JPH102959A - Control-indicated value input device for control table for terminal control - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a control-indicated value input device effectively grasps the operational state of an aircraft and safely, effectively controls it by visually displaying positional, heading, altitude and speed information of the aircraft based on these information and minimizing the movement of a line of sight on a visual screen to the minimum limit. SOLUTION: The input device has an aircraft position display unit 102-1 for visually displaying positional, heading, altitude and speed information of an aircraft based on these information to manage the operation of the aircraft in a terminal control using a radar. Control indicated values of the heading, altitude and speed information are individually input to the unit 102-1 by a heading dial 105-1, an altitude dial 105-2 and a speed dial 105-3.

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a control instruction input device for a terminal control console.

[0002]

2. Description of the Related Art Conventionally, techniques in such a field include:
For example, there are the following. FIG. 15 is a schematic configuration diagram of such a conventional terminal control console, and FIG.
Is an explanatory diagram of the control airspace, and FIG. 17 is an instrument flight system (IFR)
FIG. 18 is a diagram showing an example of a flight ticket (FPS) in an instrument flight system (IFR).

First, terms relating to aircraft operation management will be described. ACC (Area Control Center):
The Air Traffic Control Department is an organization that performs air traffic control operations and partial access control operations.Specifically, it sets and raises control intervals for aircraft that fly in control zones in the airspace under their control by instrument flight. Approve jurisdiction such as approval and descent approval.

[0004] ARTS (Automated Rada)
r Terminal System): A terminal radar information processing system processes information on an airport surveillance radar and a flight plan by an electronic computer system, and displays information such as the position of an aircraft and a flight number on a display device of a control console of a terminal control station. It is a system that displays information. FDP (Flight Data Processin)
g System): What is a flight plan information processing system?
A, B, C by computer installed in A control section
And D automatically receive flight plan information from each control unit, and after performing intensive processing, provide information necessary for flight control (FPS) and other control to the controller via a printer and CRT display device. System.

[0005] FP (Flight Plan): A flight plan is a plan that is required to be submitted to an air traffic service organization when an aircraft is about to fly, and includes a model, flight number, departure place, destination, In addition to the items necessary for controlling the aircraft such as flight path, flight altitude, flight speed, radio equipment, fuel amount displayed in time, rescue equipment installed, etc.
The necessary items in case of search and rescue are to be described. In particular, for aircraft departing by the Instrument Flight Scheme (IFR), with respect to the submitted Flight Plan (FP),
It is required to get approval from the air transport agency.

[0006] FPS (Flight Progress)
Strip): The operation slip includes information for each aircraft necessary for air traffic control, and is arranged on each relevant control console. Based on the FPS, air traffic controllers use the FPS to issue air traffic control approvals, plan for radar control, and perform manual air traffic control. FIG. 18 shows an example of the flight ticket (FPS). According to this, Japan Airlines flight 354 is a Flight Planning Information Processing System (FDP)
Computer number 0657, secondary radar individual code 17
Assigned 67, altitude 37,000 feet, flight route Oita VORDME, air route V37, Kushimoto VO
RTAC, Air Route W27, Oshima VORTAC, Onjuku VO
The Aircraft has obtained air traffic control approval from Tokyo International Airport via RTAC, took off from Fukuoka Airport at 23:36 Greenwich time, is flying at an airspeed of 486 knots, and will pass over Oshima at 00:30.

IFR (Instrument Frig)
ht Rules): The instrument flight method means that a flight takes off at an airfield with a control zone and ascends or descends and landing for that purpose, and always flies according to the instructions of a control agency (controller) according to a prescribed flight path. Also, in a flight in a control area other than the above, it is a method of flying on a predetermined flight route in accordance with an instruction of a control agency.

[0008] RDP (Radar Data Proc)
essing System): An air route radar information processing system is a system installed in an air traffic control unit (ACC) for processing information of an air route monitoring radar, and an aircraft is displayed on a display device installed in each control console. And information such as flight number and flight number. VFR (Visual Flight Rules):
The visual flight method is any flight method other than the instrument flight method (IFR).

[0009] Handoff refers to the transfer of aircraft control between controllers in adjacent control areas. First, the control airspace will be described. As shown in FIG. 16, the control airspace includes a control zone 1, an access control zone 2, and an air traffic control zone 3, and further includes an offshore control zone 4 and a non-control airspace 5. The air traffic control zone 3 is controlled by an ACC controller, the control zone 1 is controlled by a controller at the control tower of the airport, and the access control zone 2 is controlled by a controller performing terminal control operations (approach control).

