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Satellite optical communication high precision advance sighting angle compensating device

A satellite optical communication and angle compensation technology, applied in satellite communication transmission, electromagnetic wave transmission system, electrical components and other directions, can solve the problems of complex actuator and slow dynamic response speed.

Inactive Publication Date: 2010-05-12
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to provide a high-precision advance aiming angle compensation device for satellite optical communication, so as to overcome the disadvantages of complex actuators and slow dynamic response in the prior art

Method used

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  • Satellite optical communication high precision advance sighting angle compensating device
  • Satellite optical communication high precision advance sighting angle compensating device
  • Satellite optical communication high precision advance sighting angle compensating device

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Experimental program
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specific Embodiment approach 1

[0005] Specific implementation mode one: the following combination figure 1 , figure 2 and Figure 5 This embodiment will be specifically described. This embodiment is composed of an arithmetic processor 1, a drive controller 2, an aiming actuator 3 and an angle sensor 4, and the output terminal of the arithmetic processor 1, which can calculate the current point-in-advanced aiming angle value through the orbit data of the satellite, is connected to the drive One input end of the controller 2, the output end of the drive controller 2 is connected to the input end of the aiming actuator 3, the angle sensor 4 is arranged on the aiming actuator 3 to measure its rotation angle in real time, and the output end of the angle sensor 4 is connected to the drive control The other input terminal of device 2 is used to realize angle feedback, and the aiming actuator 3 is composed of No. 1 piezoelectric ceramic column 3-1, No. 2 piezoelectric ceramic column 3-2, worktable body 3-3, work...

specific Embodiment approach 2

[0006] Specific implementation mode two: the following combination image 3 This embodiment will be specifically described. The difference between this embodiment and Embodiment 1 is: angle sensor 4 is made up of No. 1 micro-displacement sensor 4-1 and No. 2 micro-displacement sensor 4-2, No. 1 micro-displacement sensor 4-1 and No. 2 micro-displacement sensor 4 -2 are all selected resistance strain sensors and built into the No. 1 piezoelectric ceramic column 3-1 and the No. 2 piezoelectric ceramic column 3-2 respectively, and the drive controller 2 is composed of the No. 1 drive control circuit 2- with the same structure. 1 and No. 2 drive control circuit 2-2, one input end of the No. 1 drive control circuit 2-1 is connected to an output end of the arithmetic processor 1, and the other input end of the No. 1 drive control circuit 2-1 is connected to the No. 1 drive control circuit 2-1. The output end of the micro-displacement sensor 4-1, an input end of the No. 2 drive contr...

specific Embodiment approach 3

[0007] Specific implementation mode three: the following combination Figure 4 This embodiment will be specifically described. The difference between the present embodiment and the second embodiment is: No. 1 drive control circuit 2-1 is composed of resistor R1, resistor R2, resistor R3, resistor R4, resistor R5, resistor R6, capacitor C, integrated operational amplifier U1A and integrated operational amplifier Composed of U2B, one end of the resistor R1 is connected to an output end of the operational processor 1, the other end of the resistor R1 is connected to one end of the resistor R4 and the inverting input end of the integrated operational amplifier U1A, and the same input end of the integrated operational amplifier U1A is connected to the resistor R3 One end of the resistor R2 and one end of the resistor R3, the other end of the resistor R3 is grounded, the other end of the resistor R2 is connected to the output end of the No. 1 micro-displacement sensor 4-1, and the o...

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Abstract

This invention relates to satellite light communication high precision aiming at angle advance compensation arrangement, which composed of the computing processor (1), driving controller (2), aiming operating structure (3) and angle sensor (4), the outlet of (1) connects with one inlet of (2), the outlet of (2) connects with the inlet of (3), (4) is arranged on (3), the outlet of (4) connects withthe other inlet, (3) is composed of number one piezo-electric ceramic pole (3-1), number two piezo-electric ceramic pole (3-2), working platform (3-3), working platform (3-4) and flexble hinge (3-5), (3-5) is fixed at the edge of the (3-4)'s down face and (3-3)'s upper face, (3-1), (3-2) are arranged in (3-2), (3-1) and (3-2)' upper face prop up the down face of (3-4), (3-5) is arranged at (3-1)and (3-2)'s sides and has the same distance with (3-1) and (3-2).

Description

technical field [0001] The invention relates to a satellite optical communication device, in particular to an advance aiming compensation device in the satellite optical communication device. Background technique [0002] The distance of signal transmission in inter-satellite optical communication is very long, which makes the relaxation time of transmission longer. When considering the relative motion between two satellites, the transmitting end must actually aim the beam to the "front" of the receiving end so that the receiving end can receive the signal. That is to say, when aiming, the transmitter must take into account the additional movement between the two stars that occurs during the beam transmission relaxation time, so as to align to the expected angular position. This aiming process is usually referred to as aiming in advance. The principle of the existing angle compensation device for advance aiming is to predict the value of the advance aiming angle at the cur...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H04B10/105H04B10/118
Inventor 谭立英马晶于思源韩琦琦
Owner HARBIN INST OF TECH
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