Minisatellite electronic load task uploading method using task template

Abstract

The invention relates to a minisatellite electronic load task uploading method using a task template. The minisatellite electronic load task uploading method includes the steps: 1) when a satellite enters a detectable and controllable area, starting an electronic load lower computer; receiving a task template uploading data packet uploaded by a ground station; and storing a task template in the load lower computer, completing uploading of the task template, storing the task template and shutting down the computer; 2) when the satellite enters a detectable and controllable area again or repeatedly later, starting the electronic load lower computer, and reading the stored task template; 3) receiving a task uploading data packet uploaded by the ground station; and 4) storing the task packet in the load lower computer, completing in-orbit generation of the task packet, storing the task packet and shutting down the computer. The minisatellite electronic load task uploading method using a task template solves the problem that a traditional minisatellite electronic load needs uploading the complete task packet data to a satellite during every task uploading process so that the uploading efficiency is lower, and can reduce the task uploading quantity for minisatellite electronic load and improve the task uploading efficiency, and the reliability and safety of the satellite.

Description

technical field [0001] The invention relates to a method for marking electronic load tasks of small satellites. Background technique [0002] The development cost of modern small satellites is low, the development period is short, the size is small, and the resistance to destruction is good, so it has been developed and applied rapidly. However, the orbit height of modern small satellites is generally low. Due to the constraints of ground stations and satellite conditions, each transit time is short, and the uplink remote control rate is low. The daily maintenance of the satellite platform needs to be completed within a limited time and limited uplink rate. , as well as a large amount of satellite-ground data exchange including telemetry and remote control data. At the same time, with the development of small satellite electronic payload technology, the types and quantities of electronic payloads carried on small satellites are increasing, their functions are becoming more ...

AI Technical Summary

Problems solved by technology

[0004] The technical problem of the present invention is: to overcome the deficiencies of the prior art, to provide a small satellite electronic load task injection method using a task template, and to solve the problem that the current small satellite electronic load needs to add the complete task to each task. All the package data is uploaded to the star, which leads to the problem of low efficiency

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