Next, an outline of the air traffic control operation will be described. Aircraft flight systems are broadly divided into VFR and IFR. The IFR flies in accordance with the instructions of an air traffic controller and flies while measuring the airway connecting the radio sign facilities with an instrument mounted on the aircraft. The duties of air traffic controllers in the airfield control tower (airfield air traffic control services)
Generally, a plane with a radius of 5 nautical miles (approximately 9 km) and a columnar airspace with a height of 3000 feet (approximately 900 m) from the airport's mark is called the control zone. It is.

The terminal control operation is to perform radar guidance for an IFR aircraft flying in a certain airspace (approach control zone) around an airport for setting a control interval and a landing order. Air traffic control services are control services performed on all IFR aircraft flying in areas other than the area around the airport.Specifically, the flight route, altitude, time, etc., are specified, and Is to set a safety interval between aircrafts by means of position reporting or radar monitoring.

Next, an example of navigation of an aircraft by the instrument flight system (IFR) will be described. As shown in FIG. 17, (1) In response to the departure of aircraft 10, Fukuoka ACC instructs the route, altitude, etc., to the destination (Tokyo International Airport 11) via the control tower at Fukuoka Airport. (2) The Fukuoka Terminal Control Center conducts radar guidance for the aircraft 10 in the Fukuoka Access Control Zone, and issues a jurisdiction boundary line C1.
Control of aircraft 10 will be transferred to Fukuoka ACC in the vicinity.

(3) The Fukuoka ACC sets an interval with another aircraft by a position report from a radar or an aircraft, and performs control transfer of the aircraft 10 to the Tokyo ACC near the jurisdiction boundary line C2. (4) The Tokyo ACC lowers the altitude to a certain altitude while setting an interval with the other aircraft, performs control transfer of the aircraft 10 near the jurisdiction boundary line C3, and instructs communication with the Tokyo Terminal control station.

(5) The Tokyo Terminal Control Center conducts radar guidance of the aircraft 10 to the landing approach start point in the Tokyo Access Control Zone 13. Next, the terminal control console will be described. As shown in FIG. 15, the terminal control console has a radar information display / operation unit 21 at a seat A on the left side, and a voice selection unit 2 at the left end and upper part thereof.
2, a strip holder 23 for holding an operation slip (FPS), an FDP data input / output device 24, and the like are provided in a seat B on the right side.

[0015]

Today, the demand for air traffic continues to increase in all parts of the world. In order to solve this problem, we are aiming for the fusion of new technologies and global unification. Among them, the data link of communication between the controller and the pilot is being studied. Currently, air traffic control operations are performed by air traffic control instructions, radar confirmation of aircraft position and altitude by radar, management of flight tickets (FPS), and the like.

It is considered that the future control operations will change greatly due to the data link of communication. In view of this situation, the present invention displays these information visually based on aircraft position information, heading information, altitude information, and speed information, and minimizes the movement of the line of sight on the visual screen. It is an object of the present invention to provide a control instruction value input device of a terminal control console capable of accurately grasping the operation status of an aircraft and performing safe and reliable control.

[0017]

In order to achieve the above object, the present invention provides: (1) a control instruction input value device for a terminal control console for controlling aircraft operation in terminal control using a radar or the like; Based on the aircraft position information, heading information, altitude information and speed information, having an aircraft position display screen that can visually display these information, heading information, altitude information, speed information on the aircraft position display screen In this case, a control instruction value can be input individually.

[2] The control instruction value input device of the terminal control console for controlling aircraft operation according to the above [1], wherein the heading information, altitude information and speed information are provided with dial-type analog input means. It is like that. [3] In the control instruction value input device of the terminal control console for controlling aircraft operation according to [1], the trackball, the headball information, the altitude information, and the speed information adjacent to the trackball, A heading dial, an altitude dial, a speed dial, and an enter bar arranged adjacent to each of the heading dial, the altitude dial, and the speed dial, which can individually input all the control instruction values. Are provided.

Therefore, based on the position information, heading information, altitude information, and speed information of the aircraft, the information is visually displayed, and the movement of the line of sight on the visual screen is minimized to operate the aircraft. It is possible to provide a control instruction value input device of a terminal control console capable of accurately grasping the situation and performing safe and reliable control.

In addition, the heading information, altitude information, and speed information can be accurately changed on a visual screen, and a control instruction can be accurately input and displayed in an analog manner. Further, the control instruction values of heading information, altitude information, and speed information can be individually input and displayed as appropriate.

