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CN116300997A - A plant protection drone and flight control system - Google Patents

A plant protection drone and flight control system Download PDF

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Publication number
CN116300997A
CN116300997A CN202310097674.7A CN202310097674A CN116300997A CN 116300997 A CN116300997 A CN 116300997A CN 202310097674 A CN202310097674 A CN 202310097674A CN 116300997 A CN116300997 A CN 116300997A
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flight
plant protection
main control
power
control unit
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程彦玮
黄晨
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Shenzhen Qingheshu Technology Co ltd
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    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10Simultaneous control of position or course in three dimensions
    • G05D1/101Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • G05D1/106Change initiated in response to external conditions, e.g. avoidance of elevated terrain or of no-fly zones
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

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  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

The invention discloses a plant protection unmanned aerial vehicle and a flight control system, which belong to the technical field of unmanned aerial vehicles and comprise an intelligent module, a power battery, a flight control module and a plurality of power modules; the intelligent module consists of an MCU main control unit, an intelligent power distribution unit and an ignition prevention unit which are integrated on the same circuit board; the MCU main control unit compares the stored second key with the stored first key of the power battery, so that potential safety hazards caused by misloading, mixed loading and unreliable installation of the power battery are avoided, meanwhile, the instantaneous current of the power battery is measured by the anti-ignition unit to protect the plant protection unmanned aerial vehicle, the power module is precharged, the safety of the plant protection unmanned aerial vehicle is guaranteed, and the MCU main control unit judges whether power failure or forced landing is needed according to flight data to protect the plant protection unmanned aerial vehicle or avoid potential safety hazards caused by paddles rotating at high speed to people.

Description

一种植保无人机以及飞行控制系统A plant protection drone and flight control system

技术领域technical field

本发明涉及一种植保无人机以及飞行控制系统,属于无人机技术领域。The invention relates to a plant protection unmanned aerial vehicle and a flight control system, belonging to the technical field of unmanned aerial vehicles.

背景技术Background technique

植保无人机,又名无人飞行器,顾名思义是用于农林植物保护作业的无人驾驶飞机,该型无人飞机由飞行平台(固定翼、直升机、多轴飞行器)、导航飞控、喷洒机构三部分组成,通过地面遥控或导航飞控,来实现喷洒作业,可以喷洒药剂、种子、粉剂等。随着无人机技术高速发展,更具广泛意义的“农业无人机”逐步替代“植保无人机”,农业无人机不仅用于喷洒施药,还能进行撒肥、撒种、撒饲料等多种工作,满足农户多样化需求,提高生产效率。Plant protection UAV, also known as unmanned aerial vehicle, as the name implies, is an unmanned aircraft used for agricultural and forestry plant protection operations. Composed of three parts, the spraying operation can be realized through ground remote control or navigation flight control, which can spray chemicals, seeds, powder, etc. With the rapid development of drone technology, "agricultural drones" with a broader meaning are gradually replacing "plant protection drones". Agricultural drones are not only used for spraying pesticides, but also for spreading fertilizers, seeds, and Feed and other work to meet the diverse needs of farmers and improve production efficiency.

参考图2,目前的植保无人机由分电板、动力电池、飞控、多个动力电池和水泵组成,动力电池向分电板提供电源,分电板将电源分流到飞控、多个动力电池和水泵,飞控控制多个动力电池和水泵,但目前市场上的植保无人机中的组件,都是没有数据互通、监测、管理,造成产品坠机问题很难分析和解决,且接线分散干扰大,可靠性低;另外动力电池直接上电冲击电流很大,对动力电池和其他组件的寿命影响很大。Referring to Figure 2, the current plant protection UAV is composed of a distribution board, a power battery, a flight controller, multiple power batteries and a water pump. The power battery provides power to the distribution board, and the distribution board shunts the power to the flight controller, multiple Power batteries and water pumps, the flight controller controls multiple power batteries and water pumps, but the components in the plant protection drones currently on the market do not have data communication, monitoring, and management, which makes it difficult to analyze and solve the problem of product crashes, and The wiring is scattered and disturbed, and the reliability is low; in addition, the direct power-on impact current of the power battery is very large, which has a great impact on the life of the power battery and other components.

发明内容Contents of the invention

针对上述提出的技术问题,本发明提供了一种植保无人机以及飞行控制系统。In view of the above-mentioned technical problems, the present invention provides a plant protection drone and a flight control system.

一种植保无人机,包括智能模块、动力电池、飞行控制模块、以及多个动力模块;A plant protection drone, including an intelligent module, a power battery, a flight control module, and multiple power modules;

智能模块由集成在同一电路板上的MCU主控单元、智能分电单元、防打火单元、信号接口单元组成;MCU主控单元通过CAN总线分别连接飞行控制模块、防打火单元、智能分电单元、动力电池、信号接口单元;The intelligent module is composed of MCU main control unit, intelligent power distribution unit, anti-sparking unit, and signal interface unit integrated on the same circuit board; the MCU main control unit is connected to the flight control module, anti-sparking unit, intelligent distribution Electric unit, power battery, signal interface unit;

动力电池,连接飞行控制模块、防打火单元以及智能分电单元,用于向MCU主控单元、飞行控制模块、防打火单元以及智能分电单元供电,以及将存储的第一密匙和故障信息通过CAN总线向MCU主控单元发送;The power battery is connected to the flight control module, anti-ignition unit and intelligent power distribution unit, and is used to supply power to the MCU main control unit, flight control module, anti-ignition unit and intelligent power distribution unit, as well as the stored first key and The fault information is sent to the MCU main control unit through the CAN bus;

