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Satellite-rocket separation autonomous power-on circuit

A technology of star-rocket separation and charging circuit, applied in the field of star-rocket separation, can solve problems such as inability to achieve rapid launch of commercial spaceflight, inflexible design ideas, and main satellite signal interference.

Active Publication Date: 2020-12-01
航天行云科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, with the rapid development of micro-satellite technology and the rapid development of commercial spaceflight, the demand for multi-satellite or satellite-carried missions is increasing day by day. If the satellites are always powered on when they are on the rocket, it may cause unnecessary damage to the main star. Signal interference, and this design idea is not flexible, and the satellite battery needs to be recharged before the launch, which cannot meet the needs of rapid commercial space launches.

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Embodiment Construction

[0025] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative efforts fall within the protection scope of the present invention.

[0026] In describing the present invention, it should be understood that the terms "center", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", " The orientation or positional relationship indicated by "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. is based on the orientation shown in the drawings Or positional relationship is only for the convenience of describing the present invention and simpl...

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Abstract

The embodiment of the invention discloses a satellite-rocket separation autonomous power-on circuit, which comprises a solar cell array, a bus, a storage battery pack, a self-starting power-on switch,a separation self-starting circuit, a separation switch, a discharge switch, a satellite service computer and a DC / DC module. Before satellite-rocket separation, the separation self-starting circuitis set to be in an enabling state, the separation switch is set to be in a closed state, the discharge switch is set in an off state, and the whole satellite is in a power-down state; after satellite-rocket separation, the separation switch is changed from a closed state to an open state, the self-starting power-on switch is switched on, the storage battery pack supplies power to the bus, the whole satellite is power-on and starts; in order to avoid faults of the separation switch or the self-starting power-on switch to enable the whole satellite to be unable to be power-on, and then the satellite service computer sends a switch-on instruction to switch on the discharge switch, the separation self-starting circuit is set to be in a forbidden state from an enabled state, the separation self-starting circuit controls the self-starting power-on switch to be switched off, and the storage battery pack supplies power to the bus through the discharge switch, so that autonomous power-on of thesatellite after satellite-rocket separation is realized.

Description

technical field [0001] The invention relates to the technical field of star-arrow separation, in particular to an autonomous power-on circuit for star-arrow separation. Background technique [0002] The traditional satellite platform is generally in the power-on state during the launch process. After the satellite and rocket are separated, the star affairs computer detects the effective signal of the satellite and rocket separation. As the initial moment of the whole satellite, it starts to execute the program control program, starts the attitude control, and the pyrotechnics detonation control. , status monitoring, load photography and other operations. However, with the rapid development of micro-satellite technology and the rapid development of commercial spaceflight, the demand for multi-satellite or satellite-carried missions is increasing day by day. If the satellites are always powered on when they are on the rocket, it may cause unnecessary damage to the main star. ...

Claims

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Application Information

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IPC IPC(8): H02J9/06H02J7/35
CPCH02J9/061H02J7/35Y02B10/70
Inventor 吕海全高佳隽王星又史礼婷邱格胡乔朋杨俊涛周通胡迅
Owner 航天行云科技有限公司