CN106530839A - Unmanned aerial vehicle assembly line type takeoff and landing method based on double ground stations - Google Patents
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Abstract
本发明公开了一种基于双地面站的无人机流水线式起降方法,属于无人机指挥自动化技术领域。具体步骤如下:1)地面站A控制第一架无人机执行起飞过程中的步骤d至步骤g;2)当地面站A控制第一架无人机完成步骤g时,地面站B控制第二架无人机完成步骤e,准备起飞检查;3)地面站A控制第一架无人机完成起飞至安全区域后,去执行控制第三架无人机执行起飞;4)地面站B控制第二架无人机完成起飞至安全区域后,去执行控制第四架无人机执行起飞;后续的无人机起飞,重复上述步骤一至步骤四;完成多个无人机的流水线式起飞;降低集结等待时间,提高编队执行任务的响应实时性及编队执行任务的航程、航时。
The invention discloses an assembly line take-off and landing method for an unmanned aerial vehicle based on dual ground stations, and belongs to the technical field of unmanned aerial vehicle command automation. The specific steps are as follows: 1) Ground station A controls the first UAV to perform step d to step g during the take-off process; 2) When ground station A controls the first UAV to complete step g, ground station B controls the first UAV to complete step g. The two UAVs complete step e and are ready for take-off inspection; 3) Ground station A controls the first UAV to take off to a safe area, then executes and controls the third UAV to perform take-off; 4) Ground station B controls After the second UAV takes off to a safe area, execute and control the fourth UAV to take off; for subsequent UAVs to take off, repeat the above steps 1 to 4; complete the assembly line takeoff of multiple UAVs; Reduce the assembly waiting time, improve the real-time response of the formation to perform tasks and the range and flight time of the formation to perform tasks.
Description
技术领域technical field
本发明属于无人机指挥自动化技术领域,具体涉及一种基于双地面站的无人机流水线式起降方法。The invention belongs to the technical field of unmanned aerial vehicle command automation, and in particular relates to an assembly line take-off and landing method for unmanned aerial vehicles based on dual ground stations.
背景技术Background technique
无人机具有费效比低、零伤亡和部署灵活等优点,可以帮助甚至代替人类在很多场景发挥作用,无论在民用领域还是军用领域,无人机均有着广阔的应用和发展前景。UAVs have the advantages of low cost-effectiveness, zero casualties, and flexible deployment. They can help or even replace humans in many scenarios. No matter in the civilian or military fields, UAVs have broad application and development prospects.
由于单个无人机的载荷有限,在应对广阔的任务区域以及单个无人机故障后将无法完成任务的不利因素,这就使得利用无人机间的协作以执行更为复杂任务的要求逐渐成为无人机研究的趋势。通过混合编队方式对多架无人机进行编队执行不同或单一任务,以保证能够完成一个或多个任务。Due to the limited load of a single UAV, the unfavorable factors of dealing with a wide mission area and the failure of a single UAV to complete the task, this makes the use of cooperation among UAVs to perform more complex tasks. Trends in drone research. Multiple UAVs are formed to perform different or single tasks through mixed formation to ensure that one or more tasks can be completed.
现在无人机执行任务仍需地面站控制,尤其是起降阶段,需要地面站实时监控。目前无人机执行编队任务时,利用单个地面站监控飞机起降。以起飞为例,地面站监控前一架飞机从停机坪驶出至飞至安全区域后才能监控下一架飞机重复上述过程,先前起飞的飞机需在集结区域等待,随着编队飞机的数量增加,集结等待的时间也变长,影响任务响应实时性;同时,等待时间变长也使飞机编队执行任务的航程、航时缩短。而且,如果在编队起飞过程中单架飞机出现特情,会影响后续飞机出动,降落过程中单架飞机出现特情也会影响后续飞机降落,甚至可能导致灾难性后果。At present, UAVs still need to be controlled by the ground station to perform tasks, especially during the take-off and landing phase, which requires real-time monitoring by the ground station. At present, when UAVs perform formation tasks, a single ground station is used to monitor aircraft takeoff and landing. Taking take-off as an example, the ground station monitors the previous aircraft from the apron until it flies to a safe area before monitoring the next aircraft to repeat the above process. The aircraft that took off previously need to wait in the assembly area. As the number of formation aircraft increases , the waiting time for assembly becomes longer, which affects the real-time response of the task; at the same time, the longer waiting time also shortens the flight range and flight time of the aircraft formation to perform the task. Moreover, if a single aircraft has a special situation during the formation take-off process, it will affect the dispatch of subsequent aircraft, and a single aircraft’s special situation during the landing process will also affect the landing of subsequent aircraft, and may even lead to disastrous consequences.