[0021]

Embodiments of the present invention will be described below with reference to the drawings. FIG. 1 is a diagram showing a display device of a terminal control console for controlling aircraft operation in terminal control according to an embodiment of the present invention, FIG. 2 is a configuration diagram of a composite display of the display device, and FIG. 1 is a schematic overall configuration diagram of an aircraft operation management system performed. Here, with regard to the aircraft ordering, it is possible to order the aircraft arrival and the aircraft departure.

In FIG. 3, reference numeral 100 denotes a control console, and a composite display 102 is arranged on the first seat 101. The composite display 102 includes a trackball 103, a hand-off button 104, a dial input unit 105, and a mouse 106. It is connected. Also,
An operation slip display unit (list display) 202 is arranged in the second seat 201, and a keyboard 203 and a mouse 20 are arranged.
4 etc. are connected.

The seats 101 and 201 are connected to the LAN 301
As a result, through the interface (I / F) 401, F
DP (aircraft operation management device) 402, aircraft order processing device (here, aircraft arrival / departure ordering device) 40
3. ACC (air traffic control unit) 404, tower (control tower control unit) 405, communication between the controller and the aircraft 410 is performed in a digital manner, and the position information, heading information, altitude information, speed information, etc. of the aircraft 410 are obtained. Get Data Link 40
6, the radar 407 is provided. Further, it is connected to another control console via the LAN 301.

Here, the data link 406 has (1) communication using a satellite, and (2) communication using a VHF band (VD
L: VHF digital link) or (3) communication using a secondary radar (SSR). 1 and 3, a composite display 102 is arranged in front of a first seat 101, a visual aircraft position display section 102-1 is arranged on the left side of the composite display 102, and a visual aircraft order display is also shown on the right side. The unit 102-2 is arranged. For details,
It will be described later with reference to FIGS.

In FIG. 1, an operation section in front of a composite display 102 arranged on a control console 100 includes:
In order from the left, a trackball 103, a handoff button 104, a heading dial 105-1, an altitude (level) dial 105-2, and a speed (speed) dial 1
05-3, a dial input unit 105 including an enter bar (fixed input unit) 105-4 is arranged, and a heading dial 105-1, an altitude dial 105-2, and a speed dial 105-3 are arranged independently, respectively. And input is possible. Also, the aircraft order display unit 102
Mouse 106 as an input device for performing the display of -2
Is connected.

An operation slip display section (list display) 202 is arranged at the second seat 201, and an operation section at the front is provided with:
A keyboard 203 and a mouse 204 are provided. FIG. 4 is a functional block diagram of an aircraft position display unit of the display device of the aircraft operation management system according to the embodiment of the present invention. In this figure, reference numeral 501 denotes a trackball processing unit;
Is a display processing unit, 503 is a selected target determination unit, 504
Is a display status storage unit, 505 is a selected target display control unit, 506 is a display data generation unit, 507 is a selection storage unit,
Reference numeral 508 denotes a control device storage unit, 509 denotes a dial processing unit, 510 denotes a selection target instruction storage unit, 511 denotes a control instruction content storage unit, 512 denotes a handoff reception storage unit,
513, a reception processing unit; 514, a handoff control unit;
Reference numeral 5 denotes a handoff transmission waiting storage unit, and 516 denotes a transmission unit.

A trackball processing section 501 is connected to the trackball 103, a handoff button 104 is connected between the selection storage section 507 and the selection target instruction storage section 510, and an aircraft position is connected to the display processing section 502. The display unit 102-1 is connected. FIG. 5 is a functional block diagram of the dial processing unit of the aircraft position display unit of the display device of the aircraft operation management system according to the embodiment of the present invention.

In this figure, reference numeral 521 denotes a data sampling unit connected to a dial input unit comprising a heading dial 105-1, an altitude dial 105-2, a speed dial 105-3, and an enter bar 105-4, and 522 denotes an A / D. The conversion unit 523 is an initial value storage unit, 524 is a current value storage unit, 525 is a numerical value detection unit, and 526 is a data transmission unit.

Hereinafter, the operation of the dial processing unit will be described. (1) The initial value storage unit 523 indicates that the target has been selected.
To be informed. (2) The analog signal output from the dial (105-1 to 105-3) is transferred to the data sampling unit 521. (3) The analog data sampled by the data sampling unit 521 is output to the A / D conversion unit 522 in order to convert the analog data into digital data.

