公开(公告)号：WO1995003598A1

公开(公告)日：1995-02-02

申请号：PCT/GB1994001512

申请日：1994-07-13

Applicant: WESBY, Philip, Bernard

IPC: G08G05/04

CPC classification number: G08G5/0013 ,  G08G3/02 ,  G08G5/0052 ,  G08G5/0082

Abstract: An earth based locating and map dissemination system wherein the locations of mobile objects in a monitored area are identified and then broadcast throughout the monitored area. Each mobile object being tracked in the monitored area carries a unique ID code device. A master ground station in a monitored area contains apparatus for paging each of the unique ID codes in the given area. The positions of each of the mobile objects carrying a unique ID code device may be determined by a bearing determination or a time delay determination based on the response to the paged signal. Alternatively, the page signal response may include the location coordinates of the mobile object as determined by a navigational system carried by the mobile object. The master ground station collects the position information for all of the mobile objects in the given area and then transmits those positions in a file throughout the given area. The position file information is coordinate encoded so that it may be superposed on a map of the area. In addition to the position files, the master ground station can transmit reference information that is also coordinate encoded. Further in addition to the position file, velocities of the mobile objects can be determined and distributed along with as predicted positions of the mobile objects based on their present position and velocity.

Abstract translation: 一种基于地球的定位和地图传播系统，其中识别被监测区域中的移动对象的位置，然后在整个监视区域广播。 在被监视区域中跟踪的每个移动对象携带唯一的ID码设备。 受监控区域中的主地面站包含用于在给定区域中寻呼每个唯一ID码的装置。 携带唯一ID码装置的每个移动对象的位置可以通过基于对寻呼信号的响应的方位确定或时间延迟确定来确定。 或者，页面信号响应可以包括由移动对象承载的导航系统确定的移动对象的位置坐标。 主地面站收集给定区域内的所有移动物体的位置信息，然后在整个给定区域的文件中传送这些位置。 位置文件信息被协调编码，使得它可以叠加在该区域的地图上。 除了位置文件之外，主地面站还可以发送也被协调编码的参考信息。 此外，除了位置文件之外，可以基于其当前位置和速度，根据移动对象的预测位置来确定和分发移动对象的速度和分布。

公开(公告)号：WO1990001202A1

公开(公告)日：1990-02-08

申请号：PCT/AU1989000321

申请日：1989-07-28

Applicant: DUNLAVY, John, Harold ,  LANE, Richard

IPC: G08G05/04

CPC classification number: G08G5/0008 ,  G01S13/9303 ,  G08G5/045

Abstract: A collision avoidance arrangement where aircraft transmits and receives radio signals modulated by a digital pulse sequence (34), if a potential collision is detected (35) the arrangement is adapted to transmit and receive interrogation radio signals and from these signals each aircraft estimates the closing speed of the aircraft (36) and then determines the range between the aircraft (37), and the arrangement also being adapted such that each aircraft transmits to the other the estimate of the closing speed calculated aboard the aircraft and then averages the estimates of the closing speed from each aircraft to obtain a more accurate value for the closing speed of the aircraft.

Abstract translation: 一种碰撞避免装置，其中飞机发射和接收由数字脉冲序列（34）调制的无线电信号，如果检测到潜在的冲突（35），该装置适于发送和接收询问无线电信号，并且从这些信号中，每个飞机估计关闭 飞机（36）的速度，然后确定飞行器（37）之间的范围，并且该装置也被适配成使得每个飞机向另一飞行器传送在飞机上计算的关闭速度的估计，然后平均估计 从每架飞机的关闭速度获得更准确的飞机关闭速度值。

公开(公告)号：WO1992005529A1

公开(公告)日：1992-04-02

申请号：PCT/EP1991001733

申请日：1991-09-12

Applicant: HELLA KG HUECK & CO. ,  SCHULTE, Peter ,  SCHMEES, Siegfried

Inventor： HELLA KG HUECK & CO.

IPC: G08G05/04

CPC classification number: G08G5/0026 ,  A01M29/06 ,  B64D47/06 ,  G08G5/0065 ,  G08G5/025

Abstract: In order to increase the effective warning, the locatability and hence the safety in the operation of aircraft in a process and device for preventing aircraft collisions in which a light flash warning device on the aircraft which has at least one light source generates periodic flashes, a first light source emits flashes at a constant frequency and a second emits flashes with a variable frequency.

公开(公告)号：WO1986002761A1

公开(公告)日：1986-05-09

申请号：PCT/JP1985000579

申请日：1985-10-17

Applicant: TOYO COMMUNICATION EQUIPMENT CO., LTD. ,  FUNATSU, Chuhei ,  KITA, Kazuyuki

Inventor： TOYO COMMUNICATION EQUIPMENT CO., LTD.