发明内容Contents of the invention
本发明的目的:为了解决上述问题,本发明提出了一种双地面站的无人机流水线式起降方法,采用了双地面站分别控制多个无人机流水线式起降,以降低无人机集结等待时间,提高编队执行任务的响应实时性及编队执行任务的航程、航时。Purpose of the present invention: In order to solve the above-mentioned problems, the present invention proposes a method for take-off and landing of unmanned aerial vehicles with two ground stations. The waiting time for aircraft assembly is reduced, and the real-time response of the formation to perform tasks and the range and flight time of the formation to perform tasks are improved.
本发明的技术方案:一种基于双地面站的无人机流水线式起降方法,其中,无人机起飞过程包括以下步骤:The technical solution of the present invention: an assembly line take-off and landing method for unmanned aerial vehicle based on dual ground stations, wherein the take-off process of the unmanned aerial vehicle includes the following steps:
a)填充加挂:耗时T1,占用机棚;a) Filling and hanging: time-consuming T1, occupying the machine shed;
b)静检:耗时T2,占用机棚;b) Static inspection: time-consuming T2, occupying the hangar;
c)动检:耗时T3,占用机棚;c) Motion detection: time-consuming T3, occupying the machine shed;
d)从机棚滑至滑行道起点:耗时T4,占用停机坪;d) Slide from the hangar to the starting point of the taxiway: time-consuming T4, occupying the apron;
e)从滑行道起点滑行至起飞线:耗时T5,占用滑行道;e) Taxiing from the starting point of the taxiway to the take-off line: time-consuming T5, occupying the taxiway;
f)起飞前检查:耗时T6,占用跑道;f) Pre-take-off inspection: time-consuming T6, occupying the runway;
g)滑跑起飞至安全区域:耗时T7,占用场站空域;g) Rolling and taking off to a safe area: Time-consuming T7, occupying the airspace of the station;
通过设置的地面站A、地面站B分别控制多个无人机流水线式完成起降;Through the set ground station A and ground station B, respectively control multiple UAVs to complete take-off and landing in an assembly line;
所述基于双地面站的无人机流水线式起降方法控制无人机起飞包括以下步骤:The method for taking off and landing of the unmanned aerial vehicle based on two ground stations to control the unmanned aerial vehicle to take off comprises the following steps:
步骤一、所述地面站A控制第一架无人机执行所述起飞过程中的步骤d至步骤g;Step 1. The ground station A controls the first UAV to perform steps d to g in the take-off process;
步骤二、当地面站A控制第二架无人机完成步骤g时,所述地面站B控制无人机完成步骤e,准备起飞检查;Step 2. When the ground station A controls the second UAV to complete step g, the ground station B controls the UAV to complete step e and prepare for take-off inspection;
步骤三、所述地面站A控制第一架无人机完成起飞至安全区域后,去执行控制第三架无人机执行起飞;Step 3. After the ground station A controls the first UAV to take off to a safe area, it executes and controls the third UAV to take off;
步骤四、所述地面站B控制第二架无人机完成起飞至安全区域后,去执行控制第四架无人机执行起飞;Step 4. After the ground station B controls the second UAV to complete take-off to a safe area, it executes and controls the fourth UAV to perform take-off;
步骤五、后续的无人机起飞,重复上述步骤一至步骤四;完成多个无人机的流水线式起飞。Step 5. For the subsequent UAV take-off, repeat the above steps 1 to 4; complete the pipelined take-off of multiple UAVs.
