空中交通管制相关的专利数据

序号	专利名	申请号	申请日	公开（公告）号	公开（公告）日	发明人
161	항공 관제 시스템	KR1020027002425	2000-08-24	KR1020020060165A	2002-07-16	배런,댄
본 발명은 과도한 수의 발못된 경고를 제공하지 않는 기동중인 항공기 사이의 저촉을 예측하기 위한 장치 및 기술에 관한 것이다. 이러한 기술은 실제와 가장 유사하게 예측이 이루어지도록 저촉 예측동안의 시간 구간을 제한하는 정보를 이용한다.
162	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.
163	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

164	Air traffic control system	JP2006312988	2006-11-20	JP2008128777A	2008-06-05	NOMOTO TAKASHI
<P>PROBLEM TO BE SOLVED: To provide a display system for air traffic control capable of performing PPI display for air traffic control only by a tracking radar, even when such a regulation allowing only the tracking radar to be placed on a platform is present. <P>SOLUTION: In this system equipped with the tracking radar 10 whose space scanning system is random, and a time matching processing means 20 for calculating a predicted position of an object target in accordance with a display updating period of a PPI display device based on a positioning time and position information of the object target detected by the tracking radar, a relative position of the object target is displayed on the PPI display device 40. <P>COPYRIGHT: (C)2008,JPO&INPIT
165	Air traffic control system	JP2001225160	2001-06-21	JP2003006798A	2003-01-10	OKADA MOTOHIRO
PROBLEM TO BE SOLVED: To improve the safety and reliability of air traffic control. SOLUTION: By two-dimensionally or one-dimensionally controlling an air craft course operating in a three-dimensional space, erroneous control in manual control is reduced and monitoring work is divided to make it easy even when a person is in charge of monitoring as the result of automating main control. COPYRIGHT: (C)2003,JPO
166	Air traffic control system	JP2003185414	2003-06-27	JP2005018619A	2005-01-20	KOSEKI KEIJIRO
<P>PROBLEM TO BE SOLVED: To improve the reliability of communication while reducing an air traffic controller's burden. <P>SOLUTION: A radar processing part 20 displays a flying body (aircraft) caught by a radar antenna 10 on a radar screen by a display part 22. When a certain aircraft is selected in the radar screen through an input part 24, a line construction part 28 determines a ground transmitting and receiving station 16 the communication area of which includes the position of the selected aircraft, and constructs a communication line with the ground transmitting and receiving station 16 by an air radio exchange part 14. <P>COPYRIGHT: (C)2005,JPO&NCIPI
167	Air traffic control system	JP2003176038	2003-06-20	JP2005011160A	2005-01-13	HAYASHI YOSHIHIKO; MAEKAWA RYOJI; KENMOCHI YUKIHIKO
<P>PROBLEM TO BE SOLVED: To provide rapid and more reliable control information to an air traffic controller. <P>SOLUTION: This air traffic control system has: a signal processing part detecting position information about a target object from observation data observed by an observation means; a first following processing part inputted with the position information about the target object in each observation period, detected by the signal processing part, and performing a following process about the target object from the latest position information about the target object and the position information about the target object which has been detected last time; and a second following processing part inputted with the position information about the target object in each observation period, and performing a following process about the target object from the latest position information about the target object and a plurality of pieces of position information about the target object, detected in the past. A processing result of the first following processing part is displayed on a display part, while a processing result of the second following processing part is inputted to the first following processing part to correct the processing result of the first following processing part by the processing result. <P>COPYRIGHT: (C)2005,JPO&NCIPI
168	Air traffic control system	US22046262	1962-08-30	US3178704A	1965-04-13	CURTIS MOORE LEONARD; JOSEPH KENNEALLY PATRICK

