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Eight-rod-connecting type non-contact satellite platform configuration and assembling method

A satellite platform, non-contact technology, used in artificial satellites, transportation and packaging, space navigation equipment, etc., can solve problems such as practical application difficulties, complex spacecraft attitude control systems, platform vibration interference, etc., to facilitate parallel development, module The effect of obvious characteristics and clear interface

Active Publication Date: 2014-09-24
SHANGHAI SATELLITE ENG INST
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  • Claims
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Problems solved by technology

At the same time, based on voice coil motor technology, foreign countries have developed a non-contact non-disturbance load satellite platform configuration based on a six-bar connection in the form of stewart, which can solve the problem of platform vibration interference, but it brings the complexity of the spacecraft attitude control system. difficulty

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  • Eight-rod-connecting type non-contact satellite platform configuration and assembling method
  • Eight-rod-connecting type non-contact satellite platform configuration and assembling method
  • Eight-rod-connecting type non-contact satellite platform configuration and assembling method

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Embodiment Construction

[0037] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0038] The eight-rod connection non-contact satellite platform configuration, through the non-contact interface module, realizes the complete isolation of the payload from the vibration and interference response of the platform, meets the requirements for the use of ultra-precision and ultra-stable pointing loads, and can be applied to very high-precision remote sensing satellites, deep space Detecting astronomical telescopes and other spacecraft carrying high-resolution sensitive payloads will gre...

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Abstract

The invention provides an eight-rod-connecting type non-contact satellite platform configuration and an assembling method. The eight-rod-connecting type non-contact satellite platform configuration comprises an upper connecting plate, a lower connecting plate, four same vertical mounting force actuators and four same horizontal mounting force actuators; both the vertical mounting force actuators and the horizontal mounting force actuators are connected between the upper connecting plate and the lower connecting plate and are arranged in a circumference manner; the vertical mounting force actuators and the horizontal mounting force actuators are arranged along the same circumference in a staggered and orthorhombic manner; the vertical mounting force actuators are vertical to the horizontal mounting force actuators. The eight-rod-connecting type non-contact satellite platform configuration implements complete isolation of an effective load on platform vibration and interference response, can be applied to spacecrafts with high-resolution sensitive effective load, such as a very-high accuracy remote sensing satellite, a deep space exploration astronomical telescope and the like, and can greatly improve exploration performance of spacecrafts.

Description

technical field [0001] The present invention relates to a non-contact satellite platform configuration, in particular to an eight-bar connection type non-contact satellite platform configuration. Background technique [0002] Flexible accessories, liquid sloshing, etc. are very flexible, and the problem of spacecraft chatter caused by dense low-frequency modes is becoming more and more obvious, which greatly limits the bandwidth of the control system; the periodic dynamic interference induced by moving parts such as flywheels, gyroscopes, and drive mechanisms is constantly Cause harmful vibration of the load. With the improvement of spacecraft performance requirements, the problems of attitude control and flutter suppression caused by these factors have become the main constraints for the development of subsequent advanced spacecraft. [0003] At present, there are mainly two types of vibration isolation platforms, passive and active, for the vibration of satellite flexible...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/10B64G1/22
Inventor 许域菲袁金如廖鹤赵洪波裘俊邓成晨赵艳彬路同山张伟
Owner SHANGHAI SATELLITE ENG INST
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