(4) The digital data when the target is selected is stored in the initial value storage unit 523. (5) Also, the signals from the dials (105-1 to 105-3) are always A / D converted in the same manner as in (2) and (3) and input to the current value storage unit 524. (6) The data is transferred to the numerical value detection unit 525 in order to compare the data stored in the initial value storage unit 523 with the data stored in the current value storage unit 524.

(7) The difference between the data in the initial value storage unit 523 and the data in the current value storage unit 524 is transferred to the data transmission unit 526, and is always transmitted from the data transmission unit 526. (8) When the confirmation input is notified from the confirmation input unit 105-4, the data transmission unit 526 transmits the confirmation input data. (9) Reset input is made by dial (105-1 to 105-
3) is sent to the data transmission unit 526.

FIG. 6 is a functional block diagram of the aircraft order display section of the display device of the aircraft operation management system according to the embodiment of the present invention. In this figure, 601 is a mouse input unit connected to the mouse 106 as an input device for displaying the aircraft order display unit 102-2, 602 is a display processing unit, 603 is a display storage unit, and 604 is a selection determination unit. , 605
Is a transmission data processing unit, 606 is a reception data processing unit, 60
Reference numeral 7 denotes a display data generation unit, and the display processing unit 602 is connected to the aircraft order display unit 102-2.

Hereinafter, the operation of the aircraft order display section will be described. (1) Normally, a signal from the aircraft order processing device 403 (see FIG. 3) is received by the reception data processing unit 606. (2) Transfer the received data to the display data generation unit 607 to generate displayable data.

(3) The parasitic data is transferred to the display processing unit 602. (4) Display on the aircraft order display section 102-2. (5) When selecting with the mouse 106, use the mouse 106
Is received by the mouse input unit 601. (6) The data is converted by the mouse input unit 601 and the mouse data is transferred to the display processing unit 602.

(7) At the same time as displaying on the aircraft order display section 102-2, the range selected by the mouse 106 is transferred to the display storage section 603. (8) The data is transferred to the selection determining unit 604, and it is determined whether the selected range is valid. (9) If valid, transfer the data to the transmission data processing unit 605. If it is invalid, it notifies the display processing unit 602 that it is invalid, and performs invalid display.

(10) The data transferred to the transmission data processing unit 605 is transmitted to the aircraft order processing device 403 (see FIG. 3). Then, as described later, the aircraft order display unit 102-2 displays the distance intervals in a tree structure in which the distance intervals are converted into time based on the information taken in from the aircraft order processing device 403. Hereinafter, the operation of this system will be described with reference to the above functional block diagram.

FIG. 7 is a functional block diagram for explaining the operation when handing off from another seat (or a control unit) to the own seat according to the embodiment of the present invention. First, the case of handoff from the other seat (or the control unit) to the own seat will be described with reference to FIG. Note that, in FIG. 7, portions that are not related to this operation are omitted from the functional blocks in FIG.

(1) First, handoff information is received from another seat via the reception processing unit 513. (2) The received handoff information is stored in the handoff receiving storage unit 5
12. Notify the handoff control unit 514. Further, the position data is transmitted to the display data generation unit 506. (3), (4), (5) The handoff control unit 514 displays the reception of the handoff request on the aircraft position display unit 102-1 in order to display the display data generation unit 506 and the display processing unit 5.
02, the hand-off input state is displayed on the aircraft position display section 102-1.

(6) The operator who sees the display inputs a target selection from the trackball 103 to the trackball processing unit 501 to accept the handoff. (7) The selected target determination unit 503 is notified of the selection from the trackball processing unit 501. (8) In the selected target determination unit 503, the display status storage unit 5
From 04, the cursor position of the trackball 103 and the aircraft target position are input, and the selected target is specified. Thereafter, the contents of the in-seat control device storage unit 508 and the handoff reception storage unit 512 are checked, and the selected target is determined to be the target in the handoff input state.

(9), (10), (11) Selected target determination unit 50
3 displays the target selection state on the aircraft position display unit 102-1 via the display data generation unit 506-display processing unit 502. Also, data is transferred from the selected target determination unit 503 to the selection storage unit 507. Further, data is transferred from the selected target determination unit 503 to the dial processing unit 509 and the transmission unit 516.

(12) The operator who sees the display operates the handoff button 104 to input execution of handoff. (13), (14), (15) Indicates the execution of handoff. That is, from the selection storage unit 507 to the self-control device storage unit 508,
The data is transmitted to the display data generation unit 506, the transmission unit 516, and the handoff reception storage unit 512, respectively, and further displayed on the aircraft position display unit 102-1 via the display processing unit 502 from the display data generation unit 506.

