CubeSat satellite platform based on mobile phone

A satellite platform and cube star technology, applied in the field of aerospace micro-nano satellites, can solve the problems of poor scalability and reconfigurability, long R&D cycle, etc., and achieve a short R&D cycle, strong scalability and reconfigurability Effect

Active Publication Date: 2017-06-13
NAT UNIV OF DEFENSE TECH
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Problems solved by technology

[0005] The invention provides a mobile phone-based CubeSat satellite platform to solve the technical problems...

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  • CubeSat satellite platform based on mobile phone
  • CubeSat satellite platform based on mobile phone
  • CubeSat satellite platform based on mobile phone

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Embodiment Construction

[0048] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0049] refer to figure 1, the preferred embodiment of the present invention provides a mobile phone-based CubeSat satellite platform, including a smart phone 10, an interface adapter module 20 and an external module, the external module includes an attitude control module 30, a communication module 40, a maneuverable module 50 and a One or more of the extended load modules 60, the smart phone 10 is connected to the attitude control module 30, the communication module 40, the motor module 50 and / or the expandable load module 60 through the interface adapter module 20, wherein the smart phone 10 , as a star computer system, used to interact with the attitude control module 30, the communication ...

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Abstract

The invention discloses a CubeSat satellite platform based on a mobile phone. The CubeSat satellite platform comprises the smartphone, an interface switching module and an external module, wherein the external module comprises one or more of an attitude control module, a communication module, a maneuvering module and an extendable loading module, the smartphone is used for performing interaction with the attitude control module, the communication module, the maneuvering module and/or the extendable loading module respectively through the interface switching module to complete satellite platform tasks, the attitude control module is used for achieving attitude control of a CubeSat, the a CubeSat is used for achieving information interaction between the CubeSat and a ground station or other spacecrafts, the maneuvering module is used for controlling the CubeSat to operate in a set orbit, and the extendable loading module is used for extending load and/or adding corresponding functional units so as to achieve extendibility of the satellite platform under the control of the smartphone. The coupling problem of satellite design, tasks and progress is effectively solved, the period of study and development is short, and expansibility and reconfigurability are high.

Description

technical field [0001] The invention relates to the field of aerospace micro-nano satellites, in particular to a mobile phone-based CubeSat satellite platform. Background technique [0002] Mobile satellites refer to the direct use of smartphone components to assemble low-cost micro-satellites. Mobile satellites will open up a new field and lower the threshold for non-aerospace hardware and software to enter the space field. [0003] At present, many institutions, including NASA of the United States and SSTL of the United Kingdom, have carried out research on mobile phone satellites. In order to verify whether the processor of the mobile phone can work in space, Surrey Satellite Technology Co., Ltd. of the United Kingdom loaded a modified Nexus-one smartphone on its STRaND-1 satellite launched in 2013. Although this task was unsuccessful, But STRaND-1 is still being called the world's first mobile phone satellite in orbit. However, the existing mobile phone satellites only...

Claims

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Application Information

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IPC IPC(8): B64G1/10B64G1/24B64G1/28B64G1/36B64G1/40B64G1/42B64G1/44
CPCB64G1/1007B64G1/24B64G1/283B64G1/363B64G1/366B64G1/40B64G1/428B64G1/443B64G1/369B64G1/245
Inventor 宋新赵勇杨磊何亮吴帅陈小前陈利虎绳涛
Owner NAT UNIV OF DEFENSE TECH
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