优选地,所述步骤二中,所述地面站B待所述地面站A的第一架飞机出动△T时刻后控制第二架飞机出动,同理,所述步骤三中,所述地面站A待所述地面站B的第二架飞机出动△T时刻后控制第三架飞机出动,△T=(T4+T5+T6+T7)-(T4+T5)=T6+T7。Preferably, in the step 2, the ground station B controls the dispatch of the second plane after the first plane of the ground station A is dispatched at a time ΔT. Similarly, in the step 3, the ground station A A controls the third aircraft to dispatch after the second aircraft of the ground station B dispatches ΔT time, ΔT=(T4+T5+T6+T7)-(T4+T5)=T6+T7.
优选地,所述基于双地面站的无人机流水线式起降方法控制无人机降落步骤与所述基于双地面站的无人机流水线式起降方法控制无人机起飞步骤相反。Preferably, the step of controlling the landing of the UAV based on the pipelined take-off and landing method of the UAV based on the dual ground stations is opposite to the step of controlling the take-off of the UAV based on the pipelined take-off and landing method of the UAV based on the dual ground stations.
本发明技术有益效果:本发明采用双地面站控制无人机流水线式起降的方案,可大幅减少飞机集结等待时间,实现快速出动,具体优点如下:Beneficial effects of the technology of the present invention: the present invention adopts the scheme of dual ground stations to control the take-off and landing of the unmanned aerial vehicle assembly line, which can greatly reduce the waiting time for aircraft assembly and realize rapid deployment. The specific advantages are as follows:
1)大幅缩短飞机编队集结等待时间,实现快速出动;1) Significantly shorten the waiting time for aircraft formation assembly and achieve rapid dispatch;
2)提高编队执行任务的航程、航时;2) Improve the voyage and flight time of the task formation;
3)起飞过程若某架飞机出现特情,不影响其他飞机出动;3) If a certain aircraft has a special situation during take-off, it will not affect the dispatch of other aircraft;
4)降落过程若某架飞机出现特情,不影响其他飞机降落,提高系统安全性。4) If a certain aircraft has a special situation during the landing process, it will not affect the landing of other aircraft, which improves the safety of the system.
附图说明Description of drawings
图1为本发明一种基于双地面站的无人机流水线式起降方法控制单机起飞的一优选实施例的流程示意图。Fig. 1 is a schematic flow chart of a preferred embodiment of a pipelined take-off and landing method for unmanned aerial vehicles based on dual ground stations of the present invention to control a single take-off.
图2为本发明一种基于双地面站的无人机流水线式起降方法控制多机起飞的一优选实施例的流程示意图。Fig. 2 is a schematic flow chart of a preferred embodiment of a pipelined take-off and landing method for unmanned aerial vehicles based on dual ground stations to control multi-aircraft take-off according to the present invention.
图3为本发明一种基于双地面站的无人机流水线式起降方法控制多机起飞的一优选实施例的地面站A、地面站B分别控制无人机示意图。Fig. 3 is a schematic diagram of ground station A and ground station B respectively controlling unmanned aerial vehicles in a preferred embodiment of a pipelined takeoff and landing method for unmanned aerial vehicles based on dual ground stations to control multi-aircraft takeoff in the present invention.
具体实施方式detailed description
为使本发明实施的目的、技术方案和优点更加清楚,下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行更加详细的描述。在附图中,自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。所描述的实施例是本发明一部分实施例,而不是全部的实施例。下面通过参考附图描述的实施例是示例性的,旨在用于解释本发明,而不能理解为对本发明的限制。基于本发明中的实施例,本领域普通技术人员在没有作出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。下面结合附图对本发明的实施例进行详细说明。In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings.
在本发明的描述中,需要理解的是,术语“中心”、“纵向”、“横向”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”“内”、“外”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明保护范围的限制。In describing the present invention, it is to be understood that the terms "central", "longitudinal", "transverse", "front", "rear", "left", "right", "vertical", "horizontal", The orientations or positional relationships indicated by "top", "bottom", "inner", "outer", etc. are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying the Means that a device or element must have a specific orientation, be constructed and operate in a specific orientation, and therefore should not be construed as limiting the scope of the invention.
