Data communication protocol controller suitable for satellite mounted equipment

A protocol controller, data communication technology, applied in the direction of data exchange, electrical components, transmission system, etc. through path configuration, can solve the problems of increasing the weight and power consumption of the spacecraft, low efficiency, etc. High efficiency and high stability

Inactive Publication Date: 2009-06-10
CENT FOR SPACE SCI & APPLIED RES
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Problems solved by technology

[0003] The purpose of the present invention is to overcome the above-mentioned existing use of software to control the circuit to generate the control signal required by the protocol. The efficiency is low, a plurality of data collectors must be set, and the defects of increasing the weight and power consumption of the spacecraft; The working efficiency and miniaturization of the device data management system, thus providing a data communication protocol controller suitable for spaceborne devices implemented by FPGA

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  • Data communication protocol controller suitable for satellite mounted equipment
  • Data communication protocol controller suitable for satellite mounted equipment
  • Data communication protocol controller suitable for satellite mounted equipment

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Embodiment Construction

[0035] The data communication protocol controller suitable for aerospace applications of the present invention will be described in detail below with reference to the drawings and specific implementation methods.

[0036] Such as figure 1 As shown, make a data communication protocol controller suitable for aerospace applications.

[0037] The control register 1 of the data communication protocol controller of this embodiment, the status register 2, the digital input timing control logic array 3, the digital output timing control array 4, the input buffer 5, the output buffer 6, and the input serial-to-parallel conversion shift register 7 and the functional modules of the output parallel-to-serial conversion shift register 8 are all implemented inside an FPGA. Among them, the control register 1 is implemented by using the basic register logic resources inside the FPGA in a manner described in VHDL. The length of the control register is 8 bits, and the working mode is synchrono...

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Abstract

The invention relates to a data communication protocol controller applicable to satellite borne equipment. The controller comprises a control register, a status register, an input cache and an output cache which are all electrically connected with an internal bus, wherein the control register 1 is in electrical connection with a digital quantity input time-sequence control logic array and a digital quantity output time-sequence control logic array through signal wires; a control signal of the digital quantity input time-sequence control logic array is in electrical connection with a serial-in shift register and an external digital quantity input channel; the serial-in shift register is in electrical connection with the input cache through an input parallel data wire; a control signal of the digital quantity output time-sequence control logic array is in electrical connection with a serial-out shift register and an external digital quantity output channel; and the serial-out shift register is in electrical connection with the output cache through a parallel output data wire. The data communication protocol controller solves the problem of automatic control on multiple communication protocols and multipath communication channels, realizes light-minimization of a data acquisition unit, and is established based on a digital logic hardware circuit, so that reliability and stability of the controller can be sufficiently guaranteed.

Description

technical field [0001] The invention relates to a data communication protocol controller, in particular to a data communication protocol controller suitable for satellite-borne equipment. Background technique [0002] In the data management system of the spacecraft, a special communication protocol is usually formulated for serial digital communication. There is a special data collector in the data management system to manage the payload unit interfaced with it according to the communication protocol. The traditional implementation method of the data collector uses software to control the external port of the CPU to generate the control signal required by the protocol, and receives or sends data under the control of the port signal. For the specific method, please refer to the synchronous communication controller based on the ISA bus in Document 1. (Chinese core journal "Microcomputer Information" (Measurement and Control Automation) 2005, Volume 21, No. 3, Synchronous Comm...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04L29/06H04L12/28
Inventor 薛长斌陈晓敏安军社周晴汪大星朱岩
Owner CENT FOR SPACE SCI & APPLIED RES
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