| 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 | COMPUTER BASED TEACHING SYSTEM FOR AIR TRAFFIC CONTROL TRAINING | PCT/AU2007/000908 | 2007-06-29 | WO2009003210A1 | 2009-01-08 | ROWLAND, Ainslie; ROWLAND, Michael |
A computer based teaching system for teaching a air traffic controller skills comprises: a plurality of lesson sections, each for presenting to a student, via a computer, theory underlying one or more skills required for competent air traffic control; and a plurality of exercise sections, each for providing, via a computer, an exercise in the form of an interactive scenario on a simulated air traffic control system, using which a student may practice air traffic control skills. The system preferably comprises a number of units useable sequentially in a predetermined order to sequentially teach to a student a plurality of air traffic control skills, which together comprise at least a subset of the skills required of an air traffic controller. |
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| 202 | Method and apparatus for avionics management | US723601 | 1996-10-01 | US5844503A | 1998-12-01 | Victor A. Riley; Robert E. Demers |
| A method and apparatus using a simplified language consistent with air traffic control syntax for inputting, displaying and controlling the operation of a flight management system of an aircraft to comply with the instructions received by the pilot from the air traffic controller. | ||||||
| 203 | 一种新型PTT信号延时控制器 | CN201520434329.9 | 2015-06-23 | CN204695026U | 2015-10-07 | 崔绍恒 |
| 本实用新型公开了一种新型PTT信号延时控制器，包括6V～24V双直流供电电源、输入端口、PTT信号通道、延时输入模块、延时控制模块、延时电子器件、输出端口和其他信号通道，所述输入端口与所述延时控制模块通过PTT信号通道连接，所述延时控制模块与所述延时电子器件连接并控制所述延时电子器件工作，所述延时电子器件输出端连接输出端口，所述输入端口还通过所述其他信号通道直接与所述输出端口直接连接；所述延时输入模块输出端口与所述延时控制模块连接；所述延时输入模块包括触摸屏；所述输入端口和所述输出端口采用RJ45串口。本实用新型对FA36网络中PTT信号进行消除“尾音”处理，优化内话系统的管制席位及录音系统环境，有效提高管制员的正常空中交通指挥工作质量；“尾音”处理时间可以设置，适用于不同距离的VHF台站，适用性广；结构简单，操作简易，电源稳定，成本低。 | ||||||
| 204 | Airport control support system | JP2002122175 | 2002-04-24 | JP2003317200A | 2003-11-07 | TANIMOTO TOMOHIKO; GOTO HIDENORI |
| PROBLEM TO BE SOLVED: To provide an airport control support system which supports ground travel control operation by an air-traffic controller without lowering the operation efficiency of an airport even in congestion and low visibility states. SOLUTION: The behavior of each moving body is predicted by detecting the position of a moving body traveling on each path of the airport, specifying an object to be detected, and calculating the moving speed and so on, and a travelable section of a moving body to be controlled is predicted from the behavior of other moving bodies; and the path of the moving body to be controlled is determined by taking them into consideration and provided for the air-traffic controller, so the burden on the air-traffic controller is lightened and a proper path can easily be provided. COPYRIGHT: (C)2004,JPO | ||||||
| 205 | Control data display system | JP32959991 | 1991-11-18 | JPH05143900A | 1993-06-11 | SASAMOTO YASUYUKI |
| PURPOSE: To improve the certainty of a judgement and a control indication by an air traffic controller by enabling the air traffic controller to accurately and easily grasp the operation state of aircrafts to be controlled. CONSTITUTION: A time search processing means 11 calculates the current position and control interval of the aircraft to be controlled according to a flight schedule data file 4 generated by a file generating means 10 and the current time. A control data display means 12 displays information showing the current position of the object aircraft and control interval and control data including the current time and map information on the display on a control display device 2. An abnormal approach warning function 13 outputs a warning of a deficiency in the control interval of the object aircraft according to the reference of the flight schedule data file 4. A simulation function 14 displays the simulation position of the object aircraft. A figure drawing function 15 draws a free figure based upon the indication of the air traffic controller on the screen on the control display device 2. COPYRIGHT: (C)1993,JPO&Japio | ||||||
| 206 | 항공교통감시및통신시스템 | KR1019960704257 | 1995-02-03 | KR100408159B1 | 2004-03-30 | 레오나드쉬흐먼; 로널드브루노; 존케팔리오티스; 스티브그린버그; 에드워드제이.제크재워스키 |
