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Modular satellite architecture

A modular and satellite technology, applied in the direction of program control and electrical program control in sequence/logic controllers, can solve problems such as unformed, reduce time and cost, meet mass production and rapid launch, and reduce debugging time Effect

Pending Publication Date: 2018-05-18
黄一君
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

CubeSat is a successful example in nano-satellites; however, in 100-kilogram small satellites, this kind of standardized and highly versatile satellite architecture design has not yet taken shape

Method used

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Embodiment Construction

[0028] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals denote the same or similar components or components having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention.

[0029] figure 1 is a structural diagram of a modular satellite architecture according to an embodiment of the present invention, figure 2 is a structural diagram of a functional module of an embodiment of the present invention, image 3 is a structural block diagram of a modular satellite architecture according to an embodiment of the present invention.

[0030] refer to Figure 1-Figure 3 , the present invention provides a modular satellite architecture, the modular satellite architecture is used for assembling production s...

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Abstract

The present invention provides a modular satellite architecture that includes a plurality of functional modules. The size and parameters of each functional module in the multiple functional modules are adjustable, and the plurality of functional modules can be freely combined. The combination can be arbitrarily according to the needs of the task, the debugging time is reduced, the mass productionand rapid launch can be fully met, and at the same time the time and cost of the satellite mass production can be greatly reduced; and the main structure of the modular satellite architecture is the various functional modules, each functional module is composed of component modules, and the component modules included in each functional module also have their own modular western standards. Therefore, the architecture has dual modularity features.

Description

technical field [0001] The present invention relates to a modular satellite architecture. Background technique [0002] Throughout the development and evolution of satellite development technology, it can be divided into three stages: (1) traditional design; (2) public platform design; (3) modular standardized design [0003] (1) The first stage: traditional design method [0004] The traditional design method is mainly based on the given mission requirements and loads, and separately designs the subsystems of the satellite, including power supply, attitude control, structure, temperature control, communication, on-board computer, etc., and then finally integrates and debugs them. . The advantage of this method is that it can efficiently complete the tasks undertaken by the satellite, but it also has the disadvantages of long development cycle and high development cost. [0005] (2) The second stage: public platform design method [0006] This method aims to design a com...

Claims

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Application Information

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IPC IPC(8): G05B19/04
CPCG05B19/04
Inventor 黄一君
Owner 黄一君
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