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    • 4. 发明公开
    • Multirate CDMA system based on orthogonal bipolar spreading vectors
    • 多速率CDMA系统基站
    • EP1471675A2
    • 2004-10-27
    • EP03027814.7
    • 2003-12-03
    • NORTHROP CORPORATION
    • Linsky, Stuart T.Wright, David A.
    • H04J11/00
    • H04B1/7093H04B2201/70703H04J13/0048
    • A modulation channelization and demodulation system based on orthogonal bipolar spreading vectors is provided that permits a variable information rate to be transmitted without inducing envelope fluctuations and permits multiple access without requiring the transmitter amplifiers to support the combined information rate of all users. The modulation system uses the vectors of a Hadamard matrix to form communication channels. The information rate on any channel may be doubled by using half the vector length to transmit information. The vector that is not non-orthogonal-in-the-half to the rate-doubled vector is preferably deactivated. In the same fashion, higher information rates may be provided through truncation of the transmission vector and the elimination of the resultant non-orthogonal vectors. A multi-channel receiver including a Fast Hadamard Transform structure comprised of controllable modified logic cells for performing the multi-rate communication of the present invention is illustrated. A multi-channel transmitter for performing the present invention is also shown.
    • 提供了一种基于正交双极性扩展向量的调制信道化和解调系统,其允许在不引起包络波动的情况下传输可变信息速率并且允许多次接入,而不需要发射机放大器来支持所有用户的组合信息速率。 调制系统使用Hadamard矩阵的向量来形成通信信道。 通过使用一半的矢量长度来传输信息,任何频道上的信息速率都可能加倍。 优选不使速率加倍的矢量不是非正交的矢量的失效。 以相同的方式,可以通过截断传输向量和消除所得到的非正交向量来提供更高的信息速率。 示出了包括用于执行本发明的多速率通信的可控修改逻辑单元的快速哈达玛变换结构的多通道接收器。 还示出了用于执行本发明的多通道发送器。
    • 5. 发明授权
    • OBSTACLE AVOIDANCE SYSTEM FOR HELICOPTERS AND AIRCRAFT
    • 直升机和飞机避障系统
    • EP0648340B1
    • 1999-06-16
    • EP94914861.3
    • 1994-04-20
    • NORTHROP CORPORATION
    • KRUMES, RolfRICHMAN, Dennis, C.BOSE, Carl, L.
    • G01S17/88
    • G01S17/933G05D1/0646
    • A system for sensing objects in the flight path of an aircraft and alerting the pilot to their presence includes a laser radar subsystem for emitting a beam of laser energy, receiving returns from objects, and processing the returns to produce range data related to the range of the objects from the aircraft. A scanning subsystem scans the beam and produces directional information related to the instantaneous direction of the beam relative to the aircraft. Processor circuitry controls operation, processes the range data and directional information with instrumentation data from the avionics system, produces video information related to the range, direction, and type of the objects, and interfaces the video information to the video display system. The processor circuitry may be programmed to (1) overlay video information on existing aircraft video display system, (2) provide acoustical warnings on an aircraft intercom, (3) analyze returns by subdividing the field of regard into a series of analysis windows, performing a statistical analysis of the returns related to each of the analysis windows, and identifying returns that fall into a common range interval, (4) transforming coordinates of objects measured relative to the aircraft to a horizon-stabilized, north-oriented coordinate system which is independent of the attitude of the aircraft, (5) inserting the coordinates of identified objects into a data base so that the coordinates may be used for constructing a video display at a later time and updating the data base to correct for movements of the aircraft, and (6) constructing a window-of-safety display of objects currently within the field of regard by adjusting the displayed position of the objects to compensate for avoidance maneuvers the pilot may execute.
    • 6. 发明公开
    • OBSTACLE AVOIDANCE SYSTEM FOR HELICOPTERS AND AIRCRAFT
    • 避障系统,直升机和飞机。
    • EP0648340A1
    • 1995-04-19
    • EP94914861.0
    • 1994-04-20
    • NORTHROP CORPORATION
    • KRUMES, RolfRICHMAN, Dennis, C.BOSE, Carl, L.
    • G01S17
    • G01S17/933G05D1/0646
    • A system for sensing objects in the flight path of an aircraft and alerting the pilot to their presence includes a laser radar subsystem for emitting a beam of laser energy, receiving returns from objects, and processing the returns to produce range data related to the range of the objects from the aircraft. A scanning subsystem scans the beam and produces directional information related to the instantaneous direction of the beam relative to the aircraft. Processor circuitry controls operation, processes the range data and directional information with instrumentation data from the avionics system, produces video information related to the range, direction, and type of the objects, and interfaces the video information to the video display system. The processor circuitry may be programmed to (1) overlay video information on existing aircraft video display system, (2) provide acoustical warnings on an aircraft intercom, (3) analyze returns by subdividing the field of regard into a series of analysis windows, performing a statistical analysis of the returns related to each of the analysis windows, and identifying returns that fall into a common range interval, (4) transforming coordinates of objects measured relative to the aircraft to a horizon-stabilized, north-oriented coordinate system which is independent of the attitude of the aircraft, (5) inserting the coordinates of identified objects into a data base so that the coordinates may be used for constructing a video display at a later time and updating the data base to correct for movements of the aircraft, and (6) constructing a window-of-safety display of objects currently within the field of regard by adjusting the displayed position of the objects to compensate for avoidance maneuvers the pilot may execute.
    • 8. 发明授权
    • PENTAGONAL RING LASER GYRO
    • EP0388402B1
    • 1993-02-03
    • EP88904423.6
    • 1987-11-02
    • NORTHROP CORPORATION
    • LIM, Wah, L.HAUCK, James, P.RAQUET, Jack, W.
    • G01C19/64H01S3/083
    • G01C19/661H01S3/083H01S3/0835
    • A ring laser gyroscope (10) incorporates a resonant cavity generally shaped as an irregular pentagon having a portion thereof conformed as three legs, a base (21), and two (22, 25) of a rectangle closed by two symmetrical other legs (23, 24) to form an apex whose bisector defines a symmetrical structure in the base of which are carried a central cathode and end mounted anodes to define two discharge paths generating oppositely directed laser beams. As a result, the enclosed area is increased, increasing sensitivity and decreasing lock-in, while magnetic effects are reduced. Additionally, the irregular shape allows for the extension of the gain medium which therefore increases the effectiveness thereof.
    • 环形激光陀螺仪(10)包括谐振腔,谐振腔通常形成为不规则五边形,其一部分形成三条腿,基部(21)和由两个对称的另一条腿(23)封闭的矩形的两个(22,25) ,24)以形成其平分线限定对称结构的顶点,在所述对称结构的基座中承载中心阴极并且端部安装阳极以限定产生相反方向的激光束的两个放电路径。 结果,封闭区域增加,灵敏度增加并且锁定减少,而磁性效应降低。 另外,不规则形状允许增益介质的延伸,因此增加了其有效性。