A Centralized Bus Sequence Control Method Based on Time Slice Planning

Abstract

The invention discloses a centralized bus timing control method based on time slice planning. The method comprises the following steps: a step of sending a fast frame message to an ADU on a comprehensive satellite electronic system; a step of reading closed loop feedback data sent back by the ADU from a BC message stack after delaying for 1.6ms; a step of sending message frames of a type A and or message frames a type B according to 64ms cycle count CNT1 and 448ms cycle count CNT2; a step of reading telemeasuring data sent back a RT from a BC message stack within a next control period; and a step of performing bus fault judgment by using CMU software within each control period, judging a bus communication state of BC and RT according to a RT message state character, and switching from a bus A to a bus B. According to the centralized bus timing control method disclosed by the invention, the bus operation is strictly controlled within one control period, thereby avoiding temporary message frame reception and transmission caused by emergency, improving the communication instantaneity of the system, reducing the bus load and ensuring the predictability of the operation state of the system.

Description

technical field [0001] The invention relates to a centralized bus sequence control method based on time slice planning, belongs to the field of embedded software, and is suitable for communication architecture design of integrated electronic system satellite-borne application software. Background technique [0002] In the spacecraft (satellite or spacecraft) 1553B bus network, the central control computer acts as a bus controller (BC) to initiate data communication, and other stand-alone computers act as remote terminals (RT) to respond to data commands and answer. In the traditional spacecraft bus communication design, the event-based bus message frame transmission method is mainly used. This method has two limitations: 1) The real-time performance is not strong. BC sends message frames to RT triggered by events. The creation, sending and receiving of data is obviously aperiodic. For messages of different lengths, the difference in transmission time will lead to a decrease ...

AI Technical Summary

Problems solved by technology

In the traditional spacecraft bus communication design, the event-based bus message frame transmission method is mainly used. This method has two limitations: 1) The real-time performance is not strong

BC initiates a message frame to RT triggered by an event. The creation, sending and receiving of data is obviously aperiodic. For messages of different lengths, the difference in transmission time will lead to a decrease in real-time performance of the system.

2) System behavior is unpredictable

The central control calculation reads the input, and the output control instructions are realized through the 1553B bus message. If the message communication is not created, sent and received according to a fixed time point, the execution time from input to output during the program running will be uncertain. , the operating state of the system will also become unpredictable due to the "chain reaction"

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