JPS5949500A - Combat simulator device - Google Patents

Abstract

(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

[Detailed description of the invention] The present invention V relates to a combat simulator device.

Combat simulator is fighter jet 1j1: force measurement,
For the purpose of developing combat techniques, for example, one fighter aircraft (self (number) vs. 14 aircraft (target)), or two fighter jets (own aircraft + friendly aircraft) vs. Koken aircraft (target), etc. Conventionally, as shown in the block division diagram in Figure 1, a target or friendly aircraft is piloted by a human pilot MP', while a target or friendly aircraft is piloted by a human pilot MP'. Since the battle is simulated depending on the combat ability and will of Ilot Kaishi, the visual control system and control device for the target (also friendly military aircraft) are used! etc. are required for the number of aircraft.
The cost efficiency of the system is poor.
:・〜・・
2 Toshimireta is the machine ii1: J: Turku.
1y′i′;J−j1″′″i K i
ri, “i51!'J) J k ii 25 r, 9
1J 7>' h D・“゛′i valence object is r1 machine t)
Therefore, it is necessary for the pilot to perform a very difficult flight, but since the interface between the pilot and the aircraft is not a direct subject of evaluation, the interface between the pilot and the aircraft is not a direct problem. ``It would be good if it actually flew nearby.''

If the target 2 is piloted by a human/4' pilot, the target will fly close to the actual flight.・−Doware is required.

On the other hand, the judgment of the 9th pilot and the 1st step can be mathematically modeled.
e:I! 'ψ Vertical seats, visibility racks, etc.' are unnecessary, and it is good to secure only the converter's fht, so by adopting this math pilot, it should be possible to improve the cost efficiency, operational efficiency, etc. of the simulator by 1 / It is.

The present study was proposed by JJF Mimata in response to this 41 concern, with the aim of providing JJA with the production of a combat simulator that would improve cost efficiency and operational efficiency, and improve the 4th place of own aircraft. "Chikufu H11 J-band, vision device, self-appointed,
The aircraft motion simulation part consists of the first aircraft arc, the equation of motion of the aircraft 3'J, the mathematical pyro, the Tronock, the Target 71/control system, the calculation of the equation of motion of the target, and the same target as the aircraft data of the aircraft 8 nodes. Exercise 4.4'
! Relative luck between pseudobu, own aircraft and target! uJ+ operation,
It is characterized by comprising a relative motion calculation section that performs scoring.

An example of 1(I) to Book 9 will be explained with reference to FIG. 1fii.
The block line 1/1 indicating the formation of the mathematical pilot in FIG. 3 and FIG.

In the above diagram, 7 is the simulated cockpit of your own aircraft, etc. (hereinafter referred to as the simulated cockpit), 9 is your own aircraft's body button, 10 is the calculation of the equation of motion of your own aircraft, and 7 , 9 , 7 Q
5 to work together to form a 41"j self-protection
No is Mathematics Pyro, Tronoc, 2, t tag site 11 river suspension 11 system, 31t:F, Kuketto 7 Koj, (
(1, iJ) In equation 1.4, 1, 2, 3, and 4 work together to form target motion simulation part #□+□1. 5 is the relative movement ↓j/-16(1;i) before the relative movement between the own aircraft and the plane, and 5 and 6 cooperate to form the relative movement calculating section 411.

The number M pilot logic 1 is, as shown in Fig. 3,
Place W, ' 1, curfew 12 of the line path of F1, 1 Δ seconds later, place 1t'a° of the opponent aircraft is expected to be 13 points to 4 (the opponent made by η) place li/1 ．． Forecast section, latest status of coupon 7 1g, maneuver trial 19,
l (4 separate maneuver trials 20, target after t-1ΔL seconds) 1 Target maneuver trial H consisting of 1 flying state calculation 21, etc.: gX, target, target and own aircraft relative relationship calculation 14, Scoring 15, best maneuver selection, 1ii11a;] 1j quantity setting 17 information ((() 11) Ij is made in the control amount setting 715. In such a device a, the action of each part is The explanation is as follows.

(1) Own luck! (Mountain 4 mo simulated part I mo simulated cockpit 7 surname = Yo Sim The pilot performs 4 quasi piloting of his own aircraft. As a result, control command iE (steering, steering, rudder pedal arrow, throttle, etc.) is given to the aircraft's motion calculation unit...the same applies hereafter), and the motor force is expressed in the autobiography to calculate the aircraft's 2 ri. When calculating the small size, the (mounting data 9 of 4) is also used.

