公开(公告)号：WO2017079340A1

公开(公告)日：2017-05-11

申请号：PCT/US2016/060172

申请日：2016-11-02

Applicant: PULSE AEROSPACE LLC

Inventor： HOLLY, Lance ,  DONOVAN, William ,  LESSIG, Aaron

IPC: B64C39/02 ,  B64D1/18

CPC classification number: B64D1/18 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/12

Abstract: A disbursement system for a UAV is provided. The disbursement system may include a plurality of disbursement nozzles operable to dispense an agricultural product at variable flowrates, a flow controller responsive to instructions and operable to regulate a volume of the agricultural product dispensed by the disbursement nozzles, and a control system. The control system may include a plurality of sensors operable to monitor a plurality of flight parameters and a processing unit configured to model an effect of the plurality of flight parameters on first flow control instructions corresponding to a prescription coverage of the agricultural product and calculate and output modulated flow control instructions to the flow controller. The control system may modulate the first control instructions to change a flowrate of one or more of the plurality of disbursement nozzles to achieve an actual coverage of the agricultural product that is closer to the prescription coverage.

Abstract translation:

提供无人机的支付系统。 分配系统可包括多个分配喷嘴和控制系统，所述多个分配喷嘴可操作以分配可变流量的农产品，流量控制器响应于指令并可操作以调节由分配喷嘴分配的农产品的体积。 控制系统可以包括可操作来监视多个飞行参数的多个传感器以及配置成对多个飞行参数对与农产品的处方覆盖范围相对应的第一流量控制指令的影响进行建模并且计算和输出 调制流量控制指令给流量控制器。 控制系统可调节第一控制指令以改变多个分配喷嘴中的一个或多个的流量，以实现更接近处方范围的农产品的实际覆盖率。

公开(公告)号：WO2017035391A1

公开(公告)日：2017-03-02

申请号：PCT/US2016/048765

申请日：2016-08-25

Applicant: PULSE AEROSPACE LLC

Inventor： HOLLY, Lance ,  DONOVAN, William

IPC: B64C27/605 ,  A63H27/127 ,  A63H27/133 ,  B64C27/00 ,  B64C27/58 ,  B64C27/59

CPC classification number: B64C27/605 ,  B64C39/024 ,  B64C2201/024

Abstract: A ganged servo flight control system for an unmanned aerial vehicle is provided. The flight control system may include a swashplate having first, second, and third connection portions; a first control assembly connected to the first connection portion of the swashplate; a second control assembly connected to the second connection portion of the swashplate; and a third control assembly connected to the third connection portion of the swashplate. The first control assembly may include two or more servo-actuators connected to operate in cooperation with each other.

Abstract translation: 提供了一种用于无人机的联动伺服飞行控制系统。 飞行控制系统可以包括具有第一，第二和第三连接部分的斜盘; 连接到斜盘的第一连接部分的第一控制组件; 连接到斜盘的第二连接部分的第二控制组件; 以及连接到斜盘的第三连接部分的第三控制组件。 第一控制组件可以包括被连接以彼此协作操作的两个或更多个伺服致动器。