| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 201 | AIR TRAFFIC CONTROL METHOD | PCT/RU2004/000058 | 2004-02-25 | WO2005081201A1 | 2005-09-01 | |
| The invention relates to aviation. The inventive method consists in defining instantaneous information about co-ordinates of airplanes and the trajectory parameters thereof by means of a navigation satellite system and/or by means of data of the navigation systems of the airplanes. After receiving said information, the trend in the change of the flight parameters between every airplane and all the other airplanes is calculated. All airplanes located in the air traffic control region are divided into three groups by a computer complex according to a required control probability. Said probability is equal to zero for the first group, is greater than zero but less than one for the second group and is equal to one for the third group. The airplanes of said groups and information associated therewith are displayed on an indicator screen by different colours. The co-ordinates and trajectory parameters for the third group of airplanes are defined at intervals which are equal or greater than 2 seconds, for the second group of airplanes at intervals which are by two times greater than for the third group and for the first group at intervals which are by four times greater than for the third group. The flight information processing and display are carried out only for the airplanes which are located at a distance equal to or less than 250 km. | ||||||
| 202 | 상용 이동 통신망을 이용한 소형 UAV 항공 교통 관제 시스템 | KR1020150060026 | 2015-04-28 | KR1020160128144A | 2016-11-07 | 김병수 |
| 본발명은상용이동통신망을이용한소형 UAV의항공교통관제시스템에관한것으로서, 더욱상세하게는상용이동통신사의 USIM 카드로식별코드가분류된소형 UAV의비행제어를위하여상용이동통신망기반의항공교통관제시스템을이용함으로써 ISM 대역폭무선주파수의제한점을극복하고저고도에서소형 UAV의안정적인통신및 통제를수행하는기술에관한것이다. 본발명에따른상용이동통신망을이용한소형 UAV 항공교통관제시스템은상용이동통신사의 USIM 카드로식별코드가분류되어있고상용통신모뎀이장착되어있는다수의소형 UAV; 다수의소형 UAV 콕핏부하단에각각장착되어항공영상을촬영및 저장할수 있는짐벌구조카메라; 상용이동통신서버와유/무선으로연결되어있고항공영상및 비행데이터를수신및 중계하는다수의상용이동통신기지국; 인터넷에상시연결되어데이터패킷교환이가능하고상용이동통신기지국이중계하는각종데이터를실시간수신및 저장하는상용이동통신서버; 다수의소형 UAV로통제명령프로토콜을전송하거나항공영상및 비행데이터를수신및 확인하는단말형태의소형 UAV 지상통제시스템; 다수의소형 UAV, 다수의상용이동통신기지국, 상용이동통신서버및 소형 UAV 지상통제시스템의전체시스템운영상황을통합적으로관제하여비행운용및 항공통제역할을수행하는소형 UAV 항공교통관제시스템;을구비하는것에특징이있다. | ||||||
| 203 | 항공관제 데이터를 이용한 관제오류 분석장치 | KR1020130102484 | 2013-08-28 | KR101410135B1 | 2014-06-23 | 이훈민 |
| According to present invention, a control error analyzing device using air control data includes a manipulating part receiving data and a manipulation command of a user, a communication part transceiving data with multiple air control centers and a display part, a storage part storing an execution program, and a data extracting program and a converting program for air control center analysis, and a control part controlling operation to analyze a state of control equipment and control work of a controller by air control center by reading the data extracting program and the converting program and the execution program stored in the storage part. The control part includes an air control data processing part receiving air control data recorded for a predetermined period from each air control center through the communication part to store the data in the storage part, an analysis data extracting part extracting analysis data by air control center by reading the air control data stored in the storage part, an analysis data converting part converting the extracted analysis data by air control center into a data format predetermined for each air control center to store the format in the storage part, and an analysis processing part storing evaluation result data in the storage part after evaluating the performance of control facility and an control error of the controller by comparing the analysis data by air control center to reference data by air control analysis item inputted by the user and using the comparison result. | ||||||
| 204 | 비행 전문 관리 방법 및 그 장치 | KR1020100104167 | 2010-10-25 | KR1020120042465A | 2012-05-03 | 오승희; 한종욱; 박효달; 이성현; 이덕규 |
| PURPOSE: A flight plan management apparatus and a method thereof are provided to increase internal efficiency of a system by distributing a flight plan through AFTN. CONSTITUTION: A flight plan classifying module(210) classifies a flight plan through an AFTN(Aeronautical Fixed Telecommunication Network). A flight plan generating module(220) generates the flight plan and adds distribution information to the generated flight plan. A flight message verifying module(230) detects error within the flight plan. A flight message distributing module(240) distributes the flight plan to the AFTN. | ||||||
| 205 | Air traffic control support device, air traffic control support method, and air traffic control support program | JP2010266942 | 2010-11-30 | JP2012118697A | 2012-06-21 | KIJIMA KENICHI; YOSHIMORI KO |
