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Satellite autonomous power-on system and control method thereof

An electrical system and satellite technology, applied in the aerospace field, can solve the problem of large discharge depth of batteries, and achieve the effects of avoiding vibration or shock response, reducing pre-launch drills, and reducing test procedures.

Active Publication Date: 2020-12-01
INNOVATION ACAD FOR MICROSATELLITES OF CAS +1
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] The purpose of the present invention is to provide a satellite autonomous power-on system and its control method to solve the problem that the existing battery has the risk of excessive discharge depth

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  • Satellite autonomous power-on system and control method thereof
  • Satellite autonomous power-on system and control method thereof
  • Satellite autonomous power-on system and control method thereof

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Embodiment Construction

[0033] The satellite autonomous power-on system and its control method proposed by the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments. Advantages and features of the present invention will be apparent from the following description and claims. It should be noted that all the drawings are in a very simplified form and use imprecise scales, and are only used to facilitate and clearly assist the purpose of illustrating the embodiments of the present invention.

[0034] In addition, unless otherwise stated, features in different embodiments of the present invention can be combined with each other. For example, a feature in the second embodiment may be used to replace a corresponding or functionally identical or similar feature in the first embodiment, and the resulting embodiment also falls within the scope of disclosure or description of the present application.

[0035] In view of the possibilit...

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Abstract

The invention provides a satellite autonomous power-on system and a control method thereof. The system comprises: a first-stage separation circuit which is configured to provide a first control signaland a first power supply signal according to a satellite-rocket separation state; a second-stage separation circuit which is configured to provide a second power supply signal according to a first remote control instruction; a satellite-borne computer which is configured to provide a discharge instruction according to the first control signal; a first-stage discharge circuit which is configured to switch on a circuit between a bus and a storage battery according to the first power supply signal and the second power supply signal; and a second-stage discharge circuit configured to turn on thecircuit between the bus and the battery according to the discharge instruction.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to a satellite autonomous power-on system and a control method thereof. Background technique [0002] Micro-nano satellites have the characteristics of low cost and short development cycle, and have been more and more researched and applied all over the world. Since the capacity of the battery used is generally very small, and the time from launch to orbit of the satellite is fixed, if the design method of the traditional satellite is adopted—the satellite is in the working state during launch, the discharge depth of the battery may decrease after the satellite is separated from the carrier. Reaching more than 70%, there is a risk of satellite power failure or even loss. Therefore, it is necessary to design a circuit so that the satellite is in a power-off state during the launch phase, and is automatically powered on after being separated from the carrier. [0003] Satellites ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02J7/00H02J7/35
CPCH02J7/0063H02J7/00306B64G1/428H02J7/0031Y02E60/10
Inventor 方圆朱月峰白皓龚文斌尚琳
Owner INNOVATION ACAD FOR MICROSATELLITES OF CAS
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