IPC: G08G05/04

CPC classification number: G08G5/0008 ,  G01S7/066 ,  G01S13/9303 ,  G08G5/0021 ,  G08G5/0052 ,  G08G5/0078

Abstract: A system for displaying a warning zone or menacing aircraft in an apparatus for preventing collision of aircraft, which simply and inexpensively offers data necessary for safety navigation of aircraft, in relation to the warning zone of aircraft, as well as positions and flying paths of other aircraft approaching with probability of collision. The system easily and inexpensively offers data necessary for safety navigation of aircraft, in relation to the warning zone of aircraft, positions and flying paths of other aircraft approaching with probability of collision, by changing the shape of the warning zone to a required shape depending upon the speed of own aircraft, and by changing the range of displaying menacing aircraft depending upon the ascending angle or descending angle of own aircraft, and displaying the detected data on the distance and azimuth of other aircraft in terms of a predetermined afterglow time.

公开(公告)号：WO1996002905A1

公开(公告)日：1996-02-01

申请号：PCT/US1995008946

申请日：1995-07-14

Applicant: WORLDWIDE NOTIFICATION SYSTEMS, INC.

Inventor： WORLDWIDE NOTIFICATION SYSTEMS, INC. ,  FARMAKIS, Tom, S. ,  ROUTSONG, Russell, D.

IPC: G08G05/04

CPC classification number: G08G9/00 ,  G01S5/0027 ,  G01S5/0072 ,  G01S19/15 ,  G01S19/40 ,  G01S19/41 ,  G01S19/49 ,  G01S2205/005 ,  G08G1/205 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0082 ,  G08G5/065

Abstract: A satellite based air traffic control (ATC) system includes an aircraft unit (18) on an aircraft and an ATC facility (48). The aircraft unit (18) includes an AARTS processor (28), GPS receivers (20, 22), a comparator (24) for comparing the GPS data, a two-way radio (44) and a transmitter (32) and receiver (33) for communicating information over a data link with the ATC facility (48). The ATC facility (18) includes an ATC computer (66), a two-way radio (52), a display (70) for displaying aircraft and a transmitter (61) and receiver (60) for communicating information and data over the data link. The aircraft transmits aircraft identification information, GPS data, aircraft status information and a transmit detect code to the ATC facility (48) to allow the ATC to track the aircraft and identify the aircraft communicating on two-way radio (52). The traffic control system and a flight control system utilizing GPS may be used for aircraft in the air and on ground and may be used for ships, boats, automobiles, trains or railroads.

Abstract translation: 基于卫星的空中交通管制（ATC）系统包括飞机上的飞机单元（18）和空中交通管制设施（48）。 飞机单元（18）包括AARTS处理器（28），GPS接收器（20,22），用于比较GPS数据的比较器（24），双向无线电（44）和发射机（32）和接收机 33），用于通过与ATC设施（48）的数据链路传送信息。 ATC设施（18）包括ATC计算机（66），双向无线电（52），用于显示飞机的显示器（70）和用于通过数据传送信息和数据的发射机（61）和接收机（60） 链接。 飞机将飞行器识别信息，GPS数据，飞行器状态信息和发射检测码发送到ATC设施（48），以允许ATC跟踪飞机并识别在双向无线电（52）上通信的飞机。 交通控制系统和使用GPS的飞行控制系统可以用于空中和地面的飞机，并可用于船舶，船只，汽车，火车或铁路。

公开(公告)号：WO1988009027A1

公开(公告)日：1988-11-17

申请号：PCT/AU1988000137

申请日：1988-05-09

Applicant: DUNLAVY, John, Harold

IPC: G08G05/04

CPC classification number: G08G5/0008 ,  G01S13/9303 ,  G08G5/0078 ,  G08G5/045

Abstract: An aircraft collision potential warning system in which each aircraft includes means for transmitting pulse sequences, in pseudo random or random fashion and on a common frequency, which include aircraft identification and altitude information. Each aircraft further includes means to receive and process incoming signals from other aircraft and, on the basis of the altitude information, discard those signals not within a collision potential altitude range. If a signal is within a collision potential altitude range, interrogation is effected specifically to the identified signal source and the closing speed between the two aircraft is determined. If the rate of change of closing speed is below a set figure, a collision potential exists.

Abstract translation: 一种飞机碰撞潜在警告系统，其中每架飞机包括用于以伪随机或随机方式以及共同频率发射脉冲序列的装置，包括飞机识别和高度信息。 每个飞机还包括接收和处理来自其他飞机的进入信号的装置，并且基于高度信息，丢弃那些不在碰撞潜在高度范围内的信号。 如果信号处于碰撞潜在高度范围内，则特定地询问询问信号源并确定两架飞机之间的关闭速度。 如果关闭速度的变化率低于设定值，则存在碰撞电势。

公开(公告)号：WO1993006579A1

公开(公告)日：1993-04-01

申请号：PCT/US1992008131

申请日：1992-09-25

Applicant: DEMPSEY, Robert, H.