防打火单元,连接全部动力模块,用于实时测量动力电池的瞬时电流,并生成电流检测结果后通过CAN总线向MCU主控单元发送;以及,对全部动力模块进行预充电处理;The anti-sparking unit is connected to all power modules for real-time measurement of the instantaneous current of the power battery, and generates current detection results and sends them to the MCU main control unit through the CAN bus; and pre-charges all power modules;

智能分电单元,连接全部动力模块,用于将动力电池提供给智能分电单元的电源分为多路,为每个动力模块单独提供一路电源;The intelligent power distribution unit is connected to all power modules, and is used to divide the power provided by the power battery to the intelligent power distribution unit into multiple channels, and provide one power supply for each power module;

飞行控制模块,连接全部动力模块,用于采集全部动力模块的飞行数据,并通过CAN总线向MCU主控单元发送飞行数据;Flight control module, connected to all power modules, used to collect flight data of all power modules, and send flight data to MCU main control unit through CAN bus;

信号接口单元,连接MCU主控单元、飞行控制模块,用于接收飞行控制模块采集的全部动力模块的飞行数据,并将飞行数据进行抗干扰处理后输出至MCU主控单元;The signal interface unit is connected to the MCU main control unit and the flight control module, and is used to receive the flight data of all power modules collected by the flight control module, and output the flight data to the MCU main control unit after anti-interference processing;

MCU主控单元,连接全部动力模块,用于接收第一密匙、故障信息、电流检测结果和飞行数据,若电流检测结果为短路或接收到故障信息,则切断MCU主控单元、飞行控制模块、防打火单元以及智能分电单元的供电,以及,用于将第一密匙与预先存储的第二密匙进行比对,若不匹配,则切断MCU主控单元、飞行控制模块、防打火单元以及智能分电单元的供电,以及,根据飞行数据与预设的飞行状态判断策略判断植保无人机是否满足正常飞行条件,若不满足正常飞行条件,且植保无人机处于未飞行阶段,则切断MCU主控单元、飞行控制模块、防打火单元以及智能分电单元的供电,若不满足正常飞行条件,且植保无人机处于飞行阶段,则生成飞行姿态调整指令,令向多个动力模块发送,多个动力模块根据飞行姿态调整至零调整植保无人机的飞行姿态使其迫降。The MCU main control unit is connected to all power modules, and is used to receive the first key, fault information, current detection results and flight data. If the current detection result is a short circuit or fault information is received, the MCU main control unit and the flight control module are cut off. , the power supply of the anti-ignition unit and the intelligent power distribution unit, and is used to compare the first key with the pre-stored second key, and if they do not match, cut off the MCU main control unit, flight control module, anti- The power supply of the ignition unit and the intelligent power distribution unit, and judging whether the plant protection drone meets the normal flight conditions according to the flight data and the preset flight status judgment strategy, if the normal flight conditions are not met, and the plant protection drone is not flying stage, cut off the power supply of the MCU main control unit, flight control module, anti-ignition unit, and intelligent power distribution unit. Multiple power modules are sent, and multiple power modules are adjusted to zero according to the flight attitude to adjust the flight attitude of the plant protection drone to make it forced to land.

对上述技术方案的进一步改进为:飞行数据包括电机及电调电压值、电机及电调电流值、电机转速、电机及电调状态。A further improvement to the above technical solution is: the flight data includes the voltage value of the motor and the ESC, the current value of the motor and the ESC, the rotational speed of the motor, and the state of the motor and the ESC.

进一步的,智能模块还包括信号接口单元;Further, the intelligent module also includes a signal interface unit;

信号接口单元,连接动力电池、MCU主控单元、飞行控制模块,用于接收飞行控制模块采集的全部动力模块的飞行数据,并将飞行数据进行抗干扰处理后输出至MCU主控单元;The signal interface unit is connected to the power battery, the MCU main control unit, and the flight control module, and is used to receive the flight data of all the power modules collected by the flight control module, and output the flight data to the MCU main control unit after anti-interference processing;

动力电池,用于向信号接口供电。The power battery is used to supply power to the signal interface.

进一步的,还包括备用电源;Further, it also includes a backup power supply;

备用电源,连接MCU主控单元,用于向MCU主控单元供电;Backup power supply, connected to the MCU main control unit, used to supply power to the MCU main control unit;

MCU主控单元,用于存储飞行数据。MCU main control unit, used to store flight data.

进一步的,还包括通讯接口,连接MCU主控单元,用于和智能终端通讯连接,实现MCU主控单元和智能终端之间飞行数据的交换。Further, it also includes a communication interface, which is connected to the MCU main control unit, and is used for communicating with the intelligent terminal, so as to realize the exchange of flight data between the MCU main control unit and the intelligent terminal.

进一步的,智能模块还包括蓝牙单元;Further, the smart module also includes a Bluetooth unit;

蓝牙单元,连接动力电池、MCU主控单元,用于使MCU主控单元与智能终端进行无线信息的交换。The Bluetooth unit is connected to the power battery and the MCU main control unit, and is used to exchange wireless information between the MCU main control unit and the smart terminal.

