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No-manned machine distant control chain circuit interruption judging and processing method

A technology for link interruption and processing method, which is applied in aircraft parts, comprehensive factory control, and comprehensive factory control. Effect

Inactive Publication Date: 2009-12-09
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] From another perspective, the data link inevitably has reliability problems. If the telemetry link is interrupted, the ground personnel cannot know the status of the aircraft in real time, but the aircraft does not know that the telemetry link is interrupted, so there is nothing to do; The remote control link is interrupted, that is, the remote control command cannot be sent to the aircraft. At this time, the aircraft can know that the remote control link has been interrupted according to the received remote control data frame
Therefore, for the interruption of the remote control link, some appropriate protective and remedial measures can be taken from the perspective of flight control and management; although it is a subordinate and passive method, it is also an effective way to improve flight safety And method, is the last barrier to deal with data link interruption failure

Method used

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  • No-manned machine distant control chain circuit interruption judging and processing method
  • No-manned machine distant control chain circuit interruption judging and processing method

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Embodiment Construction

[0032] The method of the present invention will be further described in detail below in conjunction with specific embodiments.

[0033] figure 1 It is a schematic diagram of a method for judging and processing a link interruption in the present invention. Such as figure 1 As shown, according to the communication time of the remote control link, the link interruption judgment is performed, and the link status is obtained after the judgment, and then corresponding processing is performed according to the link status. If the link status is link normal, continue to judge the link interruption; if the link status is link interruption waiting, perform link interruption waiting processing; Interruption is difficult to recover; if the link status is link recovery, link interruption recovery processing will be performed.

[0034] figure 2 It is a schematic diagram of four link state transitions for link interruption judgment in the link interruption judgment and processing method ...

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Abstract

The invention provides a method for determining and processing an interruption of a remote control link for an unmanned aerial vehicle, which is applied to the flight control and management of an autonomous control type unmanned aerial vehicle. The method comprises the following four steps of a determination of the link interruption, a waiting process of the link interruption, an irreducible process of the link interruption and a recovery process of the link interruption. The method sufficiently uses the prior information to achieve the monitoring to the remote control data link; uses interconversions among the four link states and corresponding treatment measures to achieve the self-independent monitoring and management for the link state of the unmanned aerial vehicle; and uses a corresponding treatment measure according to a specific state of the unmanned aerial vehicle to effectively improve flight security and reduce risks under the circumstance that the unmanned aerial vehicle loses a ground control. The invention has an important engineering application value.

Description

technical field [0001] The invention relates to a method for judging and processing the interruption of a remote control link of an unmanned aerial vehicle, belonging to the field of automatic control of unmanned aerial vehicles. Background technique [0002] According to the functions, the UAV system is mainly composed of four parts: aircraft system, radio measurement and control system, mission equipment system, and comprehensive support system. The radio measurement and control system of the UAV is usually the UAV data link system; it can be divided into uplink and downlink according to the direction of data transmission. The uplink mainly completes the sending and receiving of remote control commands from the ground station to the UAV, which is generally called the remote control link; the downlink mainly completes the sending and receiving of telemetry data, infrared or TV images from the UAV to the ground terminal As well as the transmission of tracking and positionin...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B19/418G08C17/00B64D31/00
CPCY02P90/02
Inventor 张翠萍王宏伦舒婷婷
Owner BEIHANG UNIV