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Testing task implementing and operating method of testing satellite

A task execution and mission technology, applied in the field of satellite testing, can solve the problems of low efficiency and high difficulty of spaceborne testing, and achieve the effect of simplifying planning difficulty, improving efficiency, and simplifying design difficulty

Inactive Publication Date: 2011-06-01
HARBIN INST OF TECH
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0003] However, the difficulty of ground task planning in the prior art leads to low efficiency of spaceborne experiments

Method used

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  • Testing task implementing and operating method of testing satellite
  • Testing task implementing and operating method of testing satellite

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Embodiment Construction

[0016] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0017] figure 1 It is a flowchart of the test task execution and operation method of the test satellite of an embodiment of the present invention, such as figure 1 shown, it includes the following steps:

[0018] S102, sending a test task command from the ground to control the execution of the satellite test task, wherein the test task command includes the test task, the start execution time of the test task and the end execution tim...

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Abstract

The invention discloses a testing task implementing and operating method of a testing satellite, which comprises the following steps: sending a testing task command from the ground to control the implementation of a satellite testing task, wherein the testing task command comprises a testing task, the implementation starting time of the testing task and the implementation finishing time of the testing task; comparing the current satellite time with the implementation starting time of the testing task, when the current satellite time and the implementation starting time of the testing task are the same, starting to implement the testing task and recording the obtained testing data through an electronic disk; comparing the current satellite time with the implementation finishing time of the testing task, when the current satellite time and the implementation finishing time of the testing task are the same or the recording of the data storage region of the electronic disk is full, stopping implementing the testing task; and transmitting the testing data in the data storage region of the electronic disk to the ground by sending a telemetering selection command from the ground.

Description

technical field [0001] The invention relates to the field of satellite testing, in particular, to a test task execution and operation method for a test satellite. Background technique [0002] The test load is a kind of load used for application test, such as various sensors without spaceflight experience, continuous data acquisition of such sensors is required in orbit. This type of test load generally has the characteristics of small size and simple function. In order not to increase the complexity of the test load, the test load is not equipped with a dedicated data transmission system, but the on-board computer collects data and transmits the data through the downlink telemetry channel. to the ground. [0003] However, in the prior art, it is difficult to plan ground missions, resulting in low efficiency of spaceborne experiments. SUMMARY OF THE INVENTION [0004] The invention provides a test task execution and operation method for a test satellite, which is used fo...

Claims

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Application Information

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IPC IPC(8): G06F19/00
Inventor 陈健李冬柏邢雷董立珉徐国栋
Owner HARBIN INST OF TECH
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