下面结合附图对本发明的实施例进行详细说明,请参照图1至图3;Embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings, please refer to Figures 1 to 3;
一种基于双地面站的无人机流水线式起降方法,通过设置的地面站A、地面站B分别控制多个无人机流水线式完成起降;以无人机起飞过程为例,无人机起飞的流程包括以下步骤:A pipeline-type take-off and landing method for UAVs based on dual ground stations. The set-up ground station A and ground station B respectively control multiple UAVs to complete the take-off and landing in a pipeline; taking the UAV take-off process as an example, no one The flight process includes the following steps:
a)填充加挂:耗时T1,占用机棚;a) Filling and hanging: time-consuming T1, occupying the machine shed;
b)静检:耗时T2,占用机棚;b) Static inspection: time-consuming T2, occupying the hangar;
c)动检:耗时T3,占用机棚;c) Motion detection: time-consuming T3, occupying the machine shed;
d)从机棚滑至滑行道起点:耗时T4,占用停机坪;d) Slide from the hangar to the starting point of the taxiway: time-consuming T4, occupying the apron;
e)从滑行道起点滑行至起飞线:耗时T5,占用滑行道;e) Taxiing from the starting point of the taxiway to the take-off line: time-consuming T5, occupying the taxiway;
f)起飞前检查:耗时T6,占用跑道;f) Pre-take-off inspection: time-consuming T6, occupying the runway;
g)滑跑起飞至安全区域:耗时T7,占用场站空域。g) Rolling takeoff to a safe area: Time-consuming T7, occupying the airspace of the station.
上述流程中,填充加挂、静检、动检过程不需要地面站参与;后续流程步骤d至步骤g均需要地面站监控,待无人机到达安全区域后,无人机交付任务站控制占空,不再属于地面站控制范围。In the above process, the process of filling and hanging, static inspection, and dynamic inspection does not require the participation of the ground station; the follow-up process steps d to steps g all require ground station monitoring. After the UAV reaches the safe area, the UAV will be delivered to the task station to control empty, no longer within the control range of the ground station.
因此本发明基于双地面站的无人机流水线式起降方法的适用阶段起点为无人机从机棚开始驶出,终点为飞至安全区域高度。Therefore, the starting point of the application stage of the pipeline type take-off and landing method of the UAV based on the dual ground stations of the present invention is that the UAV begins to drive out from the hangar, and the end point is to fly to the height of the safe area.
在机场跑道附近布置两套地面站A、B控制飞机起降,实现跑道、空域及滑行道的流水线调度,最大限度利用有限的场站资源。以某型无人机起飞为例,具体的实施例步骤如下:Arrange two sets of ground stations A and B near the airport runway to control aircraft takeoff and landing, realize the assembly line scheduling of the runway, airspace and taxiway, and maximize the use of limited station resources. Taking a certain type of unmanned aerial vehicle as an example, the specific implementation steps are as follows:
步骤一、所述地面站A控制第一架无人机执行所述起飞过程中的步骤d(从机棚滑至滑行道起点)至步骤g(滑跑起飞至安全区域)。Step 1. The ground station A controls the first UAV to perform steps d (sliding from the hangar to the starting point of the taxiway) to step g (sliding to a safe area) during the take-off process.
步骤二、当地面站A控制第二架无人机时,为实现对跑道资源的充分利用,当第一架飞机飞至安全区域后,此时所述地面站B控制无人机滑行至起飞线,准备起飞检查;根据第一架无人机飞至安全区域的时间反推第二架无人机出动时间,为△T=(T4+T5+T6+T7)-(T4+T5)=T6+T7,即第一架飞机出动△T时刻后地面站B控制第二架无人机出动。Step 2. When the ground station A controls the second drone, in order to fully utilize the runway resources, after the first plane flies to the safe area, the ground station B controls the drone to taxi to take-off Line, ready for take-off inspection; according to the time when the first UAV flies to the safe area, the second UAV dispatch time is deduced as △T=(T4+T5+T6+T7)-(T4+T5)= T6+T7, that is, the ground station B controls the second UAV to dispatch after the moment △T of the first aircraft dispatch.