进一步的,飞行状态判断策略包括:Further, the flight status judgment strategy includes:

若所有动力模块处于正常工作状态,则植保无人机处于飞行阶段。If all power modules are in normal working condition, the plant protection drone is in flight.

一种植保无人机飞行控制系统,包括植保无人机,还包括智能终端以及服务器,植保无人机和智能终端均与服务器通讯连接;A plant protection UAV flight control system, including a plant protection UAV, and also includes a smart terminal and a server, and both the plant protection UAV and the smart terminal are connected to the server through communication;

其中,智能终端,用于发送起飞指令至植保无人机,植保无人机接收起飞指令,并根据起飞指令飞离地面;以及,用于发送预设飞行轨迹至植保无人机,植保无人机接收预设飞行轨迹,并按照预设飞行轨迹进行飞行,以及,用于发送洒水指令至植保无人机,植保无人机收到洒水指令,并根据洒水指令启动水泵进行洒水作业;以及,用于发送返航指令至植保无人机,植保无人机接收返航指令,根据返航指令调整飞行姿态飞回原处。Among them, the intelligent terminal is used to send the take-off command to the plant protection drone, and the plant protection drone receives the take-off command and flies off the ground according to the take-off command; and is used to send the preset flight trajectory to the plant protection drone, and the plant protection drone The machine receives the preset flight trajectory, and flies according to the preset flight trajectory, and is used to send the watering command to the plant protection drone, and the plant protection drone receives the watering command, and starts the water pump according to the watering command to perform the watering operation; and, It is used to send the return command to the plant protection drone, and the plant protection drone receives the return command, adjusts the flight attitude according to the return command and flies back to the original place.

由上述技术方案可知:本发明提供的植保无人机通过动力电池将存储的第一密匙向MCU主控单元发送,MCU主控单元接收第一密匙后,将第一密匙与预先存储的第二密匙进行比对,只有比对成功才允许植保无人机上电,来避免了动力电池的错装、混装,而导致供电回路的额定电流、电压的偏差或不稳定造成植保无人机内部各种硬件的失欠压,长期使用导致的各种无法弥补的硬件损伤,以及在使用过程中发生冒烟爆炸及烧毁植保无人机并造成人身伤害的种种危害。It can be seen from the above technical solution that the plant protection drone provided by the present invention sends the stored first key to the MCU main control unit through the power battery, and the MCU main control unit combines the first key with the pre-stored key after receiving the first key. The second key is compared with the second key. Only when the comparison is successful, the plant protection drone is allowed to be powered on. Loss and undervoltage of various hardware inside the human-machine, various irreparable hardware damages caused by long-term use, and various hazards such as smoke explosion and burning of plant protection drones during use, causing personal injury.

同时,动力电池还用于将存储的故障信息通过CAN总线向MCU主控单元发送,当植保无人机出现故障,将故障信息写入动力电池内部的可存储介质中,当MCU主控单元收到、检测到故障信息,禁止动力电池对植保无人机的供电,避免动力电池损害植保无人机,保障植保无人机的安全和使用寿命。At the same time, the power battery is also used to send the stored fault information to the MCU main control unit through the CAN bus. When the plant protection drone fails, the fault information will be written into the storable medium inside the power battery. If the fault information is detected, the power battery is prohibited from powering the plant protection drone, so as to prevent the power battery from damaging the plant protection drone and ensure the safety and service life of the plant protection drone.

同时,防打火单元,实时测量动力电池的瞬时电流,并生成电流检测结果后通过CAN总线向MCU主控单元发送;MCU主控单元接收瞬时电流后,若电流检测结果为短路,则禁止动力电池对植保无人机的供电,来保障植保无人机的安全,保障人员的安全。At the same time, the anti-ignition unit measures the instantaneous current of the power battery in real time, and generates the current detection result and sends it to the MCU main control unit through the CAN bus; after the MCU main control unit receives the instantaneous current, if the current detection result is a short circuit, the power supply is disabled. The battery supplies power to the plant protection drone to ensure the safety of the plant protection drone and the safety of personnel.

同时,防打火单元还用于对全部动力模块进行预充电处理;以减少接触器接触时火花拉弧,降低冲击,增加安全性。At the same time, the anti-ignition unit is also used to pre-charge all power modules; to reduce spark arcing when the contactor contacts, reduce impact and increase safety.

飞行控制模块还于采集全部动力模块的飞行数据,并通过CAN总线向MCU主控单元发送飞行数据,MCU主控单元收到飞行数据后,根据飞行数据与植保无人机是否处于飞行阶段,来禁止动力电池对植保无人机的供电,或者调整植保无人机的飞行姿态使其迫降,来保护植保无人机,避免高速旋转的桨叶对人造成的安全隐患。The flight control module also collects the flight data of all power modules, and sends the flight data to the MCU main control unit through the CAN bus. Prohibit the power supply of the power battery to the plant protection drone, or adjust the flight attitude of the plant protection drone to make it make a forced landing to protect the plant protection drone and avoid the safety hazards caused by the high-speed rotating blades.

附图说明Description of drawings

为了更清楚的说明本发明实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作简单的介绍,显而易见的,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其它附图。In order to more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the accompanying drawings that need to be used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the accompanying drawings in the following description are only These are some embodiments of the present invention. Those skilled in the art can also obtain other drawings based on these drawings without creative work.

图1为本发明提供的植保无人机的示意图。Fig. 1 is a schematic diagram of the plant protection drone provided by the present invention.