When the machine is handed off and becomes a control target of the own seat, the handoff receiving storage unit 512
Is erased, and the data is written into the in-control device storage unit 508. FIG. 8 is a functional block diagram illustrating an operation in the case of handoff from one's seat to another seat according to the embodiment of the present invention.

Hereinafter, a case of handoff from one's seat to another seat will be described with reference to FIG. Note that, in FIG. 8, portions that are not related to this operation are omitted from the functional blocks in FIG. (1) A target to be handed off to another seat is selected and input from the trackball 103 and the trackball processing unit 501 is input.
Send to

(2) The trackball processing unit 501 notifies the selection of a target from the selected target determination unit 503.
Notify to (3) In the selected target determination unit 503, the display status storage unit 5
From 04, the cursor position of the trackball 103 and the aircraft target position are input, and the selected target is specified. Thereafter, the contents of the in-seat control device storage unit 508 are checked, and the selected target is determined to be a target under the in-seat control.

(4) The data of the selected target is transferred from the selected target determination section 503 to the selected target display control section 505. In addition, the selection target determination unit 503
Transmits the target data to the dial processing unit 509 and the transmission unit 516. (5) The control instruction content storage unit 511 is checked, and if there is a control instruction in the past, the data is transferred to the selected target display control unit 505 if there is no control instruction, and if not, the data stored in the display status storage unit 504 is transferred.

(6), (7), (8) The transferred data is displayed on the aircraft position display section 102-1. That is, the information is displayed on the aircraft position display unit 102-1 via the display data generation unit 506 and the display processing unit 502. Further, the contents are transferred to selected target instruction storage section 510. (9) The operator who sees the display operates the handoff button 104 to input execution of handoff.

(10), (11), (12) Display during handoff transmission. That is, the information is displayed on the aircraft position display unit 102-1 from the selected target instruction storage unit 510 via the display data generation unit 506 and the display processing unit 502. In addition, data is stored in the handoff transmission waiting storage unit 515 so that another target can perform handoff during transmission, and the handoff information is transmitted to the handoff destination seat via the transmission unit 516.

(13), (14) Handoff approval is received from the handoff destination seat. That is, it is received from the reception processing unit 513 and transmitted to the handoff control unit 514. (15) The hand-off transmission waiting storage unit 515 is checked, and it is checked which received hand-off response is the received content. (16), (17), (18) Displays the end of handoff. That is, the end of handoff is displayed on the aircraft position display unit 102-1 from the handoff control unit 514 via the display data generation unit 506 and the display processing unit 502. In addition, the contents of the hand-off transmission waiting storage unit 515 and the contents of the control device storage unit 508 are deleted.

FIG. 9 shows a heading showing an embodiment of the present invention.
FIG. 4 is a functional block diagram illustrating an operation when changing altitude and speed. Hereinafter, a case where the heading, altitude, and speed are changed will be described with reference to FIG. In FIG. 9, portions that are not related to this operation are omitted from the functional blocks in FIG.

(1) The target of the aircraft to be changed is selected and input on the trackball 103 and transmitted to the trackball processing unit 501. (2) The trackball processing unit 501 transmits to the display processing unit 502 and the selected target determination unit 503 that the target has been selected. (3) In the selected target determination unit 503, the display status storage unit 5
From 04, the cursor position of the trackball 103 and the aircraft target position are input, and the selected target is specified. Thereafter, the contents of the in-seat control device storage unit 508 are checked, and the selected target is determined to be a target under the in-seat control.

(4) The data of the selected target is transferred from the selected target determination unit 503 to the selected target display control unit 505. In addition, the selection target determination unit 503
Transfer the target data to the dial processing unit 509 and the transmission unit 516. (5) The control instruction content storage unit 511 is checked, and if there is a control instruction in the past, the data is transferred to the selected target display control unit 505 if there is no control instruction, and if not, the data stored in the display status storage unit 504 is transferred.

(6), (7), (8) The transferred data is displayed on the aircraft position display section 102-1. That is, the selected target display control unit 505 to the display data generation unit 506,
Aircraft position display unit 102-1 via display processing unit 502
To be displayed. Further, the contents are transferred to selected target instruction storage section 510. (9) The operator inputs the data to be changed by the dial processing unit 509.
To the selected target instruction storage unit 510. (Data obtained by sampling analog dial information in the dial processing unit 509 is input periodically.)

(10), (11), (12) The changed data is displayed on the aircraft position display section 102-1 in real time. That is, the information is displayed on the aircraft position display unit 102-1 from the selected target instruction storage unit 510 via the display data generation unit 506 and the display processing unit 502. (13) The operator who has watched the aircraft position display section 102-1 confirms and inputs the data change from the dial processing section 509.

