Integrated unmanned aerial vehicle control system based on software bus

A technology of software bus and control system, applied in the direction of control/adjustment system, vehicle position/route/height control, non-electric variable control, etc., to achieve the effect of improving reliability, improving usability and fault tolerance

Active Publication Date: 2018-11-06
SOUTH CHINA UNIV OF TECH
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  • Abstract
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AI Technical Summary

Problems solved by technology

[0007] An integrated drone control system based on software bus, based on middleware technology and service-oriented architecture; adding an intermediate layer between the system layer and the application layer, that is, the soft bus layer, solves various problems in the complex UAV cyber-physical system architecture. Module communication, integration and configuration issues, to achieve a one-stop multi-control monitoring that integrates task assignment, route planning, control command, and process monitoring; the middleware is abstracted into a software bus that connects various components, providing standardized and reliable message transmission services , request the required data from the software bus through the standard interface, the software bus transmits messages in real-time asynchronous communication mode, and undertakes the data service of message routing, network protocol, data encoding and decoding, and message queue

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  • Integrated unmanned aerial vehicle control system based on software bus
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  • Integrated unmanned aerial vehicle control system based on software bus

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Embodiment Construction

[0030] The present invention will be described in further detail below in conjunction with the examples, but the embodiments of the present invention are not limited thereto. If there are any parts that are not specifically described in detail below, those skilled in the art can realize or understand with reference to the prior art.

[0031] An integrated UAV control system architecture based on software bus in this example, such as figure 1 As shown, the centralized management mode based on the software bus is adopted to realize the integrated control of multi-machine tasks and global resource scheduling. Main content of the present invention comprises:

[0032] 1) Integrated system architecture based on software bus

[0033] Integrated system architecture based on software bus such as figure 1 As shown, it includes UAV, sensing equipment, ground control system (bus node, computing node, bus agent), network and other parts.

[0034] bus agent. The bus agent is distributed...

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Abstract

The invention provides an integrated unmanned aerial vehicle control system based on a software bus. The system comprises a software bus-based integrated unmanned aerial vehicle control system architecture (1), a lightweight software bus communication framework (2) and a centralized software bus-based global resource management mode. Through the service-oriented system architecture, the reliability and the openness of an assembly are improved, the heterogeneity of resources are shielded, functions of the resources are packaged, and a one-stop multi-control bus control system with multiple functions integrated is designed; and a transparent data transmission mechanism is provided for a heterogeneous node, and decoupling between a user and a message protocol is realized. A multi-perspectiveglobal resource management mode for a multi-unmanned aerial vehicle system with computing resource heterogeneity and task interdependence is designed, and the real-time performance and the certainty of the control system are ensured. While the openness and the reliability of the architecture are ensured, the real-time performance of the control system and the resource utilization ratio are improved.

Description

technical field [0001] The invention relates to an integrated control system structure supporting multi-UAV control, in particular to a service-oriented UAV control system based on a software bus. Background technique [0002] The drone control system is an integrated remote control system that can be used to achieve interoperability between drone systems. But existing ground control systems have little or no versatility and interoperability. For example, the U.S. Air Force's Predator ground control system cannot monitor the Air Force's Global Hawks or the Marine Corps' Vanguard drones. At present, the relatively mature ground control systems include: the U.S. Navy's general UAV ground control system managed by the Navy's Unmanned Aerial Systems Project Office (PMA-263) and developed by Raytheon's Intelligence and Information Systems Department since 2000 - Tactical Control System (TCS), and developed a TCS core system that can operate a variety of NATO UAVs to achieve int...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/104
Inventor 张平汤峰李方谈佳
Owner SOUTH CHINA UNIV OF TECH
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