图2为现有技术提供的植保无人机的示意图。Fig. 2 is a schematic diagram of a plant protection drone provided by the prior art.

图3为本发明提供的植保无人机中智能模块的示意图。Fig. 3 is a schematic diagram of the intelligent module in the plant protection drone provided by the present invention.

图4为本发明提供的植保无人机的方框图。Fig. 4 is a block diagram of the plant protection drone provided by the present invention.

图5为本发明提供的植保无人机飞行控制系统的示意图。Fig. 5 is a schematic diagram of the flight control system of the plant protection drone provided by the present invention.

具体实施方式Detailed ways

下面将结合本发明中的附图,对本发明实施例中的技术方案进行清楚、完整的描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通的技术人员在没有做出创造性劳动的前提下所获得的所有其它实施例,都属于本发明的保护范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the present invention. Apparently, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

参考图1、图3和图4,一种植保无人机,包括智能模块、动力电池、飞行控制模块、以及多个动力模块;Referring to Figure 1, Figure 3 and Figure 4, a plant protection UAV includes an intelligent module, a power battery, a flight control module, and multiple power modules;

智能模块由集成在同一电路板上的MCU主控单元、智能分电单元、防打火单元、信号接口单元组成;MCU主控单元通过CAN总线分别连接飞行控制模块、防打火单元、智能分电单元、动力电池、信号接口单元;The intelligent module is composed of MCU main control unit, intelligent power distribution unit, anti-sparking unit, and signal interface unit integrated on the same circuit board; the MCU main control unit is connected to the flight control module, anti-sparking unit, intelligent distribution Electric unit, power battery, signal interface unit;

参考图1、图3和图4,动力电池,一般为蓄电池,在本发明中为植保无人机提供电源,动力电池连接飞行控制模块、防打火单元以及智能分电单元,用于向MCU主控单元、飞行控制模块、防打火单元以及智能分电单元供电;以及将存储的第一密匙向MCU主控单元发送,MCU主控单元接收第一密匙后,将第一密匙与预先存储的第二密匙进行比对,若不匹配,则禁止动力电池对植保无人机的供电,不难想到,动力电池内部设置有可存储介质,可存储介质存储有第一密匙;第一密匙和第二密匙均是植保无人机在生产阶段所设置的,分别保存在动力电池,以及与之适配的MCU主控单元中,一般而言,通过这种方式,避免了动力电池的错装、混装,而导致供电回路的额定电流、电压的偏差或不稳定造成植保无人机内部各种硬件的失欠压,长期使用导致的各种无法弥补的硬件损伤,以及在使用过程中发生冒烟爆炸及烧毁植保无人机并造成人身伤害的种种危害,动力电池还用于将存储的故障信息通过CAN总线向MCU主控单元发送,同理,故障信息也是存储在动力电池内部的可存储介质中,故障信息为后期写入的,当植保无人机出现故障,且被认定为是动力电池故障,可通过MCU主控单元,或其他方式,将故障信息写入动力电池内部的可存储介质中,此时的动力电池即为故障电池,当MCU主控单元收到、检测到故障信息,禁止动力电池对植保无人机的供电,避免动力电池损害植保无人机,保障植保无人机的安全和使用寿命。Referring to Fig. 1, Fig. 3 and Fig. 4, the power battery, generally a storage battery, provides power for the plant protection drone in the present invention, and the power battery is connected to the flight control module, the anti-ignition unit and the intelligent power distribution unit for supplying power to the MCU. The main control unit, the flight control module, the anti-ignition unit and the intelligent power distribution unit are powered; and the stored first key is sent to the MCU main control unit. After the MCU main control unit receives the first key, it sends the first key Compare it with the pre-stored second key. If it does not match, the power battery is prohibited from powering the plant protection drone. It is not difficult to imagine that the power battery is equipped with a storable medium, and the storable medium stores the first key. ; Both the first key and the second key are set during the production stage of the plant protection drone, and are respectively stored in the power battery and the MCU main control unit adapted to it. Generally speaking, in this way, It avoids the wrong installation and mixed installation of the power battery, which leads to the deviation or instability of the rated current and voltage of the power supply circuit, which leads to the loss and undervoltage of various hardware inside the plant protection drone, and various irreparable hardware damage caused by long-term use. , and various hazards such as smoke explosion and burning of plant protection drones and personal injuries during use. The power battery is also used to send the stored fault information to the MCU main control unit through the CAN bus. Similarly, the fault information is also Stored in the storable medium inside the power battery, the fault information is written later. When the plant protection drone fails and is identified as a power battery fault, the fault information can be sent to the main control unit through the MCU or other methods. Write it into the storable medium inside the power battery. At this time, the power battery is a faulty battery. When the MCU main control unit receives and detects the fault information, it prohibits the power battery from powering the plant protection drone to avoid damage to the plant protection by the power battery. UAVs ensure the safety and service life of plant protection drones.

