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An autonomously configurable aircraft control system based on embedded multitasking

A control system and aircraft technology, which is applied in the field of autonomously configurable aircraft control systems based on embedded multi-tasking, and can solve problems such as high cost and long change cycle.

Active Publication Date: 2019-06-18
SHANGHAI AEROSPACE CONTROL TECH INST
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  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0002] The spacecraft control software is the core software of the spacecraft. The traditional architecture system can only design the aircraft control software architecture according to the pre-set tasks. Once the user's requirements change, it needs to be redesigned, and a series of projects such as corresponding requirement design and testing must be carried out. changes, the change period is long, and the cost is high

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  • An autonomously configurable aircraft control system based on embedded multitasking
  • An autonomously configurable aircraft control system based on embedded multitasking
  • An autonomously configurable aircraft control system based on embedded multitasking

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[0027] In order to describe the technical content, structural features, achieved goals and effects of the present invention in detail, the following will be described in detail in conjunction with the embodiments and accompanying drawings.

[0028] see figure 1 and Table 1 to Table 3, figure 1 It writes the relationship between the 8 major modes and the 4 major segments corresponding to user needs. Table 1 describes the binding format requirements of the system; Table 2 writes an example table of binding parameters customized according to user needs; Table 3 shows the 8 major modes Relationship table with 4 major sections;

[0029] The present invention is based on the embedded multi-task autonomously configurable aircraft control software architecture system comprising the following steps:

[0030] S1, such as figure 1 The user layer divides the top-level user layer of the software input, corresponding to: mode and segment management module, according to the flight process...

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Abstract

The invention discloses an embedded structure-based multi-task autonomously-configurable aircraft control system. The system includes a top-level user layer, an intermediate functional layer and a hardware driving layer; the top-level user layer realizes the free combination management of the user layer according to user requirements through marking a flight process on the ground; the intermediatefunctional layer realizes fully-autonomous navigation, guidance attitude control and data management, autonomously generates various guidance and attitude control strategies in an on-orbit manner tosatisfy flexible autonomous control requirements; and the hardware driving layer performs function encapsulation on hardware operation in the form of an object code base, provides related hardware driving modules so that the upper layers can call the hardware driving modules.

Description

technical field [0001] The invention relates to a space vehicle control software architecture system, in particular to an embedded multi-task-based self-configurable aircraft control system. Background technique [0002] The spacecraft control software is the core software of the spacecraft. The traditional architecture system can only design the aircraft control software architecture according to the pre-set tasks. Once the user's requirements change, it needs to be redesigned, and a series of projects such as corresponding requirement design and testing must be carried out. changes, the change period is long, and the cost is high. Contents of the invention [0003] The technical problem solved by the present invention is: to overcome the deficiencies of the prior art, to provide a control system based on embedded multi-tasks that can be configured autonomously, and to provide a generalized space vehicle control software architecture design, which can be applied to differ...

Claims

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Application Information

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IPC IPC(8): G05B23/02
CPCG05B23/0221
Inventor 梁珣余薛浩黄飞姚建刘玉梅王迪
Owner SHANGHAI AEROSPACE CONTROL TECH INST
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