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Method for controlling generator tripping based on small satellite dual-machine system

The technology of a dual-machine system and control method is applied in the direction of response error generation, redundant data error detection in hardware, and instruments, which can solve problems such as satellite long-term gaps, and achieve long-term gap problems and fast Restoration, improvement of reliability and lifespan effect

Pending Publication Date: 2020-10-02
XIAN MICROELECTRONICS TECH INST
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  • Abstract
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Problems solved by technology

[0004] The purpose of the present invention is to solve the long-time gap problem existing in the satellite flight mission switching process, and to provide a control method based on the small satellite dual-machine system cut-off

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  • Method for controlling generator tripping based on small satellite dual-machine system
  • Method for controlling generator tripping based on small satellite dual-machine system
  • Method for controlling generator tripping based on small satellite dual-machine system

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Embodiment Construction

[0036] In order to enable those skilled in the art to better understand the solutions of the present invention, the following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only It is an embodiment of a part of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0037] It should be noted that the terms "first" and "second" in the description and claims of the present invention and the above drawings are used to distinguish similar objects, but not necessarily used to describe a specific sequence or sequence. It is to be understood that the data so used are interchangeable under appropriate circums...

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Abstract

The invention discloses a method for controlling generator tripping based on a minisatellite dual-computer system, and belongs to the field of satellite computers. According to the control method forgenerator tripping based on the minisatellite dual-computer system, dual computers are monitored by watchdogs, and the method comprises the following operations: when a host is on duty, enabling the host to regularly write data into a host FIFO and a standby FIFO; if dog bite occurs once, submitting NMI interruption, recording and rewinding the satellite computer application program, and running the satellite computer application program again; if dog bite occurs twice continuously, resetting the host system, enabling software and hardware of the host system to recover to the initial state, and enabling the program to run again; if dog bite occurs for three times continuously, powering up a standby machine, automatically transmitting data to the FIFO of the standby machine by the FIFO of the host machine after the standby machine is reset, finishing data migration after the standby machine extracts the data, and rerunning the system. According to the invention, the problem of long-timegaps in the flight mission switching process is solved.

Description

technical field [0001] The invention belongs to the field of satellite computing, in particular to a control method based on a small satellite dual-machine system cut-off. Background technique [0002] As the core component of the satellite platform system, the star computer is responsible for completing the comprehensive information processing of the satellite, managing and controlling each mission module on the satellite, monitoring the status of the entire satellite, coordinating the work of the entire satellite, and realizing various controls and settings with the payload. Complete the remote control telemetry mission of the whole star. The traditional Starworks computer adopts a dual-computer cold backup architecture and is in the working mode of always powering on. [0003] In view of the importance of the position of the star computer in the entire star, when facing a complex space environment, when the star computer has a failure mode such as a single event flip, de...

Claims

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Application Information

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IPC IPC(8): G06F11/07G06F11/20G06F11/10
CPCG06F11/0757G06F11/2028G06F11/1004
Inventor 李彦妮
Owner XIAN MICROELECTRONICS TECH INST
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