参考图1,防打火单元,连接全部动力模块,用于实时测量动力电池的瞬时电流,并生成电流检测结果后通过CAN总线向MCU主控单元发送;MCU主控单元接收瞬时电流后,若电流检测结果为短路,则禁止动力电池对植保无人机的供电,来保障植保无人机的安全,保障人员的安全,同时,最佳方案是,还设置有备用电源,当动力电池对植保无人机的供电中断时,由备用电源来向植保无人机供电,并调整植保无人机的飞行姿态返回地面。Referring to Figure 1, the anti-ignition unit is connected to all power modules for real-time measurement of the instantaneous current of the power battery, and generates the current detection result and sends it to the MCU main control unit through the CAN bus; after the MCU main control unit receives the instantaneous current, if If the current detection result is a short circuit, the power supply of the power battery to the plant protection drone is prohibited to ensure the safety of the plant protection drone and the safety of personnel. At the same time, the best solution is to also have a backup power supply. When the power supply of the drone is interrupted, the backup power supply is used to supply power to the plant protection drone, and the flight attitude of the plant protection drone is adjusted to return to the ground.

防打火单元还用于对全部动力模块进行预充电处理;动力模块中,电源接通瞬间,电容两端的电压不会突变,而电容两端的电流会突变。那接触器会因为大电流发生粘连或损坏,影响动力模块的电机控制器的安全性和可靠性,而防打火单元的预充电处理,给大电容进行充电,以减少接触器接触时火花拉弧,降低冲击,增加安全性。The anti-sparking unit is also used to precharge all the power modules; in the power module, the moment the power is turned on, the voltage across the capacitor will not change suddenly, but the current across the capacitor will change suddenly. The contactor will be stuck or damaged due to high current, which will affect the safety and reliability of the motor controller of the power module, and the pre-charging treatment of the anti-ignition unit will charge the large capacitor to reduce sparks when the contactor is in contact. arc, reducing impact and increasing safety.

参考图1、图3和图4,智能分电单元,连接全部动力模块,用于将动力电池提供给智能分电单元的电源分为多路,为每个动力模块单独提供一路电源,智能分电单元连接动力电池,将动力电池的电压分配给不同的动力模块。Referring to Figure 1, Figure 3 and Figure 4, the intelligent power distribution unit is connected to all power modules, and is used to divide the power provided by the power battery to the intelligent power distribution unit into multiple channels, providing a separate power supply for each power module. The electric unit is connected to the power battery, and the voltage of the power battery is distributed to different power modules.

参考图1、图3和图4,飞行控制模块,连接全部动力模块,用于自动保持植保无人机的正常飞行姿态,飞行控制模块内部设置有陀螺仪,加速计,地磁感应,以及控制电路等,飞行控制模块还用于接收传来的遥控信号,责按照指令,控制电调,调度电流,让动力模块的机分别以不同的速度旋转,调整植保无人机的机姿态。Referring to Figure 1, Figure 3 and Figure 4, the flight control module is connected to all power modules to automatically maintain the normal flight attitude of the plant protection drone. The flight control module is equipped with a gyroscope, an accelerometer, a geomagnetic sensor, and a control circuit Etc., the flight control module is also used to receive the incoming remote control signal, and is responsible for controlling the ESC and dispatching the current according to the instruction, so that the machine of the power module rotates at different speeds, and adjusts the machine attitude of the plant protection drone.

飞行控制模块还于采集全部动力模块的飞行数据,并通过CAN总线向MCU主控单元发送飞行数据,飞行数据包括电机及电调电压值、电机及电调电流值、电机转速、电机及电调状态,MCU主控单元收到飞行数据后,根据飞行数据与预设的飞行状态判断策略判断植保无人机是否满足正常飞行条件,若不满足正常飞行条件,且植保无人机处于未飞行阶段,则禁止动力电池对植保无人机的供电,若不满足正常飞行条件,且植保无人机处于飞行阶段,则生成飞行姿态调整指令,令向多个动力模块发送,多个动力模块根据飞行姿态调整植保无人机的飞行姿态使其迫降。The flight control module also collects flight data of all power modules, and sends flight data to the MCU main control unit through the CAN bus. The flight data includes motor and ESC voltage values, motor and ESC current values, motor speed, motor and ESC State, after the MCU main control unit receives the flight data, it judges whether the plant protection UAV meets the normal flight conditions according to the flight data and the preset flight state judgment strategy. If it does not meet the normal flight conditions, and the plant protection UAV is not flying. , the power supply of the power battery to the plant protection drone is prohibited. If the normal flight conditions are not met and the plant protection drone is in the flight stage, a flight attitude adjustment command is generated and sent to multiple power modules. Attitude Adjust the flight attitude of the plant protection drone to make it forced to land.

参考图1、图3,信号接口单元连接动力电池、MCU主控单元、飞行控制模块,用于接收飞行控制模块采集的全部动力模块的飞行数据,并将飞行数据进行抗干扰处理后输出至MCU主控单元;信号接口单元实际上为抗干扰电路,干扰电路用于滤掉各种杂波,谐波,及干扰信号,保障飞行数据的正常传输。Referring to Figure 1 and Figure 3, the signal interface unit is connected to the power battery, the MCU main control unit, and the flight control module, and is used to receive the flight data of all power modules collected by the flight control module, and output the flight data to the MCU after anti-interference processing The main control unit and the signal interface unit are actually anti-interference circuits, which are used to filter out various clutter, harmonics, and interference signals to ensure the normal transmission of flight data.