169	Apparatus for air traffic control	US83796459	1959-09-03	US3113292A	1963-12-03	ERIC PARKER

170	Air traffic control system	US9390049	1949-05-18	US2515633A	1950-07-18	COLEY NELSON B

171	Air traffic control apparatus and air traffic control information processing method	US12381010	2009-03-05	US20100153875A1	2010-06-17	Mark James O'Flynn; Virginie Bernard Blond
An air traffic control apparatus comprises a display device for graphically displaying air traffic control information and items of anticipated event information about air traffic; a memory device for storing data and instructions for operating the apparatus; and a processor coupled to the display device and the memory device. The processor causes the display device to display the items of anticipated event information, a time-line and an indication of current time on said time-line in an agenda window. The items of anticipated event information include anticipated time information. The items of anticipated event information are arranged against the time-line in accordance with the anticipated time information of the items of anticipated event information. A section of said time-line includes the current time and a specific period of time in future in relation to the current time. The items of anticipated event information corresponding to the section of the time-line are displayed in the agenda window.
172	AIR TRAFFIC CONTROL METHOD	US13241189	2011-09-22	US20120010763A1	2012-01-12	William L. Goodman; Syed T. Shafaat; John A. Brown; Jennifer L. Gertley; Robert P. Smith
A method of operating an air traffic control system may include receiving, by a control system, an instruction from a control system user. The method may further include providing, by the control system, the instruction to an airplane via a data link between the control system and a system of the airplane. In addition, the method may include adjusting, by the airplane system, at least one airplane control to correspond to the instruction.
173	Air traffic control systems	US3742503D	1971-05-19	US3742503A	1973-06-26	STRATTON A
An air traffic headway control system comprises a ground transmitter located en route and a receiver in each aircraft. The transmitter transmits cyclic sequences of distinctive signals whose timing is controlled by a highly stable master oscillator. These are received in the aircraft which also has a stable oscillator synchronized to the master oscillator of the transmitter. Reference pulses which are timed with respect to the stable oscillator are generated in the receiver and a comparison is made between the timing of the reference pulses and the time of reception of the sequences of distinctive signals to provide an indication of the position of the aircraft in the lane. A perturbation is applied to the timing of the beginning of each sequence which represents the desired motion of the aircraft. The receiver also includes means for controlling the speed of the aircraft in accordance with its indicated position so as to maintain or correct its position. The means for making the comparison in timing preferably includes a correlation detector.
174	Air traffic control system	US4649060	1960-08-01	US3136991A	1964-06-09	DE FAYMOREAU ETIENNE C L; BAUDIN JEAN A

175	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.
176	航空管制システム	JP2011112292	2011-05-19	JP5659082B2	2015-01-28	アロン，ヤイル

177	Air traffic control system	JP2001225159	2001-06-21	JP2003006800A	2003-01-10	OKADA MOTOHIRO
PROBLEM TO BE SOLVED: To improve the safety and reliability of air traffic control. SOLUTION: The predictive altitudes of two air crafts approaching the intersection nearly simultaneously on a top view at an intersection or a predictive altitude difference between both of the air crafts is predicted and displayed by a computer. COPYRIGHT: (C)2003,JPO
178	Air traffic control method	US13241189	2011-09-22	US08417396B2	2013-04-09	William L. Goodman; Syed T. Shafaat; John A. Brown; Jennifer L. Gertley; Robert P. Smith
A method of operating an air traffic control system may include receiving, by a control system, an instruction from a control system user. The method may further include providing, by the control system, the instruction to an airplane via a data link between the control system and a system of the airplane. In addition, the method may include adjusting, by the airplane system, at least one airplane control to correspond to the instruction.
179	Method for controlling air traffic	US12008999	2008-01-17	US20090187332A1	2009-07-23	Joshua Popik Glucoft
A method is disclosed for controlling the traffic of flying vehicles. More specifically, a method using a one-to-one function is described that can assign one and only one elevation of travel to each allowable desired direction of travel.
180	Air-traffic regulating systems	US3775767D	1972-01-17	US3775767A	1973-11-27	FIELDING J
An improved position-prediction method and subsystem to permit better ground prediction of aircraft future position is disclosed. It is proposed for use in air traffic control systems which offer an IPC (intermittent positive control) service to all VER aircraft which carry the not yet standardized DABS beacon (a planned discretely-addressable variant of present radar-response beacons which is to include automatic reception and display of ground-to-air commands). Disclosure proposes that this planned new beacon should include modest cost means to report turn rate periodically and that a string of successive radar fixes be data processed with a corresponding string of such turn rate reports to derive aircraft ''''flight-headings'''' which are both accurate (due to averaging many noisy radar fixes over many seconds of time) and very current by virtue of the turn rate reports which effectively remove the long lag resulting from such averaging. The disclosure shows five different methods and means to process such data so as to derive accurate current ''''flight-headings'''' and to predict future positions based thereon.

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