| PROBLEM TO BE SOLVED: To provide an air traffic control support device for enabling a user to reduce time and labor to create an avoidance plan and to quickly and reliably avoid occurrence of conflict.SOLUTION: An air traffic control support device 100 supports air traffic control and includes: an avoidance plan creation part 101 for creating avoiding procedure which shows a change of flight plan so as to avoid an occurrence of conflict and creating an avoidance plan comprising the created avoiding procedure if the occurrence of conflict between aircraft is detected based on flight plan information showing a flight plan of aircraft; and an avoidance plan output part 102 for outputting the created avoidance plan. | ||||||
| 206 | Air traffic control system, air traffic control information storage method and air traffic control information storage program | JP2007205157 | 2007-08-07 | JP2009042874A | 2009-02-26 | MIURA MITSUTAKA; YAMASHITA YOSHIHISA; KAWAMURA KENZO; NOGUCHI KAZUNOBU |
| PROBLEM TO BE SOLVED: To maintain consistency of airplane information stored by converting tables 160 among control devices 100 of an air traffic control system, and to quickly share correct information among the control devices 100. SOLUTION: This air traffic control system has an airplane information processing center device 200 managing to centralize the airplane information of all airplanes. The control device 100 control-processing the airplane can change only information (the airplane information) about the airplane, and the airplane information of the airplane not control-processed even by any control device 100 executes an exclusive control according to a characteristic of the air traffic control system which can be updated by only the airplane information processing center device 200. COPYRIGHT: (C)2009,JPO&INPIT | ||||||
| 207 | 航空管制支援装置、航空管制支援方法、及び、航空管制支援プログラム | JP2010266942 | 2010-11-30 | JP5645259B2 | 2014-12-24 | 憲一 木島; 香 吉森 |
| 208 | Air traffic control system and portable information terminal used in air traffic control system | JP2005180583 | 2005-06-21 | JP2007004253A | 2007-01-11 | FURUHATA TOMOKI; SHIOMI KAKUICHI; KANEDA NAOKI |
| PROBLEM TO BE SOLVED: To provide an air traffic control system making a portable information terminal display a screen similar to a control console, and capable of generating and issuing a control instruction from the portable information terminal, and to provide the portable information terminal used in the air traffic control system. SOLUTION: The control console 1 transmits information necessary to display various kinds of screens of the same contents as contents displayed on a control console display device 3 on the portable information terminal 10 side, from a wireless communication device 2C in response to request from the portable information terminal 10. When receiving control instruction transmission request including control instruction data to an airplane from the portable information terminal 10, the control console 1 transmits the control instruction data included in the request to the corresponding airplane. When the control instruction data is inputted on an input screen for inputting the control instruction to the airplane displayed on an information display part 10B, the portable information terminal 10 transmits the control instruction transmission request including the control instruction data to the control console 1 by a wireless communication device 10E to allow the control console 1 to transmit the control instruction to the corresponding airplane. COPYRIGHT: (C)2007,JPO&INPIT | ||||||
| 209 | Air traffic control instruction error correction system and air traffic control instruction error correction method | JP2002308780 | 2002-10-23 | JP2004145566A | 2004-05-20 | YOSHIDA HIROAKI |
| PROBLEM TO BE SOLVED: To provide an air traffic control instruction error correction system that improves safety of air traffic. SOLUTION: A data collation/warning device 7 can output warning information to a speaker 8 and an information display device 3 if air traffic control information acquired from an air traffic control information management device 2 carries no aircraft identifier uttered by a controller, to improve safety of air traffic. COPYRIGHT: (C)2004,JPO | ||||||
| 210 | 管制支援システム、管制支援方法および管制支援プログラム | PCT/JP2014/001795 | 2014-03-27 | WO2014156169A1 | 2014-10-02 | 寺本 幸生; 安藤 友人; 多賀戸 裕樹; 喜田 弘司 |
将来に渡る回避案の信頼性を管制官が理解しやすい態様で表示することができる管制支援システムを提供する。図形特定部７１は、注目機の区間情報と周辺機の区間情報との組毎に、注目機の区間情報によって表される３次元ベクトルを含みｘｙ平面に垂直な平面内で、周辺機により規定される所定範囲を表す図形を特定する。変換行列算出部７２は、注目機の通過点から次の通過点に向かうｘｙ平面内の２次元ベクトルをｘ軸に沿って順に並ぶように変換した場合における、２次元ベクトルを包含しｘｙ平面に垂直な平面からｘ軸および時間軸によって規定される平面への変換を表す変換行列を、２次元ベクトル毎に算出する。表示処理部７３は、図形を変換し、通過点および注目機が当該通過点を通過する時刻によって定まる点を結んだ線と、変換後の図形とを表示する。 |
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| 211 | Air-traffic control information processing system | JP2008234532 | 2008-09-12 | JP2010067136A | 2010-03-25 | YOSHII TSUYOSHI; KONO MITSURU |