步骤三、所述地面站A控制第一架无人机完成起飞至安全区域后,转去控制第三架飞机,同样,利用第二架飞机飞至安全区域时间反推第三架飞机出动时间,同样为第二架飞机出动△T时刻后地面站A控制第三架出动。Step 3. After the ground station A controls the first UAV to take off to the safe area, it turns to control the third aircraft. Similarly, use the time when the second aircraft flies to the safe area to reverse the dispatch time of the third aircraft , also the ground station A controls the dispatch of the third plane after the time △T of the dispatch of the second plane.
步骤四、地面站B控制第二架飞机飞至安全区域后,转去控制第四架飞机,重复上述过程,第四架飞机在第三架飞机出动△T时刻后出动。Step 4. After the ground station B controls the second aircraft to fly to the safe area, it turns to control the fourth aircraft and repeats the above process. The fourth aircraft is dispatched after the third aircraft dispatches at time △T.
步骤五、后续的无人机起飞,重复上述过程,由双地面站轮值完成多个无人机的流水线式起飞。Step 5. For subsequent UAV take-off, repeat the above process, and the dual ground stations will take turns to complete the assembly-line takeoff of multiple UAVs.
所述基于双地面站的无人机流水线式起降方法控制无人机降落步骤与所述基于双地面站的无人机流水线式起降方法控制无人机起飞步骤相反。The step of controlling the landing of the UAV based on the pipelined take-off and landing method of the UAV based on the dual ground stations is opposite to the step of controlling the take-off of the UAV based on the pipelined take-off and landing method of the UAV based on the dual ground stations.
当出动N(N为偶数)架无人机时,如果以单个地面站控制无人机起飞,出动共需花费时间Tsig=N·(T4+T5+T6+T7),如果以双地面站监控无人机起飞,出动共需花费时间Tdou=(T4+T5+T6+T7)+(N-1)·(T6+T7),因此出动N架无人机时共节省时间Tsur=(N-1)·(T4+T5);When dispatching N (N is an even number) UAVs, if a single ground station is used to control the UAVs to take off, it will take a total time Tsig=N·(T4+T5+T6+T7), if two ground stations are used to monitor It takes a total time Tdou=(T4+T5+T6+T7)+(N-1)·(T6+T7) for the UAV to take off, so the time saved when dispatching N UAVs is Tsur=(N- 1) (T4+T5);
上述无人机流水线式起飞过程中,第N架无人机出动时,第N-2架无人机已飞至安全区域为前提,即T6+T7>T4+T5,亦即监控第N-2架飞机的地面站已空闲可立刻转为控制第N架飞机,但根据实际飞机型号的不同,可能存在T6+T7<T4+T5的情况,此时第N-2架飞机飞至安全区域时,第N架飞机尚未达到起飞线,此种情况以双地面站监控飞机起飞,花费时间Tdou=(T4+T5+T6+T7)+(N-1)*(T4+T5),此时节省时间为Tsur=(N-1)*(T6+T7);During the pipelined take-off process of the above-mentioned drones, when the Nth drone is dispatched, the N-2th drone has flown to a safe area as a prerequisite, that is, T6+T7>T4+T5, that is, monitoring the N-th drone The ground stations of the 2 aircrafts are free and can be immediately transferred to control the Nth aircraft, but depending on the actual aircraft type, there may be a situation where T6+T7<T4+T5, at this time the N-2th aircraft flies to the safe area At this time, the Nth aircraft has not yet reached the take-off line. In this case, two ground stations are used to monitor the aircraft take-off, and it takes time Tdou=(T4+T5+T6+T7)+(N-1)*(T4+T5), at this time Time saving is Tsur=(N-1)*(T6+T7);
起飞过程中,若已经起飞的飞机出现特情需要迫降时,其中的一个地面站控制飞机迫降,另一个地面站仍可以监控其他飞机起降,不会导致任务失败;降落过程中,若正在降落的飞机出现特情需要复飞,复飞后另一个地面站可控制后续飞机降落,可减少后续飞机降落等待时间,避免可能出现的油量不足造成灾难性事故,若降落过程中,有其他飞机出现特情需要迫降时,另一个地面站可控制出现特情的飞机在迫降道上迫降,提高系统安全性。During the take-off process, if the aircraft that has already taken off has a special situation and needs to make an emergency landing, one of the ground stations will control the aircraft to make an emergency landing, and the other ground station can still monitor the take-off and landing of other aircraft, which will not cause the mission to fail; during the landing process, if it is landing If the aircraft needs a go-around due to special circumstances, another ground station can control the landing of the subsequent aircraft after the go-around, which can reduce the waiting time for the subsequent aircraft to land, and avoid possible catastrophic accidents caused by insufficient fuel. If there are other aircraft during the landing process When a special situation requires an emergency landing, another ground station can control the special situation of the aircraft to make an emergency landing on the emergency landing road, improving system security.
