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Method for using multistage vibration isolation platform to improve optic loading imaging quality

A vibration isolation platform, imaging quality technology, applied in general control systems, instruments, adaptive control and other directions, can solve problems such as low accuracy and stability of payload imaging

Inactive Publication Date: 2014-05-14
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Abstract
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AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the problem of low imaging accuracy and stability of optical payloads in the prior art, and discloses a method for improving the imaging quality of optical payloads using a multi-stage vibration isolation platform

Method used

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  • Method for using multistage vibration isolation platform to improve optic loading imaging quality
  • Method for using multistage vibration isolation platform to improve optic loading imaging quality
  • Method for using multistage vibration isolation platform to improve optic loading imaging quality

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Embodiment 1

[0051] like figure 1 As shown, a vibration isolation platform includes: an upper platform 1, a lower platform 3, and a strut 2 connecting the upper platform 1 and the lower platform 3; the installation form of the vibration isolation platform on the satellite is as follows figure 2 As shown, it can be installed between satellite actuators such as flywheel 5 or control moment gyroscope 6 and satellite body 9, and between optical payload 8 and satellite body 9; when adding vibration isolation between flywheel 5 and satellite body 9 When the platform is installed, the upper platform of the vibration isolation platform can be fixedly connected with the flywheel housing to form a set of upper platform system; when using the vibration isolation platform between the control moment gyroscope 6 and the satellite body 9, a set Mounting frame 7, one end of mounting frame 7 is fixedly connected at the upper platform place of vibration-isolation platform, and the other end of mounting fra...

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Abstract

The invention relates to a method for improving optic loading imaging quality, in particular to the method for using a multistage vibration isolation platform to improve the optic loading imaging quality, and belongs to the field of high-frequency vibration control. The vibration isolation platform comprises an upper platform, a lower platform and a support rod for connecting the upper platform and the lower platform. The vibration isolation platform can be installed on a flywheel or a control moment spinning top and the like between a satellite actuating mechanism and a satellite star or between an optic payload and the satellite star. The control moment spinning top, an installation support and the upper platform of the vibration isolation platform jointly form an upper platform system. When the optic payload and the satellite star are needed for loading the vibration isolation platform, a base of the optic payload is fixedly connected with the upper platform of the vibration isolation platform to form a set of the upper platform system. The lower platforms of all vibration isolation platforms are fixedly connected onto the satellite star to jointly form a lower platform system. The method solves the problem that imaging accuracy and stability of the optic payload on a star are low.

Description

technical field [0001] The invention relates to a method for improving the imaging quality of an optical load, in particular to a method for improving the imaging quality of an optical load by using a multi-stage vibration isolation platform, and belongs to the field of high-frequency vibration control. Background technique [0002] At present, the main vibrating components on spacecraft are actuators with high-speed rotors such as flywheels or control moment gyroscopes. Their vibration is mainly caused by the static and dynamic unbalance of the high-speed rotor and the installation error of the mechanical bearing, and the resulting vibration will directly affect the imaging quality of the optical load. Combining a Design Method of Flywheel Attitude Control System for Flexible Aircraft (Geng Yunhai, Cui Hutao, Cui Haiying, Yang Di. Design of Flywheel Attitude Control System for Flexible Aircraft[J]. System Engineering and Electronic Technology. 2001, 23(6) :55-58), and addi...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/08G05B13/04
Inventor 张尧张景瑞翟光
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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