Incremental model-based spacecraft telemetering method

A spacecraft and model technology, applied in the field of spacecraft measurement and control, can solve the problems of telemetry parameter content error, design efficiency reduction, telemetry parameter sequence (position error, etc.), achieve the effect of reducing development cost and eliminating quality accidents

Active Publication Date: 2017-02-15
BEIJING INST OF SPACECRAFT SYST ENG
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AI Technical Summary

Problems solved by technology

There are tens of thousands of telemetry parameters for large and complex spacecraft. In the process of model development, when manually writing software codes related to telemetry parameters, the workload of program writing, testing and verification is enormous.
Due to the lack of a telemetry design model compatible with the design of spaceborne telemetry software components, models in different fields provide different levels of refinement, methods, and formats for telemetry system design inputs,

Method used

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  • Incremental model-based spacecraft telemetering method

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Embodiment Construction

[0034] Such as figure 1 Shown, be the schematic diagram of the inventive method, main steps are as follows:

[0035] Step 1 is to establish the incremental telemetry design model of the spacecraft. In the present invention, the telemetry design model of the spacecraft is decomposed into three parts: the data system system model, the detailed design model, and the system integration model, so as to ensure that the design elements of the telemetry system of the spacecraft are consistent. Repeat without omission. Specific as figure 2 shown.

[0036] (1) The data system system model includes:

[0037] Spacecraft topology configuration sub-model: including terminal (Remote Terminal-RT) name, terminal code, terminal address;

[0038] Telemetry transmission frame structure sub-model: including synchronization header, master header (including version number, spacecraft identifier (SCID), virtual channel identifier (VCID), virtual channel data unit (VCDU) counter, flag field),...

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Abstract

The invention discloses an incremental model-based spacecraft telemetering method. The method comprises the steps of (1) building a spacecraft incremental telemetering design model which includes a data system model, a detail design model and a system integration model; (2) finishing related parameter design of the data system model, the detail design model and the system integration model in sequence; (3) converting the data system model, the detail design model and the system integration model after parameter design into configuration codes compilable for a computer; (4) finishing configuration code combination and providing the configuration codes for satellite-borne telemetering software components; and (5) reading the corresponding configuration codes by satellite-borne software, and finishing spacecraft telemetering data acquisition, storage, retrieval, packing, scheduling, framing, virtual channel scheduling and telemetering transmission frame generation and transmission. The method can ensure design information of a spacecraft telemetering system not to be repeated and omitted, thereby remarkably improving the design efficiency of the spacecraft telemetering system.

Description

technical field [0001] The invention belongs to the field of space vehicle measurement and control, relates to a space vehicle telemetry method, and is suitable for the space vehicle telemetry system design. Background technique [0002] The spacecraft telemetry system is an important functional part of the spacecraft, including functions such as telemetry data collection, storage, organization, scheduling, and downloading. The telemetry system plays an important role in the spacecraft field, covering the entire process of spacecraft system functional testing and on-orbit application. Therefore, a high-efficiency, zero-error telemetry system design method is a necessary prerequisite to ensure the safety and reliability of spacecraft system testing and on-orbit operation. [0003] "Small Satellite Software Telemetry Scheme and Modular Design Method" (Journal of Quantum Electronics, Vol. 21, No. 3, 2004) proposed a telemetry system design method based on modular design. Tele...

Claims

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Application Information

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IPC IPC(8): G06F17/50
CPCG06F30/20
Inventor 田志新张亚航郑国成王宇飞李小娟鲁帆孔祥皓倪辰李劲东
Owner BEIJING INST OF SPACECRAFT SYST ENG
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