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Compact six-freedom-degree accurate tracking and pointing device for satellite load

A technology of pointing devices and degrees of freedom, applied in the field of aerospace vehicles in the field of aerospace technology, can solve problems such as power supply/control cable routing design, limited payload working space, and large working envelope, achieving good engineering feasibility and Scalability, strong engineering realizability, tracking and pointing angles and effects with a large range

Active Publication Date: 2018-01-19
SHANGHAI SATELLITE ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, although the traditional six-degree-of-freedom space pointing device can meet high-precision tracking and pointing functions, and is widely used in satellite precise pointing and positioning, vibration isolation and space docking, etc., it has limited working space for payloads, power supply / control cable routing, etc. In addition, if the working space is expanded by means of translation and rotation, the working envelope of the device on the satellite will be relatively large, which will seriously affect the space resources of other components on the satellite, and cause mechanical, optical and electromagnetic interference.

Method used

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  • Compact six-freedom-degree accurate tracking and pointing device for satellite load

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Embodiment Construction

[0032] 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.

[0033] Such as Figure 1-Figure 15 As shown, a compact six-degree-of-freedom precise tracking and pointing device for satellite load provided by this embodiment,

[0034]The pointing device consists of an upper platform and a lower platform connected in series along the normal direction of the installation surface. The upper platform is responsible for the precise pointing and follow-up tracking of the payload in any direction of six degrees of freedom, and the lower platform is responsible for th...

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Abstract

The invention discloses a compact six-freedom-degree accurate tracking and pointing device for a satellite load, and the device is formed by the series connection of an upper platform and a lower platform in a normal direction of an installation surface. The upper platform comprises a pointing interface assembly, an adjustment interface assembly, six sets of drive assemblies, an upper platform control single-chip microcomputer, and an upper platform compressing and releasing device. The upper platform comprises an adjustment assembly, a lower platform compressing and releasing apparatus, a fixed plate, and a lower platform control single-chip microcomputer. The device can avoid the interference in a tracking and pointing work space under the cooperation of the upper and lower platforms, and meets the demands of the large-range and large-angle continuous precise follow-up tracking and orientation locating of a satellite effective load. The device can effectively reduce a motion envelopespace of the device through extending the work space of the upper platform through the lower platform, achieves the compact design, and saves the satellite space resources. The tracking and pointingdirection can be any one direction of the six degrees of freedom, and the device can flexibly achieve the full-airspace and full-disc tracking and pointing of the satellite effective load.

Description

technical field [0001] The invention relates to aerospace vehicles in the field of aerospace technology, in particular to a compact six-degree-of-freedom precise tracking and pointing device for satellite loads. Background technique [0002] Payloads such as optical instruments and antennas on satellites have higher and higher requirements for large-angle, large-scale tracking and pointing tasks and their accuracy, and there are multi-degree-of-freedom tracking and pointing requirements. In order to meet this requirement, only relying on satellite attitude Control has the problems of high cost and low efficiency, and when the satellite has more than two payloads that need to be tracked at the same time or point to different areas, the satellite attitude control cannot meet the requirements. Therefore, it is necessary to design a corresponding mechanism or device to carry the payload on the device to realize on-orbit large-angle, large-scale tracking and pointing tasks, and t...

Claims

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Application Information

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IPC IPC(8): G06T7/292
Inventor 俞洁蒋国伟铁琳白沁园梁奕瑾
Owner SHANGHAI SATELLITE ENG INST
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