IPC: G08G05/04

CPC classification number: H05B41/34 ,  B64D47/06 ,  H05B41/42

Abstract: A system and method for extending the useful life of anti-collision lights (100) comprising inert gas flash tubes and which are included on commercial, military, and business jet aircraft. When the aircraft is cruising in high altitude tightly controlled airspace (18) (where instrument flight rules are controlling, i.e., at altitudes above 18,000 feet), and when the aircraft is not undergoing a substantial change in altitude, the power input (58) to the anti-collision lights (100) is reduced. The reduction in the power provides a significant increase in the useful life of the flash tube while causing only a slight reduction in the intensity of the light output of the flash tube.

公开(公告)号：WO1987002493A1

公开(公告)日：1987-04-23

申请号：PCT/JP1985000578

申请日：1985-10-17

Applicant: TOYO COMMUNICATION EQUIPMENT CO., LTD. ,  FUNATSU, Chuhei ,  KITA, Kazuyuki

Inventor： TOYO COMMUNICATION EQUIPMENT CO., LTD.

IPC: G08G05/04

CPC classification number: G08G5/0013 ,  G01S13/782 ,  G01S13/91 ,  G01S13/9303 ,  G08G5/0008 ,  G08G5/0065 ,  G08G5/0082 ,  G08G5/025

Abstract: An alarm restraining system in an apparatus for preventing collision of aircraft which restrains useless alarms produced by the apparatus responsive to signals from other approaching aircraft that are flying at a lower altitude and that are virtually not likely to collide during the takeoff or landing. The system restrains useless alarm that may be produced responsive to signals emitted from other aircraft that are staying in the airfield or that are running along the runway, by decreasing an alarm limit value or by setting it to zero on the side of lower altitudes, by estimating the atmospheric pressure in the nearby airport based upon the altitude data on the aircraft and the data on atmospheric pressure, and further relying upon the altitude value found from the above estimated value and the data on atmospheric pressure contained in the response signals from other aircraft, upon the data on atmospheric pressure in the nearby airport received from the airport center, and upon the altitude value based upon the data on atmospheric pressure contained in the response signals from other aircraft.

Abstract translation: 一种用于防止飞机碰撞的装置中的报警限制系统，该装置响应于在较低高度飞行并且在起飞或着陆期间实际上不可能碰撞的来自其他接近的飞行器的信号而限制该装置产生的无用报警。 该系统限制了无用的报警，其可以响应于停留在机场中或沿着跑道运行的其他飞机发出的信号而产生，通过降低报警极限值或通过在较低高度侧将其设置为零，由 根据飞机上的高度数据和大气压力数据估计附近机场的大气压力，并进一步依靠从上述估计值中找到的高度值和来自其他飞机的响应信号中包含的大气压力数据 根据从机场中心收到的附近机场的大气压力数据，以及基于来自其他飞机的响应信号中包含的关于大气压力的数据的高度值。

公开(公告)号：WO1997034276A1

公开(公告)日：1997-09-18

申请号：PCT/DE1997000484

申请日：1997-03-07

Applicant: VDO LUFTFAHRTGERÄTE WERK GMBH ,  SCHIEFELE, Jens ,  SCHULZE, Richard ,  VON VIEBAHN, Harro

Inventor： VDO LUFTFAHRTGERÄTE WERK GMBH

IPC: G08G05/04

CPC classification number: G08G5/045 ,  G08G5/006

Abstract: In a method of detecting a collision risk and preventing air collisions, it is proposed that probabilities should be calculated for the likely presence of one's own aircraft in predetermined sectors at a number of selected times (probabilities of presence) and these probabilities for one's own aircraft and those for other objects should be used to calculate the probabilities of one's own aircraft and at least one of the other objects being present simultaneously in a given sector (probability of collision) for the predetermined sectors and selected times.

Abstract translation: 在用于检测碰撞的风险并避免在航空冲突的方法中规定，概率为各个自己的飞机与该飞机更多选定的时间将位于预定空间元素（概率）计算出的，以及从该 自己飞机的概率和其他对象的概率的自己的飞行器的同时停留和在相应的空间元素的其他对象（碰撞概率）中的至少一个的概率可以被计算为预定空间元素和所选择的时间点。

公开(公告)号：WO1992005530A1

公开(公告)日：1992-04-02

申请号：PCT/EP1991001734

申请日：1991-09-12

Applicant: HELLA KG HUECK & CO. ,  LEPPER, Werner ,  SCHMEES, Siegfried ,  SCHULTE, Peter ,  NOLTE, Dieter

Inventor： HELLA KG HUECK & CO.

IPC: G08G05/04

CPC classification number: B64D47/02

Abstract: In a process and device for preventing bird-strikes on aircraft with at least one light source on the aircraft which is a discharge lamp and with a control device which varies the frequency of the light flashes generated within at least one cycle time, a simple and economic design is obtained which reduces the power losses, allocates a supply device to at least one light source consisting of at least one voltage transformer and at least one first capacitor and the voltage transformer provides a constant power at varying frequencies of the flashes generated.