本发明一种基于双地面站的无人机流水线式起降方法为国内首创,可大幅减少飞机集结等待时间,提高编队执行任务的响应实时性,同时提高编队执行任务的航程、航时。The invention is the first in China to take off and land the UAV assembly line based on dual ground stations, which can greatly reduce the waiting time for aircraft assembly, improve the real-time response of formation tasks, and improve the range and flight time of formation tasks.
最后需要指出的是:以上实施例仅用以说明本发明的技术方案,而非对其限制。尽管参照前述实施例对本发明进行了详细的说明,本领域的普通技术人员应当理解:其依然可以对前述各实施例所记载的技术方案进行修改,或者对其中部分技术特征进行等同替换;而这些修改或者替换,并不使相应技术方案的本质脱离本发明各实施例技术方案的精神和范围。Finally, it should be pointed out that the above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit them. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that: they can still modify the technical solutions described in the aforementioned embodiments, or perform equivalent replacements for some of the technical features; and these The modification or replacement does not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the various embodiments of the present invention.
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109116866A (en) * | 2018-09-20 | 2019-01-01 | 四川腾盾科技有限公司 | A kind of unmanned plane is two-way independently to drive into control method |
| WO2020021485A1 (en) * | 2018-07-27 | 2020-01-30 | Aldarwish Ahmad Fareed H | Autonomous aircraft control systems and related methods |
| CN112904886A (en) * | 2019-12-03 | 2021-06-04 | 顺丰科技有限公司 | Unmanned aerial vehicle flight control method and device, computer equipment and storage medium |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2001145090A (en) * | 1999-11-16 | 2001-05-25 | Mitsubishi Electric Corp | Monitoring device |
| CN105223964A (en) * | 2015-09-28 | 2016-01-06 | 沈阳航空航天大学 | A kind of control system for UAV Formation Flight |
| EP2978258A1 (en) * | 2014-07-22 | 2016-01-27 | Alcatel Lucent | Seamless replacement of a first drone base station with a second drone base station |
| US20160046387A1 (en) * | 2014-08-18 | 2016-02-18 | Sunlight Photonics Inc. | Methods and apparatus for a distributed airborne wireless communications fleet |
| WO2016053194A1 (en) * | 2014-10-03 | 2016-04-07 | Infinium Robotics Pte Ltd | System for performing tasks in an operating region and method of controlling autonomous agents for performing tasks in the operating region |
| CN105513434A (en) * | 2016-01-18 | 2016-04-20 | 毕雪松 | Unmanned plane flight control system and control method thereof |
| CN105599900A (en) * | 2016-01-20 | 2016-05-25 | 清华大学合肥公共安全研究院 | Low-altitude positioning load air-drop method based on multi-rotor unmanned aerial vehicle |
| CN105825718A (en) * | 2016-04-26 | 2016-08-03 | 广东容祺智能科技有限公司 | Unmanned aerial vehicle comprehensive management platform system |
| CN205543960U (en) * | 2016-02-15 | 2016-08-31 | 西南交通大学 | High efficiency unmanned aerial vehicle crowd power patrol inspection system |
| WO2016154949A1 (en) * | 2015-03-31 | 2016-10-06 | SZ DJI Technology Co., Ltd. | Authentication systems and methods for generating flight regulations |
| CN106054903A (en) * | 2016-07-27 | 2016-10-26 | 中南大学 | Multi-rotor unmanned aerial vehicle self-adaptive landing method and system |
-
2016
- 2016-11-30 CN CN201611084626.0A patent/CN106530839B/en active Active