(14), (15), (16) Data is sent to the transmitting section 516 to notify the pilot. Also, the fact that the pilot is being notified is displayed. The display is displayed on the aircraft position display unit 102-1 from the selected target instruction storage unit 510 via the display data generation unit 506 and the display processing unit 502. (17) Reception processing unit 5 receives notification of acceptance of change instruction from pilot
13 to the selected target instruction storage unit 510.

(18), (19), (20) The data is stored in the control instruction content storage section 511 which stores the fact that the change instruction has occurred. It also indicates that the pilot has accepted the instruction. That is, the information is displayed on the aircraft position display unit 102-1 from the selected target instruction storage unit 510 via the display data generation unit 506 and the display processing unit 502. Also, it transmits from the selected target instruction storage unit 510 to the transmission unit 516.

FIG. 10 is a functional block diagram illustrating the operation of the embodiment of the present invention in a normal state without changing the display. Hereinafter, the normal operation will be described with reference to FIG. Note that, in FIG. 10, portions that are not related to this operation are omitted from the functional blocks in FIG. (1) Location information, heading information, altitude information,
The speed information is received via the reception processing unit 513.

(2), (3) Display the change information in real time. That is, the display data generation unit 506 and the display processing unit 50
2 on the aircraft position display unit 102-1. (4) The display content is stored in the display status storage unit 504. FIG.
1 is an explanatory view of an aircraft position display method on an aircraft position display unit showing an embodiment of the present invention, FIG. 12 is a diagram showing a legend of aircraft position display on the aircraft position display unit, and FIG. 13 is an aircraft position display unit It is a figure which shows the flow of an aircraft position tag display to the user.

Hereinafter, a specific aircraft position display section 102-
1 will be described with reference to FIG. 11, a dotted line 701 indicates a flight route, and a tag 702 indicates a specific code (call sign) of the aircraft, for example, JAL008, altitude 120, and speed 36H. A, B,... Indicate the seats under control.

The display of the tag 702 can be changed according to the arrival or takeoff at the airport. For example, with the trackball 103, the ANA 144
Is selected, the display changes from ANA 144: 80 (altitude) and 28H (speed) to 330 (heading), 80 (altitude), and 28H (velocity), as shown in the frame 703 of FIG.
H (speed) is displayed.

The control instruction input procedure will be described in further detail. (1) In the situation where no aircraft is selected,
The flight number, altitude, and speed are displayed. (2) When the ANA 144 is selected by the trackball 103 as a pointing device, for example, the flight number, heading,
The altitude and speed are displayed, and the position one minute later is displayed. (3) Dial 1 for the selected aircraft
The heading, the altitude, and the speed can be input by using 05-1 to 105-3 and the like. After the control instruction is input, the operation ticket display unit (list display unit: display unit in strip format) is updated by confirming and inputting with the enter bar 105-4.

Here, the flow of tag display on the aircraft position display section will be described with reference to FIG. (1) First, as shown in FIG. 13A, before a control instruction is given, a call sign, here, ANA 144, altitude 80, and speed 28 are displayed (normal state). In addition, the mark △ indicates the position of the aircraft.

(2) Next, as shown in FIG.
When a target is selected to instruct control, ANA1
44, heading 180, altitude 80, and speed 28 are displayed. Here, the input mode is displayed, for example, by changing the overall color. Here, the solid line heading 180, altitude 80, speed 2
Numeral 8 indicates the current values of the heading, altitude, and speed of the aircraft, and the dotted line heading 180, altitude 80, and speed 28 in the lower row (control instruction input area) indicate the input mode. A dotted line connected to the mark indicates a heading.

(3) Next, as shown in FIG.
During the input of the indicated value, for example, a heading 100,
Enter the altitude 60. The speed 28 is not changed and is indicated by a dotted line. (4) Next, as shown in FIG. 13 (d), the enter bar 105-4 is operated to confirm the input, and while waiting for the pilot's confirmation approval, the confirmation confirmation from the pilot is performed by blinking or the like. Indicates that it is waiting.

(5) Next, as shown in FIG.
When the pilot approves the confirmation, the altitude 60 in the lower row (control instruction input area) is displayed. (6) Next, as shown in FIG. 13 (f), when the target is selected again, the heading 18 which is the previous control instruction is issued.
0, the altitude 80, the speed 28, the heading 100, the altitude 60, the speed 28 as the current control instruction, and the time are displayed.