参考图1、图3和图4,MCU主控单元,连接全部动力模块,用于接收第一密匙、故障信息、电流检测结果和飞行数据,若电流检测结果为短路或接收到故障信息,则切断MCU主控单元、飞行控制模块、防打火单元以及智能分电单元的供电,以及,用于将第一密匙与预先存储的第二密匙进行比对,若不匹配,则切断MCU主控单元、飞行控制模块、防打火单元以及智能分电单元的供电,以及,根据飞行数据与预设的飞行状态判断策略判断植保无人机是否满足正常飞行条件,若不满足正常飞行条件,且植保无人机处于未飞行阶段,则切断MCU主控单元、飞行控制模块、防打火单元以及智能分电单元的供电,若不满足正常飞行条件,且植保无人机处于飞行阶段,则生成飞行姿态调整指令,令向多个动力模块发送,多个动力模块根据飞行姿态调整至零调整植保无人机的飞行姿态使其迫降。Referring to Figure 1, Figure 3 and Figure 4, the MCU main control unit is connected to all power modules to receive the first key, fault information, current detection results and flight data. If the current detection result is short circuit or fault information is received, Then cut off the power supply of the MCU main control unit, the flight control module, the anti-ignition unit and the intelligent power distribution unit, and compare the first key with the pre-stored second key, and if they do not match, then cut off The power supply of the MCU main control unit, the flight control module, the anti-ignition unit and the intelligent power distribution unit, and, according to the flight data and the preset flight state judgment strategy, judge whether the plant protection UAV meets the normal flight conditions, and if it does not meet the normal flight conditions Conditions, and the plant protection UAV is in the non-flying stage, then cut off the power supply of the MCU main control unit, flight control module, anti-ignition unit and intelligent power distribution unit, if the normal flight conditions are not met, and the plant protection UAV is in the flight stage , the flight attitude adjustment command is generated and sent to multiple power modules, and the multiple power modules are adjusted to zero according to the flight attitude to adjust the flight attitude of the plant protection drone to make it forced to land.

在另一些实施例中,还包括备用电源;备用电源连接MCU主控单元,用于向MCU主控单元供电;备用电源可以配置为纽扣电池,保证动力电池未向MCU主控单元提供电源时,向MCU主控单元供电。In other embodiments, it also includes a backup power supply; the backup power supply is connected to the MCU main control unit, and is used to supply power to the MCU main control unit; the backup power supply can be configured as a button battery to ensure that when the power battery does not provide power to the MCU main control unit, Supply power to the MCU main control unit.

MCU主控单元内置有存储FLASH,能够不断循环记录所有飞行数据。The MCU main control unit has a built-in storage FLASH, which can continuously record all flight data in a loop.

在另一些实施例中,还包括通讯接口,通讯接口连接MCU主控单元,用于和智能终端通讯连接,实现MCU主控单元和智能终端之间飞行数据的交换,通讯接口可以为TYPC接口。In some other embodiments, it also includes a communication interface, the communication interface is connected to the MCU main control unit, and is used to communicate with the intelligent terminal to realize the exchange of flight data between the MCU main control unit and the intelligent terminal. The communication interface can be a TYPC interface.

参考图1、图3,在另一些实施例中,智能模块还包括蓝牙单元;蓝牙单元连接动力电池、MCU主控单元,用于使MCU主控单元与智能终端进行无线信息的交换。Referring to Fig. 1 and Fig. 3, in some other embodiments, the smart module further includes a Bluetooth unit; the Bluetooth unit is connected to the power battery and the MCU main control unit, and is used for exchanging wireless information between the MCU main control unit and the smart terminal.

可以通过TYPC接口电脑或手机APP查看飞行数据,用于历史故障分析和飞行数据分析,大大提高了分析和解决问题的能力The flight data can be viewed through the TYPC interface computer or mobile APP for historical fault analysis and flight data analysis, which greatly improves the ability to analyze and solve problems

飞行状态判断策略包括:若所有动力模块处于正常工作状态,则植保无人机处于飞行阶段。The flight state judgment strategy includes: if all power modules are in normal working state, the plant protection UAV is in the flight stage.

一种植保无人机飞行控制系统,包括植保无人机,还包括智能终端以及服务器,植保无人机和智能终端均与服务器通讯连接;A plant protection UAV flight control system, including a plant protection UAV, and also includes a smart terminal and a server, and both the plant protection UAV and the smart terminal are connected to the server through communication;

其中,智能终端,用于发送起飞指令至植保无人机,植保无人机接收起飞指令,并根据起飞指令飞离地面;以及,用于发送预设飞行轨迹至植保无人机,植保无人机接收预设飞行轨迹,并按照预设飞行轨迹进行飞行,以及,用于发送洒水指令至植保无人机,植保无人机收到洒水指令,并根据洒水指令启动水泵进行洒水作业;以及,用于发送返航指令至植保无人机,植保无人机接收返航指令,根据返航指令调整飞行姿态飞回原处。Among them, the intelligent terminal is used to send the take-off command to the plant protection drone, and the plant protection drone receives the take-off command and flies off the ground according to the take-off command; and is used to send the preset flight trajectory to the plant protection drone, and the plant protection drone The machine receives the preset flight trajectory, and flies according to the preset flight trajectory, and is used to send the watering command to the plant protection drone, and the plant protection drone receives the watering command, and starts the water pump according to the watering command to perform the watering operation; and, It is used to send the return command to the plant protection drone, and the plant protection drone receives the return command, adjusts the flight attitude according to the return command and flies back to the original place.