(2) Target movement simulation section Mathematics/Yairoy) Logic 1 is the digit 1 of the other aircraft's Δ in seconds.
t7. is N by curve nointing of the 115-line path.
゛Prediction, also target y) r, 1: Time t KJ
Knoruji 4. The relative position with Np is considered as an initial Cj session. (The maneuver of l='l is attempted at 19. Attempt all 20 maneuvers.

The result of each of these maneuvers is /4'+, Δ in seconds? Depending on the location of the aircraft's target and the attachment of the expected partner aircraft (the target aircraft viewed from the target/i5), the target and own (
Preliminarily determine the relative position 14 of the length 1iIIJ L, as a result, evaluate whether it is desirable to select a multiple maneuver by scoring 15, select the best maneuver 16,
Control corresponding to the next best maneuver: i71: I7
Set.

Here φ. is bank angle command, anc &, j, normal acceleration command, Fc1r-, 'i mislast command, this control h'φC=ane+FC
δ1 by Tadat system an + system 2 using
, δ8, δ8 steering view 3゛1. do. Here, δr
l yo lag-1: It angle, δ. is the elevator 111'e angle, δa is the aileron 1ife angle, and these steering angles δr,
δ8, δ3 and target 4. are [1
Using jI, the target motion is calculated by calculation 3 of the target motion equation.

(3) Relative motion Hama j) Part 7 Own machine motion 41. Accordingly, from the results of the plane's own motion and the target movement determined by the model, we calculate the pairwise motion of the white plane and the plane of the plane by 5, and calculate the Scoring 6 is performed for the 1st and 1st results of the game, and the calculation result d of this relative motion is also fed to the mathematics/guirotrono ri 1 and hardware control 8.

This kind of -4,', 11;', 1:, L'l learning/guironotology l to control the target story.
By doing this between the Sims and the pilot, one person and 11 six minutes Jl Mo4'r5i cockpit, etc., ・k to 1 aircraft, multiple aircraft to multiple aircraft (in this case, friendly forces 7 (t Air-to-air combat (piloted by Mathematics/P Ilot) or iiJ-No.

In addition, in the above-mentioned real MQ 1], a configuration may be adopted in which the feed from the relative movement 5 of the self, others, and the target is not performed in the mathematics/satellite rotation.

This story 1. Even in the formation of
], above; "Similar to this mode of control, the mathematical pilot can use mathematics to manipulate the aircraft, or the mathematical pyro. I will unilaterally send out the number of coupons regardless of the matter.

By staying vertically, the enemy can simulate an attack against this unilaterally flying Turk.
It is in charge of numerical optimization for a certain - rectangular target flight.

In short, according to the present invention, the equation of motion of tJ, self(;some's 4H7,!j pseudo pilot seat, visibility device 1゛f, own aircraft's 4,1 body r-ta, self-A table, Equation 3): Motion simulation section, mathematics/zoironotologic, TARDAT control system, calculation of target's equation of motion, KOOKUUT movement simulation section consisting of aircraft data, relative motion calculation between own aircraft and target, and relative calculation consisting of scoring. Since it is equipped with a converter I/simulator device that is highly cost-effective and operationally efficient, it is extremely useful industrially.

/1. l>'1 concave 1.1j simple 1 situation Ming 11/1ζ
・J-'i'i mino's party, toshimu yū', I don't have to worry about Glock ijii'l! Figure, Figure 2 C1j, Example of the present invention h (6 examples) 5, Glock diagram shown, 31st mel
(t; 12B 21; lI Mathematics, 9th and 10th Toro),
FIG.

No...G 5t, 4゛iro, tronoc, 2...Turkey 8-point decoy 1 system, 3...Equation of motion of target p9.4...Turkey soto rod data, 5...
...Relative motion performance between own aircraft and Turke 8 Soto 19.6...Scoring, 7..., 1';! , j! ie cockpit, etc., 8...no-doware control, 9... own aircraft, amazing aircraft data, 10... own aircraft's equation of motion τ: 1111
...Position of the opponent's aircraft, 12...Kagufinoto of the flight path, 13...The location of the opponent's aircraft after t+Δ (5shi,
Prediction, 14... Relative motion calculation between target and own aircraft -115... Scoring, 16... Best manu-bano scale selection, 17... Control 11. Setting, 18... Latest status f/jA, 79... Maneuver trial, 20...
! 1' Try another maneuver.

Claims (1)

[Claims] The aircraft's cockpit, visibility-I device, aircraft's physical appearance, aircraft movement simulation section consisting of the calculation of the equation of motion of the aircraft, mathematics, ?iro, tronoc, and target. It is characterized by comprising a control system, a target motion simulation section that calculates the equation of motion of the target, a target motion simulation section that includes a tartar, a target aircraft body, and a vehicle, and a relative motion calculation section that computes the relative motion between the own aircraft and the target and performs scoring. computer, simulator equipment