For the selected aircraft,
The heading, altitude, and speed are input using the dials 105-1 to 105-3, etc., and after the control instruction is input, the operation ticket display unit (list display unit) is automatically input by confirming input using the enter bar 105-4. Updated and displayed. Therefore, aircraft location information, heading information,
A first display screen capable of visually displaying the information based on the altitude information and the speed information; and a second display screen capable of inputting list information based on the flight ticket and visually displaying the list information. And the first and second display screens can be displayed in association with each other.

The dials 105-1 to 105-3 required for inputting the heading, altitude, and speed are installed beside the trackball 103 as hardware. In addition, by simultaneously selecting a plurality of aircraft in the aircraft position display unit 102-1, for example, an algorithm for adjusting a time interval of the selected aircraft is activated, and a list of necessary control instructions for each aircraft is provided. Get.

With this configuration, according to the present invention, the present invention supports the controller and the pilot without relying solely on voice communication, and provides information on the position of the aircraft on a visual screen. It is possible to perform safe and reliable control capable of executing confirmation based on aircraft arrival order information. FIG. 14 is an explanatory diagram of an aircraft order display method on the aircraft arrival order display unit according to the embodiment of the present invention.

Hereinafter, a specific aircraft order display section 102-
2 will be described with reference to FIG. Code identifying the aircraft (eg, JAS
288) is arranged in a tree structure at intervals obtained by converting the speed into time, and the aircraft arrival order arriving at the airport from below is displayed on the aircraft order display section 102-2.

That is, the aircraft order display section 102-2 indicates the aircraft order and the time interval between the aircraft. By arranging the aircraft at equal intervals in the vertical direction, the intervals at the junction can be made equal. In addition, it is possible to predict the approach time and the order of aircraft that enter from outside the airspace in charge of control.

This display information is based on information from the aircraft order processing device 403 shown in FIG. Further, the region 705 can be selected also in the aircraft order display section. In this example, the driver joins the control seat A from the control seat C while lowering the altitude, and enters the landing position at the control seat F.

Further, it can be seen that the control of the aircraft taking off from the aircraft taking off at the control seat B is performed. JAL002 that has taken off: The altitude 15 and the speed 18H are displayed as dotted lines in the aircraft order display, and finally disappear. In this way, the operating status of the aircraft can be displayed visually and dynamically and accurately.

Therefore, the controller operates the aircraft position display section 10.
2-1, aircraft order display section 102-2, flight ticket display section 2
02 visually on the screen without moving your eyes,
In addition, it is possible to dynamically and accurately confirm, and it is possible to perform reliable control. With this configuration,
When hand setting from another seat to own seat or from one seat to another seat, it is possible to assist while visually confirming this on the screen, and to perform safe and reliable transfer of control.

Although the terminal control has been described in the above embodiment, the present invention can be appropriately applied to air route control. Further, the present invention is not limited to the above-described embodiments, and various modifications are possible based on the gist of the present invention, and these are not excluded from the scope of the present invention.

[0074]

As described above, according to the present invention, the following effects can be obtained. (1) Based on the position information, heading information, altitude information, and speed information of the aircraft, the information is visually displayed, and the movement of the line of sight on the visual screen is minimized to reduce the operation status of the aircraft. It is possible to provide a control instruction value input device of a terminal control console capable of accurately grasping and performing safe and reliable control.

(2) The heading information, altitude information, and speed information can be accurately changed on a visual screen, and a control instruction can be accurately input and displayed in an analog manner. (3) Heading information, altitude information, and speed information can be individually input and displayed as appropriate.

[Brief description of the drawings]

FIG. 1 is a diagram showing a display device of a control console for terminal control according to an embodiment of the present invention.

FIG. 2 is a configuration diagram of a composite display of a display device of a control console for terminal control according to an embodiment of the present invention.

FIG. 3 is a schematic overall configuration diagram of an aircraft operation management system to which the present invention is applied.

FIG. 4 is a functional block diagram of an aircraft position display unit of the display device of the aircraft operation management system according to the embodiment of the present invention.

FIG. 5 is a functional block diagram of a dial processing unit of an aircraft position display unit of the display device of the aircraft operation management system according to the embodiment of the present invention.

FIG. 6 is a functional block diagram of an aircraft order display unit of the display device of the aircraft operation management system according to the embodiment of the present invention.

FIG. 7 is a functional block diagram illustrating an operation when handing off from another seat (or a control unit) to the own seat according to the embodiment of the present invention.

