首页> 外国专利> LASER PULSE COMPRESSION RANGING SYSTEM USING DOUBLE-CHIRPED PULSES

LASER PULSE COMPRESSION RANGING SYSTEM USING DOUBLE-CHIRPED PULSES

机译:采用双脉冲的激光脉冲测距系统

摘要

1,249,843. Lasers. UNITED AIRCRAFT CORP. 27 Feb., 1970, No. 9661/70. Heading H1C. [Also in Division H4] Laser rangefinding apparatus has a pair of Q switched lasers A and B, Fig. 2, each controlled by the same rotating mirror 14. The mirror rotates about axis 16 so that while the resonator of laser A formed by reflectors 12, 18 and 14 is increasing in length, the resonator of laser B is decreasing in length. The resonator mirrors 12, 18, 181 and 14 are arranged so that the lasers give simultaneous output pulses which are superimposed into one beam by mirrors 24 and 26. Because one resonator shortens as the other lengthens, the frequency of the pulse from laser A falls during the pulse, while that of laser B rises, Fig. 3. The combined output is thus a so called " double chirped " pulse, and allows advantage to be taken of the laser bandwidth, giving high resolution. The lasers are preferably of the CO 2 type, and the pulse lasts for 1 Á see, allowing considerable energy to be transmitted, but since this is a relatively long time for radar applications the receiving apparatus, Fig. 5, includes a compression circuit to restore the advantages of the laser bandwidth. The laser pulse, which may be amplified before transmission, is scattered from a target and received by a square law photodetector. The resulting electrical signal is subjected to high pass filtering to give an a.m. signal which is used to modulate a 300 MHz carrier in a balanced modulator carrier suppressed circuit 58. The resulting signal, in the form of a.m. sidebands, is fed to compressor 16 which has a group delay which increases linearly with frequency. The effect of this is to amplify the high frequencies of the signal and to attenuate and delay the low frequencies, hence producing a spike output, Figs 7, 8 (not shown), which may be visually displayed.
机译:1,249,843。激光。联合飞机公司1970年2月27日,编号9661/70。标题H1C。 [也在H4区中]激光测距设备具有一对Q开关激光器A和B,图2,每个都由同一旋转镜14控制。该镜绕着轴16旋转,因此激光器A的谐振器由反射镜形成图12、18和14的长度增加,而激光器B的谐振器的长度减少。设置谐振腔镜12、18、181和14,使激光器同时发出输出脉冲,并由反射镜24和26叠加成一个光束。由于一个谐振腔随着另一个谐振腔的延长而缩短,因此来自激光器A的脉冲频率下降在脉冲期间,激光器B的脉冲上升,图3。因此,组合输出为所谓的“双double”脉冲,并允许利用激光器带宽的优势,从而提供高分辨率。激光器最好是CO 2型激光器,脉冲持续1 s见,允许发射大量能量,但是由于这对于雷达应用来说是相对较长的时间,因此图5的接收设备包括一个压缩电路,用于恢复了激光带宽的优势。可以在传输之前被放大的激光脉冲从目标散射并被平方律光电探测器接收。所得的电信号经过高通滤波,得到一个am信号,该信号用于在平衡调制器载波抑制电路58中调制300 MHz载波。所得的am边带形式的信号被馈送到压缩机16。具有群延迟,该群延迟随频率线性增加。这样的效果是放大信号的高频并衰减和延迟低频,因此产生图7、8(未示出)的尖峰输出,其可以被可视地显示。

著录项

  • 公开/公告号GB1249843A

    专利类型

  • 公开/公告日1971-10-13

    原文格式PDF

  • 申请/专利权人 UNITED AIRCRAFT CORPORATION;

    申请/专利号GB19700009661

  • 申请日1970-02-27

  • 分类号G01S17/10;H01S3;H01S3/05;H01S3/098;H01S3/105;H01S3/11;H01S3/121;H01S3/123;H01S3/23;

  • 国家 GB

  • 入库时间 2022-08-23 09:13:07

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