| PROBLEM TO BE SOLVED: To provide an air-traffic control information processing system for reducing a burden on an air-traffic controller by reducing the number of aircraft to be controlled in an early stage. SOLUTION: An air-traffic control information processing system 1 includes:a route changing device 2 which acquires airframe information from each aircraft P existing in a control airspace Area, and predictively determines whether or not a plurality of aircraft P interfere with each other in the future when each aircraft P flies on a set route, and changes routes for the plurality of aircraft P when determining that the aircraft P interfere with each other. When a plurality of aircraft P do not belong to the same category, the route changing device 2 changes the routes so that the plurality of aircraft P can be prevented from interfering with each other, and when the plurality of aircraft P belong to the same category, associates the plurality of aircraft P with each other as group candidates, and changes the routes of the plurality of aircraft P so that they can be close to each other in a more early stage. COPYRIGHT: (C)2010,JPO&INPIT | ||||||
| 212 | Air traffic control training support apparatus | JP23837597 | 1997-09-03 | JPH1185002A | 1999-03-30 | TSUNODA NAOYUKI; SAKAMOTO TEIJIRO |
| PROBLEM TO BE SOLVED: To make it possible to automatically discriminate and display the signal of a pseudo target and the signal of a real target by comparing the relative speed calculated from the Doppler frequencies of a pulse compressed reception signal with the relative speed calculated from target motion. SOLUTION: An expanded pulse generator 3 modulates the pseudo target signal and the real target signal to expanded pulse in such a manner that pulse compression may be executed at the time of signal reception. A pulse compression signal processor 4 subjects the pseudo target and the real target signal inputted from an antenna 6 to pulse compression. A Doppler detector 11 detects Doppler frequencies from the pulse compressed signals. A speed calculator 12 calculates the relative speed of the target from the Doppler frequencies. A decision apparatus 13 decides that the target is the pseudo target from the calculated relative speed which is below the specified value. As a result, manipulated variable is lessened as compared with the decision of the pseudo target and the manual impartation of the attribute and the reliability of the monitor of the real target during training may be improved. | ||||||
| 213 | Air traffic control system and control panel for control desk | JP2013037747 | 2013-02-27 | JP2014164703A | 2014-09-08 | SATO KENJI; YAMAUCHI MANABU; YAMAMURO HITOMI |
| PROBLEM TO BE SOLVED: To improve the operability of a control desk so as to reduce burden in air traffic control operations.SOLUTION: The air traffic control system includes touch operation devices 12-1 to 12-4 with an operation display switching part for displaying multiple buttons indicating respective multiple communication lines for air traffic control by dividing them into multiple blocks and receiving a selection operation per block and an operation display part for displaying in a depressible manner each of multiple buttons included in a block selected by the operation display switching part, and transfer units 11-1 to 11-4 each of which transfers data via a communication line corresponding to a button on the operation display part when the button is depressed. | ||||||
| 214 | Information processor used for air traffic control system | JP2005266943 | 2005-09-14 | JP2007079938A | 2007-03-29 | YAMADA TATSURO; TAGUCHI JITSUO |
| <P>PROBLEM TO BE SOLVED: To continue alarm monitoring using a simple method for outputting alarm, even if the state goes into one where the alarm output by an original system is disabled. <P>SOLUTION: This information processor 14 is provided with a radar information acquisition part 21 for acquiring radar information from a radar device 10. A control part 20 makes a display device 37 display positions of an aircraft and an object having possibility of collision against the aircraft through a display control part 35, on the basis of the radar information acquired by the radar information acquisition part 21. A collision decision processing part 24 decides the possibility of collision of the airplane against the object, on the basis of whether the positions of the object and the aircraft displayed by the control part 20 overlap. The control part 20 outputs an alarm, when the collision decision processing part 24 decides that there is a possibility of collision. <P>COPYRIGHT: (C)2007,JPO&INPIT | ||||||
| 215 | Air traffic control information display method and its device | JP33239199 | 1999-11-24 | JP2001148100A | 2001-05-29 | NAKAO TAKETOSHI |