以上借助具体实施例对本发明做了进一步描述,但是应该理解的是,这里具体的描述,不应理解为对本发明的实质和范围的限定,本领域内的普通技术人员在阅读本说明书后对上述实施例做出的各种修改,都属于本发明所保护的范围。The present invention has been further described above with the help of specific embodiments, but it should be understood that the specific description herein should not be construed as limiting the spirit and scope of the present invention. Various modifications made in the embodiments all belong to the protection scope of the present invention.

Claims (7)

1.一种植保无人机,其特征在于,包括智能模块、动力电池、飞行控制模块、以及多个动力模块;1. A plant protection unmanned aerial vehicle, characterized in that it includes an intelligent module, a power battery, a flight control module, and a plurality of power modules; 所述智能模块由集成在同一电路板上的MCU主控单元、智能分电单元、防打火单元、信号接口单元组成;所述MCU主控单元通过CAN总线分别连接所述飞行控制模块、所述防打火单元、所述智能分电单元、所述动力电池、所述信号接口单元;The intelligent module is composed of an MCU main control unit, an intelligent power distribution unit, an anti-ignition unit, and a signal interface unit integrated on the same circuit board; the MCU main control unit is respectively connected to the flight control module, the The anti-ignition unit, the intelligent power distribution unit, the power battery, and the signal interface unit; 所述动力电池,连接所述飞行控制模块、所述防打火单元、所述信号接口单元以及所述智能分电单元,用于向所述MCU主控单元、所述飞行控制模块、所述防打火单元、所述信号接口单元以及所述智能分电单元供电,以及将存储的第一密匙和故障信息通过所述CAN总线向所述MCU主控单元发送;The power battery is connected to the flight control module, the anti-ignition unit, the signal interface unit and the intelligent power distribution unit, and is used to provide power to the MCU main control unit, the flight control module, the The anti-ignition unit, the signal interface unit and the intelligent power distribution unit supply power, and send the stored first key and fault information to the MCU main control unit through the CAN bus; 所述防打火单元,连接全部所述动力模块,用于实时测量所述动力电池的瞬时电流,并生成电流检测结果后通过所述CAN总线向所述MCU主控单元发送;以及,对全部所述动力模块进行预充电处理;The anti-sparking unit is connected to all the power modules, and is used to measure the instantaneous current of the power battery in real time, and generate a current detection result and send it to the MCU main control unit through the CAN bus; and, for all The power module is pre-charged; 所述智能分电单元,连接全部所述动力模块,用于将所述动力电池提供给所述智能分电单元的电源分为多路,为每个所述动力模块单独提供一路电源;The intelligent power distribution unit is connected to all the power modules, and is used to divide the power provided by the power battery to the intelligent power distribution unit into multiple channels, and provide one power supply for each of the power modules; 所述飞行控制模块,连接全部所述动力模块,用于采集全部所述动力模块的飞行数据,并通过所述CAN总线向所述MCU主控单元发送所述飞行数据;The flight control module is connected to all the power modules, and is used to collect flight data of all the power modules, and send the flight data to the MCU main control unit through the CAN bus; 所述信号接口单元,连接所述MCU主控单元、所述飞行控制模块,用于接收所述飞行控制模块采集的全部所述动力模块的所述飞行数据,并将所述飞行数据进行抗干扰处理后输出至所述MCU主控单元;The signal interface unit is connected to the MCU main control unit and the flight control module, and is used to receive the flight data of all the power modules collected by the flight control module, and perform anti-interference on the flight data output to the MCU main control unit after processing; 所述MCU主控单元,连接全部所述动力模块,用于接收所述第一密匙、所述故障信息、所述电流检测结果和所述飞行数据,若所述电流检测结果为短路或接收到故障信息,则切断所述MCU主控单元、所述飞行控制模块、所述防打火单元以及所述智能分电单元的供电,以及,用于将所述第一密匙与预先存储的第二密匙进行比对,若不匹配,则切断所述MCU主控单元、所述飞行控制模块、所述防打火单元以及所述智能分电单元的供电,以及,根据所述飞行数据与预设的飞行状态判断策略判断所述植保无人机是否满足正常飞行条件,若不满足所述正常飞行条件,且所述植保无人机处于未飞行阶段,则切断所述MCU主控单元、所述飞行控制模块、所述防打火单元以及所述智能分电单元的供电,若不满足所述正常飞行条件,且所述植保无人机处于飞行阶段,则生成飞行姿态调整指令,令向多个所述动力模块发送,多个所述动力模块根据所述飞行姿态调整至零调整所述植保无人机的飞行姿态使其迫降。The MCU main control unit is connected to all the power modules, and is used to receive the first key, the fault information, the current detection result and the flight data, if the current detection result is a short circuit or receive If fault information is received, then cut off the power supply of the MCU main control unit, the flight control module, the anti-ignition unit and the intelligent power distribution unit, and use the first encryption key with the pre-stored The second key is compared, if they do not match, then cut off the power supply of the MCU main control unit, the flight control module, the anti-ignition unit and the intelligent power distribution unit, and, according to the flight data Judging whether the plant protection UAV meets the normal flight conditions with the preset flight state judgment strategy, if the normal flight conditions are not met, and the plant protection UAV is in the non-flying stage, then cut off the MCU main control unit , if the power supply of the flight control module, the anti-ignition unit and the intelligent power distribution unit does not meet the normal flight conditions, and the plant protection drone is in the flight stage, then generate a flight attitude adjustment command, The order is sent to a plurality of the power modules, and the plurality of the power modules are adjusted to zero according to the flight attitude to adjust the flight attitude of the plant protection drone to make it forced to land. 2.如权利要求1所述的植保无人机,其特征在于,所述飞行数据包括电机及电调电压值、电机及电调电流值、电机转速、电机及电调状态。2. The plant protection unmanned aerial vehicle according to claim 1, wherein the flight data includes motor and ESC voltage value, motor and ESC current value, motor speed, motor and ESC status. 3.如权利要求1所述的植保无人机,其特征在于,还包括备用电源;3. The plant protection drone according to claim 1, further comprising a backup power supply; 所述备用电源,连接所述MCU主控单元,用于向所述MCU主控单元供电;The backup power supply is connected to the MCU main control unit for supplying power to the MCU main control unit; 所述MCU主控单元,用于存储所述飞行数据。The MCU main control unit is used to store the flight data. 4.如权利要求3所述的植保无人机,其特征在于,还包括通讯接口,连接所述MCU主控单元,用于和所述智能终端通讯连接,实现所述MCU主控单元和所述智能终端之间所述飞行数据的交换。4. The plant protection unmanned aerial vehicle as claimed in claim 3, characterized in that, it also includes a communication interface connected to the MCU main control unit for communicating with the intelligent terminal to realize the communication between the MCU main control unit and the MCU main control unit. exchange of the flight data between the smart terminals. 5.如权利要求1所述的植保无人机,其特征在于,所述智能模块还包括蓝牙单元;5. The plant protection unmanned aerial vehicle as claimed in claim 1, wherein said smart module also includes a bluetooth unit; 所述蓝牙单元,连接所述动力电池、所述MCU主控单元,用于使所述MCU主控单元与智能终端进行无线信息的交换。The bluetooth unit is connected to the power battery and the MCU main control unit, and is used for exchanging wireless information between the MCU main control unit and the smart terminal. 6.如权利要求1所述的植保无人机,其特征在于,所述飞行状态判断策略包括:6. plant protection unmanned aerial vehicle as claimed in claim 1, is characterized in that, described flight state judging strategy comprises: 若所有所述动力模块处于正常工作状态,则所述植保无人机处于飞行阶段。If all the power modules are in normal working condition, the plant protection drone is in flight. 7.一种植保无人机飞行控制系统,其特征在于,包括权利要求1至7任一项的所述植保无人机,还包括智能终端以及服务器,所述植保无人机和所述智能终端均与所述服务器通讯连接;7. A plant protection UAV flight control system, characterized in that, comprising the plant protection UAV according to any one of claims 1 to 7, also comprising an intelligent terminal and a server, the plant protection UAV and the intelligent The terminals are all communicated with the server; 其中,所述智能终端,用于发送起飞指令至所述植保无人机,所述植保无人机接收所述起飞指令,并根据所述起飞指令飞离地面;以及,用于发送预设飞行轨迹至所述植保无人机,所述植保无人机接收所述预设飞行轨迹,并按照所述预设飞行轨迹进行飞行;以及,用于发送洒水指令至所述植保无人机,所述植保无人机收到所述洒水指令,并根据所述洒水指令启动水泵进行洒水作业;以及,用于发送返航指令至所述植保无人机,所述植保无人机接收所述返航指令,根据所述返航指令调整飞行姿态飞回原处。Wherein, the intelligent terminal is used to send a take-off command to the plant protection drone, and the plant protection drone receives the take-off command and flies off the ground according to the take-off command; and is used to send a preset flight trajectory to the plant protection UAV, the plant protection UAV receives the preset flight trajectory, and flies according to the preset flight trajectory; and, for sending watering instructions to the plant protection UAV, the The plant protection UAV receives the watering instruction, and starts the water pump according to the watering instruction to perform the watering operation; and, is used to send a return instruction to the plant protection UAV, and the plant protection UAV receives the return instruction , adjust the flight attitude according to the return instruction and fly back to the original place.
CN202310097674.7A 2023-02-10 2023-02-10 A plant protection drone and flight control system Pending CN116300997A (en)