| An air traffic surveillance and communication system for air traffic controllers, includes a plurality of ground based first radio transceivers located in specific geographic sectors, respectively, and having a first frequency channel for supporting party-line digital voice and a second frequency channel dedicated to supporting a digital data channel for down-linking dependent surveillance data and for both up-link and down-link data communications. The first and second frequency channels are paired such that each time a frequency change is commanded by the ground both the first and second frequency channels will be automatically tuned to a new air-ground frequency paid. The system also includes a plurality of aircraft based second digital radio transceivers, one located in each aircraft. Each second radio transceiver has corresponding first and second frequency channels and a navigational data source on each aircraft. The navigational data source incorporates triply redundant GPS receivers for producing highly accurate aircraft navigation data selected from aircraft latitude, longitude, altitude, speed, heading and glide data which is coupled to the respective aircraft transceiver for transmission on said second channel to at least one of the plurality of ground based first radio transceivers. Each ground based first radio transceiver has a communication controller for formatting up-link data and separating down-linked surveillance data and disseminating same to air traffic controllers in the sectors of said aircraft. In a preferred embodiment, in a TDMA format with digital radio transceiver operates with a 12.5 kHz spacing, differential QPSK signal modulation is used and each broadcast is by short transmission bursts having a guard band signal preamble and a management/user data field. | ||||||
| 207 | Altitude warning device for aircraft | JP29537795 | 1995-11-14 | JPH09138900A | 1997-05-27 | NEMOTO SHIGERU |
| PROBLEM TO BE SOLVED: To reduce the burden of an air traffic controller by suppressing the generation of unnecessary warning by an aircraft in the neighborhood of a lowest guiding altitude. SOLUTION: An altitude filter circuit S2 extracts an objective aircraft in the neighborhood of a lowest guiding altitude based on information of an MVA storing circuit S1 storing the lowest guiding altitude (MVA), and an altitude changing rate extraction circuit S6 extracts the altitude changing rate of the objective aircraft based on information of an altitude changing pattern storing circuit S5. Whether the flight of the aircraft in the neighborhood of MVA satisfies or not the regulation of instrument flight is judged by these. When it satisfies, the altitude change is judged to be one instructed by an air traffic controller so that warning is not generated. On the other hand when it does not satisfy, the altitude change is recognized to be one without instruction so that warning is generated. Thereby warning generated at the time of changing an altitude to the neiborhood of MVA with the instruction of the air traffic controller is suppressed. COPYRIGHT: (C)1997,JPO | ||||||
| 208 | Air traffic control auxiliary system and air traffic control auxiliary method | JP2012045759 | 2012-03-01 | JP2013182411A | 2013-09-12 | ITAKURA KUNIMASA; AKAMATSU MANABU |
| PROBLEM TO BE SOLVED: To provide an air traffic control auxiliary system and an air traffic control auxiliary method capable of presenting new information for assisting air traffic control to an air traffic controller.SOLUTION: An air traffic control auxiliary system 10 of the present invention comprises: detection means 20 that acquires detection information including a position and travelling direction of an aircraft; storage means 30 in which topographic information is stored; calculation means 40 that extracts the topographic information corresponding to the acquired detection information from the storage means, arranges the extracted topographic information and the acquired position of the aircraft in a virtual three-dimensional space, and calculates a visual field when seeing the travelling direction from the position of the aircraft and outputs the visual field as visual field information; and display means 50 that displays the outputted visual field information. | ||||||
| 209 | ENHANCED SYSTEM AND METHOD FOR AIR TRAFFIC CONTROL | PCT/US2007/062036 | 2007-02-13 | WO2007098329A1 | 2007-08-30 | JUDD, Thomas D. |
A system and method for engaging in two-way communication between a pilot and an air traffic controller by speech and hearing processes wherein spoken messages are compared to a database of categorized messages for matching and selecting a categorized message for transmission between pilot and air traffic control. |
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| 210 | Air traffic control system | US3623090D | 1968-11-15 | US3623090A | 1971-11-23 | GILBERT GLEN A; HOBBS JAMES |
| An aircraft traffic control system which has a first portion that allows aircraft to detect other aircraft in their vicinity so that they are aware of them and which also allows an aircraft to maintain a particular spacing with respect to a selected aircraft to alleviate the load on the ground air traffic controllers, is disclosed. The identification, altitude and coordinates of an aircraft is transmitted and received by other aircraft and/or by ground stations to allow other aircraft to be aware of the position of traffic, and the ground stations may utilize the information for local and en route control so that monitoring and control of all aircraft may be maintained throughout the system. Various instrumentations and implementations are disclosed which allow existing facilities to be used with modifications which are simple and relatively inexpensive.