FIG. 8 is a functional block diagram illustrating an operation in the case of handoff from one's seat to another seat according to the embodiment of the present invention.

FIG. 9 is a functional block diagram illustrating an operation when changing the heading, altitude, and speed according to the embodiment of the present invention.

FIG. 10 is a functional block diagram illustrating an operation in a normal state without a change in display according to the embodiment of the present invention.

FIG. 11 is an explanatory diagram of a method for displaying an aircraft position on an aircraft position display unit according to the embodiment of the present invention.

FIG. 12 is a diagram illustrating a legend of an aircraft position display on an aircraft position display unit according to the embodiment of the present invention.

FIG. 13 is a diagram illustrating a flow of displaying an aircraft position tag on an aircraft position display unit according to the embodiment of the present invention.

FIG. 14 is an explanatory diagram of a method for displaying an aircraft order on an aircraft arrival order display unit according to the embodiment of the present invention.

FIG. 15 is a schematic configuration diagram of a conventional terminal control console.

FIG. 16 is an explanatory diagram of a control airspace.

FIG. 17 is a diagram illustrating an example of navigation of an aircraft by an instrument flight system (IFR).

FIG. 18 shows an operation ticket (F) in the instrument flight system (IFR).
FIG. 14 is a diagram illustrating an example of a (PS).

[Explanation of symbols]

 REFERENCE SIGNS LIST 100 control table 101 first seat 102 composite display 102-1 aircraft position display section 102-2 aircraft order display section 103 trackball 104 handoff button 105 dial input section 105-1 heading dial 105-2 advanced dial 105-3 speed dial 105-4 Enter bar (fixed input unit) 106,204 Mouse 201 Second seat 202 Flight ticket display unit (List display) 203 Keyboard 301 LAN 401 Interface (I / F) 402 FDP (Aircraft operation management device) 403 Aircraft order Processing device 404 ACC (air traffic control unit) 405 Tower (control tower control unit) 406 Data link 407 Radar 410 Aircraft 501 Trackball processing unit 502, 602 Display processing unit 503 Selector Target determination unit 504 Display status storage unit 505 Selected target display control unit 506 Display data generation unit 507 Selection storage unit 508 Self-control device storage unit 509 Dial processing unit 510 Selection target instruction storage unit 511 Control instruction content storage unit 512 Handoff reception storage unit 513 reception processing unit 514 handoff control unit 515 handoff transmission waiting storage unit 516 transmission unit 521 data sampling unit 522 A / D conversion unit 523 initial value storage unit 524 current value storage unit 525 numerical value detection unit 526 data transmission unit 601 mouse input unit 602 Display processing unit 603 Display storage unit 604 Selection determination unit 605 Transmission data processing unit 606 Receive data processing unit 607 Display data generation unit 701 Flight route (dotted line) 702 Tag 703 Frame 705 area

 ──────────────────────────────────────────────────続 き Continued on the front page (72) Inventor Keiichiro Nakagami 1-7-12 Toranomon, Minato-ku, Tokyo Oki Electric Industry Co., Ltd. (72) Inventor Takefumi Nakamura 1-7-12 Toranomon, Minato-ku, Tokyo No. Oki Electric Industry Co., Ltd. (72) Inventor Takashi Sagawa 1-7-12 Toranomon, Minato-ku, Tokyo Oki Electric Industry Co., Ltd. (72) Inventor Tamotsu Sasaki 1-7-12 Toranomon, Minato-ku, Tokyo Oki Inside Electric Industry Co., Ltd.

Claims (3)

[Claims] 1. A control instruction input device for a terminal control console for managing aircraft operation in terminal control using a radar or the like, comprising: (a) aircraft position information;
Based on heading information, altitude information and speed information, the aircraft has an aircraft position display screen capable of visually displaying the information, and (b) heading information is displayed on the aircraft position display screen.
A control instruction input device for a terminal control console that enables individual input of control instruction values for altitude information and speed information. 2. The control instruction value input device for a terminal control console for managing aircraft operation according to claim 1, wherein
The heading information, the altitude information, and the speed information are provided with a dial-type analog input means, and a control instruction value input device for a terminal control console is provided. 3. The control instruction value input device for a terminal control console for managing aircraft operation according to claim 1, wherein
(A) a trackball; (b) a side-by-side heading dial adjacent to the trackball and capable of individually inputting control instruction values for heading information, altitude information, and speed information; and an altitude dial. And a speed dial; and (c) a control indication value for a terminal control console, comprising: a head dial, an altitude dial, and an enter bar arranged adjacent to each of the speed dials. Input device.