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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN206195445U (en) * 2016-11-29 2017-05-24 合肥赛为智能有限公司 Many rotors plant protection unmanned aerial vehicle power supply system and many rotors plant protection unmanned aerial vehicle thereof
CN108803654A (en) * 2018-06-04 2018-11-13 成都天麒科技有限公司 A kind of unmanned plane safe starting method
CN109383825A (en) * 2017-08-11 2019-02-26 菜鸟智能物流控股有限公司 aircraft
CN109921108A (en) * 2019-02-26 2019-06-21 深圳飞马机器人科技有限公司 Unmanned plane battery data management method and system
CN111431245A (en) * 2020-05-14 2020-07-17 广州极飞科技有限公司 Load matching system, method and load

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN206195445U (en) * 2016-11-29 2017-05-24 合肥赛为智能有限公司 Many rotors plant protection unmanned aerial vehicle power supply system and many rotors plant protection unmanned aerial vehicle thereof
CN109383825A (en) * 2017-08-11 2019-02-26 菜鸟智能物流控股有限公司 aircraft
CN108803654A (en) * 2018-06-04 2018-11-13 成都天麒科技有限公司 A kind of unmanned plane safe starting method
CN109921108A (en) * 2019-02-26 2019-06-21 深圳飞马机器人科技有限公司 Unmanned plane battery data management method and system
CN111431245A (en) * 2020-05-14 2020-07-17 广州极飞科技有限公司 Load matching system, method and load

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