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2001145090A (en) * | 1999-11-16 | 2001-05-25 | Mitsubishi Electric Corp | Monitoring device |
| EP2978258A1 (en) * | 2014-07-22 | 2016-01-27 | Alcatel Lucent | Seamless replacement of a first drone base station with a second drone base station |
| US20160046387A1 (en) * | 2014-08-18 | 2016-02-18 | Sunlight Photonics Inc. | Methods and apparatus for a distributed airborne wireless communications fleet |
| WO2016053194A1 (en) * | 2014-10-03 | 2016-04-07 | Infinium Robotics Pte Ltd | System for performing tasks in an operating region and method of controlling autonomous agents for performing tasks in the operating region |
| WO2016154949A1 (en) * | 2015-03-31 | 2016-10-06 | SZ DJI Technology Co., Ltd. | Authentication systems and methods for generating flight regulations |
| CN105223964A (en) * | 2015-09-28 | 2016-01-06 | 沈阳航空航天大学 | A kind of control system for UAV Formation Flight |
| CN105513434A (en) * | 2016-01-18 | 2016-04-20 | 毕雪松 | Unmanned plane flight control system and control method thereof |
| CN105599900A (en) * | 2016-01-20 | 2016-05-25 | 清华大学合肥公共安全研究院 | Low-altitude positioning load air-drop method based on multi-rotor unmanned aerial vehicle |
| CN205543960U (en) * | 2016-02-15 | 2016-08-31 | 西南交通大学 | High efficiency unmanned aerial vehicle crowd power patrol inspection system |
| CN105825718A (en) * | 2016-04-26 | 2016-08-03 | 广东容祺智能科技有限公司 | Unmanned aerial vehicle comprehensive management platform system |
| CN106054903A (en) * | 2016-07-27 | 2016-10-26 | 中南大学 | Multi-rotor unmanned aerial vehicle self-adaptive landing method and system |
Non-Patent Citations (1)
| Title |
|---|
| 邓高湘: "小型无人直升机中继数据链系统设计与实现", 《中国优秀硕士学位论文全文数据库 工程科技II辑2015年》 * |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020021485A1 (en) * | 2018-07-27 | 2020-01-30 | Aldarwish Ahmad Fareed H | Autonomous aircraft control systems and related methods |
| US11307598B2 (en) | 2018-07-27 | 2022-04-19 | Ahmad Fareed Aldarwish | Autonomous aircraft control systems and related methods |
| US11884392B2 (en) | 2018-07-27 | 2024-01-30 | Ahmad Fareed Aldarwish | Autonomous aircraft control systems |
| IL280412B1 (en) * | 2018-07-27 | 2025-03-01 | Ahmad Fareed H Aldarwish | Autonomous aircraft control systems and related methods |
| IL280412B2 (en) * | 2018-07-27 | 2025-07-01 | Ahmad Fareed H Aldarwish | Autonomous aircraft control systems and related methods |
| CN109116866A (en) * | 2018-09-20 | 2019-01-01 | 四川腾盾科技有限公司 | A kind of unmanned plane is two-way independently to drive into control method |
| CN109116866B (en) * | 2018-09-20 | 2021-05-14 | 四川腾盾科技有限公司 | Bidirectional autonomous driving-in control method for unmanned aerial vehicle |
| CN112904886A (en) * | 2019-12-03 | 2021-06-04 | 顺丰科技有限公司 | Unmanned aerial vehicle flight control method and device, computer equipment and storage medium |
| CN112904886B (en) * | 2019-12-03 | 2023-08-11 | 丰翼科技(深圳)有限公司 | Unmanned aerial vehicle flight control method and device, computer equipment and storage medium |
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|---|---|
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