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| 211 | Aircraft traffic separation maintaining system | JP2012162792 | 2012-07-23 | JP2013033474A | 2013-02-14 | BUSHNELL GLENN SCOTT |
| PROBLEM TO BE SOLVED: To provide a method and an apparatus for maintaining a desired level of separation between aircrafts, taking into account various factors that may affect much labor and cost, the ability of the pilot of an aircraft, and the ability of human air traffic controllers required for air traffic control.SOLUTION: A closest point of approach 310 between a first vehicle 302 traveling along a first path 306 and a second vehicle 304 traveling along a second path 308 is predicted. A plurality of compensation commands for altering the first path of the first vehicle are generated using the closest point of approach and a desired level of separation between the first vehicle and the second vehicle. The plurality of compensation commands are integrated with a plurality of control commands for the first vehicle to form a plurality of final control commands configured to maneuver the first vehicle to substantially maintain the desired level of separation between the first vehicle and the second vehicle. A response of the first vehicle to the plurality of final control commands is a desired response. | ||||||
| 212 | Expert system for air traffic control and controller training | US931867 | 1986-11-18 | US4827418A | 1989-05-02 | Arthur Gerstenfeld |
| A expert system form of artificial intelligence for control of air traffic which may also be utilized for air traffic controller training. The expert system receives input data representing the altitude and heading of all aircraft in the control area. The aircraft data is compared with the data of the other aircraft. Sequencing and local flow control is optimized and if a potential conflict arises between two aircraft, clearances are transmitted to the aircraft to resolve the conflict. The aircraft data is also compared with a knowledge base of air traffic control rules for the particular airport involved. An inference engine written in LISP (or another AI language) allows real time access to the knowledge base. The position and heading of each aircraft is monitored and controlled until turned over to the tower for final approach. The expert system may also be used for air traffic controller training and be used as a intelligent tutor. The air traffic controller trainee's clearances are input and compared to those generated by the system. If the trainee's clearances are in error, or can be improved, the expert system prompts the trainee and coaches him in a way so that he learns from his past errors. | ||||||
| 213 | AIRPLANE DISTRESS SYSTEM | PCT/US2002/029658 | 2002-09-20 | WO2003024187A2 | 2003-03-27 | UNDERSTEIN, Norman |
An airline distress system is provided for an airplane. The airplane includes a pilot cockpit and a transponder for transmitting signals to an air traffic controller. The airline distress system includes an auxiliary transponder that transmits auxiliary signals to the air traffic controller. The auxiliary transponder is preferably disposed outside of the pilot cockpit and inaccessible to airplane crew and passengers. In one embodiment, a sensor is operatively coupled with the cockpit door, and a switch communicates with the sensor and the auxiliary transponder. The auxiliary transponder is configured to be automatically activated by the switch according to a signal from the sensor that the cockpit door has been opened. |
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| 214 | SCHEDULE MANAGEMENT SYSTEM AND METHOD FOR MANAGING AIR TRAFFIC | PCT/US2013/045655 | 2013-06-13 | WO2014004101A1 | 2014-01-03 | SUBBU, Rajesh, Venkat; CHAN, David, So Keung; BROOKSBY, Glen, William; KLOOSTER, Joel, Kenneth; TORRES, Sergio |
A system and method to improve efficiency in aircraft maneuvers meant to accommodate time-related constraints in air traffic, information related to flight performance and atmospheric conditions is gathered onboard an aircraft, then transmitted to an air traffic control center, in the event of a delay or any other event which necessitates an alteration in an aircraft trajectory, the data is sent to a decision support tool to compute and provide alternative trajectories, preferably including operator- preferred trajectories, within air traffic constraints. Air traffic controllers can then offer an alternative trajectory to an aircraft that is more efficient, cost effective, and/or preferable to the aircraft operator. |
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| 215 | Stereoscopic 3-D Presentation for Air Traffic Control Digital Radar Displays | US14186040 | 2014-02-21 | US20140306950A1 | 2014-10-16 | Jason G. Russi; Brent T. Langhals; Michael E. Miller; Eric L. Heft |
