A control handover method for unmanned aerial vehicles based on the joint architecture of unmanned systems

A technology of control rights and unmanned aerial vehicles, applied in control/regulation systems, non-electric variable control, three-dimensional position/course control, etc., can solve problems such as direct execution of coordinated tasks, achieve important military benefits and promote application prospects , Improve reliability and ensure mission safety

Active Publication Date: 2021-08-31
CHINESE AERONAUTICAL RADIO ELECTRONICS RES INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Each UAV system is in an independent state, and even UAV systems of the same type generally do not have the ability to directly perform collaborative tasks

Method used

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  • A control handover method for unmanned aerial vehicles based on the joint architecture of unmanned systems
  • A control handover method for unmanned aerial vehicles based on the joint architecture of unmanned systems
  • A control handover method for unmanned aerial vehicles based on the joint architecture of unmanned systems

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Embodiment Construction

[0036] The specific implementation manner of the present invention will be described in detail in conjunction with the summary of the invention and the accompanying drawings.

[0037] The general architecture of unmanned systems defined by the Joint Architecture for Unmanned Systems (JAUS) adopts a hierarchical organization method and is divided into system layer, subsystem layer, node layer, and component / instance layer from top to bottom. and the service layer. A "system" is a collection of interoperable "subsystems," typically a physical entity within a system, such as an unmanned vehicle or an operator control unit. Subsystems are broken down into "nodes," which provide a complete set of processing functions, such as a computer or a motion controller. A node manages one or more "components", which generally exist in the node in the form of an application program, while a component consists of a set of "services". JAUS Topology Diagram Institute figure 1 shown.

[0038]...

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Abstract

The invention discloses a UAV control right handover method based on the joint architecture of unmanned systems. Aiming at the use requirements of the handover control of UAVs between different UAV control stations, through the research on the joint architecture of unmanned systems, Define a group of components that have nothing to do with specific applications, specify the standard interface messages for communication, and improve the interoperability between UAVs and UAV control stations. Based on the unmanned system joint architecture, design a set of UAV control transfer methods, including UAV control transfer method under normal UAV control station and UAV control under abnormal UAV control station transfer method. This method improves the interoperability of UAV systems and meets the mission requirements of UAVs taking off and landing in different places and cross-regional operations.

Description

technical field [0001] The invention belongs to unmanned system control power handover technology, and specifically relates to a method for unmanned aerial vehicle control power handover based on unmanned system joint architecture, which solves the problem of dynamic control switching of multiple unmanned aerial vehicle controllers to the unmanned aerial vehicle. Background technique [0002] With the increasingly complex combat environment, increasingly diverse combat missions, and expanding operational scope, multi-UAV cooperative mission execution has gradually become the main mode for UAVs to participate in operations. In practical applications, UAVs are often controlled by multiple control stations to complete tasks. In the Iraq War, the Predator’s mission process was as follows: it was first airlifted to the frontline, and at the frontline airport, the local UAV control station made a route plan according to the mission, controlled the UAV to take off, and reached its ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 章豪刘国梁蒋丰亦王建勇龚瑞骆斌
Owner CHINESE AERONAUTICAL RADIO ELECTRONICS RES INST
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