angle calculation means 12 ′ is the following modification to the gimbal angle calculation means 12 of FIG.
That is, to specify the reproduction accuracy for each degree of freedom, a diagonal weight matrix W is added to the left side of the equation (6) shown in the first embodiment as follows.

As described above, the simulation accuracy can be improved by setting the weighting coefficient according to the purpose of use of the simulation.
Of course, the reproduction accuracy setting means 16 can also be applied to the second embodiment.

9 and 10 show an application example of the reproduction accuracy setting means 16 of FIG. 8. FIG. 9 shows the reproduction accuracy setting means 16 for designating the reproduction accuracy based on the flight state output from the aircraft motion model. The weight coefficient is changed from moment to moment.
According to this, it is possible to obtain the best sensation reproduction accuracy at that moment by concentrating the reproduction error on the motion axis having the smallest human sensitivity according to the driving conditions such as the flight state.
FIG. 10 is provided with an interface means 17 for inputting a weighting coefficient for adjusting the weighting coefficient by a test pilot using a mathematical expression or a graph. As a result, the simulation accuracy can be adjusted in accordance with the feeling of each pilot. It is also possible for the test pilot to fine-tune the simulation accuracy by himself.

  In addition to aircraft simulation, this embodiment can be applied to general swinging devices such as automobiles and amusement devices. At this time, the detailed design is changed according to the purpose of use by changing the degree of freedom as appropriate.

It is a block diagram which shows the outline of the simulation apparatus which concerns on embodiment of this invention. It is a block diagram which shows the structure of the control mechanism and drive mechanism of the simulation apparatus which concern on this 1st Example. It is explanatory drawing which shows the simulator mechanism which concerns on embodiment of this invention. It is a figure explaining the arm tip acceleration of the simulator mechanism which concerns on this 1st Example. It is an elevation view showing a simulator mechanism according to an embodiment of the present invention. It is a front view which shows the simulator mechanism which concerns on embodiment of this invention. It is a block diagram which shows the structure of the control mechanism and drive mechanism of the simulation apparatus which concerns on the 2nd Example. It is a block diagram which shows the structure of the control mechanism and drive mechanism of the simulation apparatus which concerns on the 3rd Example. It is a block diagram which shows another Example of the reproduction precision setting means in FIG. It is a block diagram which shows another Example of FIG.

Explanation of symbols

DESCRIPTION OF SYMBOLS 11 Arm turning speed calculation means 12 Gimbal angle calculation means 13 Simulator acceleration angular speed calculation means 14 Airframe motion model calculation means 15 4-axis command calculation means 16 Reproduction accuracy setting means 17 User interface means 21 Swiveling drive means 22 Gimbal axis driving means 43 Turning apparatus 44 Pivot Arm 46 Pivot Axis 54 Yaw Axis Rotation Device 55 Yaw Axis 56 Pitch Axis Rotation Device 57 Pitch Axis 58 Roll Axis Rotation Device 59 Roll Axis 100 Simulation Device 101 Simulator Control Mechanism 102 Simulator Drive Mechanism 103 Simulator Mechanism

Claims (5)

A simulation apparatus comprising means for calculating a virtual vehicle motion model based on operation information input by a subject, and means for rotationally driving a plurality of axes including a turning axis and a plurality of gimbal axes based on the motion model. In
A turning speed calculating means for calculating a turning speed of the turning axis based on the motion model, an acceleration angular speed calculating means for calculating a translational acceleration and an angular speed acting on the subject from the gimbal angle, and the calculated translational acceleration, respectively. And an angle calculation means for calculating a correction amount of the gimbal angle based on the angular velocity, the deviation of the motion model, and the angular velocity of the pivot axis,
A simulation apparatus, wherein the rotation driving means is driven based on the calculated motion data, and the rotational angular velocity is reproduced together with the translational acceleration acting on the subject. A simulation apparatus comprising means for calculating a virtual vehicle motion model based on operation information input by a subject, and means for rotationally driving a plurality of axes including a turning axis and a plurality of gimbal axes based on the motion model. In
Acceleration angular velocity calculation means for calculating translational acceleration and angular velocity acting on the subject from the gimbal angle, respectively, and calculating the angular velocity of the turning axis from the motion model, and the calculated translational acceleration and angular velocity and the deviation of the motion model And a turning speed / angle calculating means for calculating a correction amount of the gimbal angle based on the angular speed of the turning axis,
A simulation apparatus, wherein the rotation driving means is driven based on the calculated motion data, and the rotational angular velocity is reproduced together with the translational acceleration acting on the subject.   3. The simulation apparatus according to claim 1, further comprising: a reproduction accuracy setting unit that sets a weighting factor such that any one of the accelerations and the angular velocities obtained by the acceleration angular velocity calculation unit emphasizes the reproduction accuracy. .   4. The simulation apparatus according to claim 3, wherein the reproduction accuracy setting means sequentially changes the weighting factor based on a vehicle motion model.   4. The simulation apparatus according to claim 3, wherein the reproduction accuracy specifying means comprises interface means for allowing the subject to input a weighting coefficient.

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