| PROBLEM TO BE SOLVED: To make easily and surely graspable control information on aircraft. SOLUTION: This device is provided with a control information storage part 21 to store information, an update processing part 22 to update the control information of the aircraft from a radar part 40 and to store it in the control information storage part 21, a display control part 23 to read the information and to control a display screen device 31 so as to display plural target symbols to indicate the positions and traveling directions of the respective aircrafts, to display data blocks to indicate a specified information at specified positions in the vicinity of the display positions of the respective target symbols and to display a reader line to connect the target symbols and the data blocks and is constituted so that the display control part 23 is actuated according to positional information of the transfer destination to be inputted from a pointing device 32 and pieces of the control information (data blocks) regarding the aircraft are transferred and displayed at the specified position of a display screen 31A. | ||||||
| 216 | Air-traffic control training supporting device | JP6070297 | 1997-03-14 | JPH10254346A | 1998-09-25 | TSUNODA NAOYUKI; HIWATARI KOSUKE |
| PROBLEM TO BE SOLVED: To make it possible to automatically separate a flight path of a real target from that of a virtual target and display them by controlling fight path information, which are correlated with various factors of a virtual target and are in a one-to-one correspondence therewith, as flight information and outputting them to a display device. SOLUTION: Based on the detected data from a target observation device 1 and various factors of a virtual target set by a training scenario generating device 2 and transferred from a target factors transfer device 3, a smoothed vector calculated by a target tracking device 4 is held as flight path information. A time corrector 6 operates time correction of the flight information and the virtual target factors, and a correlation unit 7 by a fixed correlation fate operates a correlation processing between the time-matched flight path and virtual target factors, and a one-to-one corresponding judging unit 9 judges whether or not a correlation result of the flight path and the virtual target factors are in a one-to-one correspondence. And if they are in an one-to-one correspondence, an attribute is updated according to whether of not they are the flight path and virtual targets in a target control database 15, and the updated flight path and attribute are displayed on a display device 16. | ||||||
| 217 | Integrated display device for air traffic control information | JP7794095 | 1995-04-03 | JPH08273099A | 1996-10-18 | SATO HIROYOSHI; YAMAZAKI SHUNICHI |
| PURPOSE: To provide the integrated air traffic control information display device with configuration for integrally displaying plural kinds of information required for the execution of an air traffic control job and centralizing an information input environment. CONSTITUTION: This device is provided with a map information storage means 10 for storing air area map information (information required for map formation) in order to integrally display the information concerning a control object airplane inputted from other control information processing system or an input device 2 on a display device 3, position information display control means 11 for displaying an airplane identification image moving on a display map, operation schedule information display control means 12 for displaying the operation schedule information of the airplane, flight schedule information display control means 13 for displaying the flight schedule information concerning the selected airplane, and control instruction information input/display control means 14 for displaying the contents, etc., of control instruction to the airplane. | ||||||
| 218 | Vehicular unit for atc device | JP340381 | 1981-01-13 | JPS57116501A | 1982-07-20 | KATOU MASAKAZU; WATANABE SHIYOUICHI |
| PURPOSE: To enable an ATC system to operate even in a no signal zone by inserting an emergency operation switch operating circuit to the pressure line of an ATC defect detector and the resetting circuit of a defect holding relay. CONSTITUTION: When a train approaches a ground non signal zone so that no presence detector 4 detects no signal, a holding relay 8 operates to operate an emergency brake. When an emergency operation switch 10 is closed, an emergency operation relay 11 will operate. Thus, the relay 8 is reset by the contact 11b of the relay 11, and the pressure line of a defect detector A is disconnected via the contact 11a of the relay 11. Then, the train becomes possible to run in a no signal zone. When the switch 10 is opened, the pressure line of the detector A is again connected. In this manner, a normal operation having a normal ATC defect detecting function becomes possible. COPYRIGHT: (C)1982,JPO&Japio | ||||||
| 219 | 航空管制用通信システム及びゲートウェイ装置 | JP2012179560 | 2012-08-13 | JP5949309B2 | 2016-07-06 | 田濃 邦彦; 西貝 公男; 加藤 禎久; 堀越 貴之 |
| 220 | 航空管制システム及び管制卓用操作パネル | JP2013037747 | 2013-02-27 | JP5909452B2 | 2016-04-26 | 佐藤 健司; 山内 学; 山室 仁美 |
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