| An apparatus and method of presenting air traffic data to an air traffic controller are provided. Air traffic data including a two dimensional spatial location and altitude for a plurality of aircraft is received. A disparity value is determined based on the altitude for each aircraft of the plurality of aircraft. Left and right eye images are generated of the plurality of aircraft where at least one of the left and right eye images is based on the determined disparity value. The left and right eye images are simultaneously displayed to the air traffic controller on a display. The simultaneously displayed images provide an apparent three-dimensional separation of each of the aircraft of the plurality of aircraft on the display. | ||||||
| 216 | Air traffic voice interactive simulator | US259831 | 1999-03-01 | US5961331A | 1999-10-05 | Gregory Fisch |
| A computerized air traffic voice interactive simulator is provided for simulating the communications between a pilot and an air traffic controller. The air traffic voice interactive simulator includes an audio input means, central processing unit and audio input means. The central processing unit interprets and evaluates verbal responses received from a user through the audio input means for selecting an appropriate audio message for production on the audio output means. The audio messages are selected to provide feedback and interactive communication with a user so as to simulate dialog between a pilot and air traffic controller. | ||||||
| 217 | SYSTEMS AND METHODS FOR CONTEXT BASED CPDLC | EP15177591.3 | 2015-07-20 | EP2980773A1 | 2016-02-03 | KUMAR, Rakesh; DOMINIC, Maria John Paul; PANDEY, Vivek Kumar; KOMMURI, Siva; GANDHI, Darshan |
Systems and methods for context based controller pilot data link communication (CPDLC) are provided. In certain implementations, a method for CPDLC includes receiving data through the selection of a selectable item on a pilot interface, wherein the pilot interface is a a non-CPDLC interface and communicating the data to a CPDLC application. Further, the method also includes constructing a CPDLC message based on the data; and transmitting the CPDLC message to an air traffic controller.
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| 218 | Method and apparatus for heads-up critical information display on air traffic control tower glass window walls | US11476677 | 2006-06-29 | US20070100499A1 | 2007-05-03 | Kathy Staub |
| A heads-up display system that can be configured to display critical information on the glass window wall in an air traffic control tower cab so an air traffic controller can view the information without taking his or her eyes off the runways or movement areas. Multiple input devices communicate critical information to a computer's central processing unit which processes the information, creates a display, and sends it to a display device. The display device creates a substantially transparent image of the critical information on the window wall of an air traffic control tower. | ||||||
| 219 | Electronic flight data strips and method for air traffic control | US30126 | 1998-02-25 | US6131065A | 2000-10-10 | John A. Marszalek |
| A portable, re-usable, battery-powered, electronic device for storing, displaying and modifying air traffic control information. The electronic flight data strip receives input data from an external data source via infrared or radio transmission, stores the data in an on-board memory device, displays selected portions of the received data for viewing by an air traffic controller, and receives and displays inputs from the air traffic controller either directly through integral switches or via aforesaid communications channels. All input and output data messages and air traffic controller commands may be stored and time tagged for later retrieval. The contents of the stored memory can also be interrogated and modified by external data processing devices. Following completion of the flight, the contents of the internal memory can be interrogated for the purpose of archiving or investigation and/or cleared for subsequent re-use on another flight. | ||||||
| 220 | Multi-use bearing and range line | US12381011 | 2009-03-05 | US07868813B2 | 2011-01-11 | Mark James O'Flynn; Lillian Chang; Virginie Bernard Blond |
| A method (400), a system and a computer program product are disclosed for graphically displaying air traffic control information in an air traffic control system. Information about objects in an air traffic control environment is compiled and calculated (410). Tokens (e.g., text, icons, images, or other symbols) corresponding to the objects in the air traffic control environment are displayed (420). At least two objects are selectively designated (430) in combination as a source object and a target object connected by a bearing and range line token (210, 220, 230, 240). Air traffic control information (212, 222, 232, 242) about the combination of objects associated with the bearing and range line token dependent upon the combination of objects designated in the combination is displayed (440). The displayed air traffic control information is required decision making information to enable an air traffic controller to manage air traffic. Display of the air traffic management information is dynamically updated (450) upon any change of the designated objects. | ||||||
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