CONFIGURABLE NETWORK SWITCH FOR INDUSTRIAL CONTROL SYSTEMS INCLUDING DETERMINISTIC NETWORKS

    公开(公告)号:US20220353192A1

    公开(公告)日:2022-11-03

    申请号:US17863777

    申请日:2022-07-13

    摘要: A network switch includes a first port configured for communication with a first electric device and a second port configured for communication with a second electric device in a deterministic network. The network switch includes one or more processors configured to receive at the first port a communication packet associated with the first electric device and the second electric device, determine if the communication packet satisfies a plurality of protocol constraints, and in response to the communication packet satisfying the plurality of protocol constraints, input one or more message characteristics from the communication packet into a model associated with a first industrial process. The model is configured to output a process behavioral classification based on the one or more message characteristics. The one or more processors receive a process behavioral classification for the communication packet, and selectively generate a control action for the ICS based on the process behavioral classification.

    Detecting the spoofing of a signal
    12.
    发明授权

    公开(公告)号:US11480689B2

    公开(公告)日:2022-10-25

    申请号:US16681318

    申请日:2019-11-12

    IPC分类号: G01S19/21 G01S19/24 G01S19/29

    摘要: A method for detecting the spoofing of a signal from a satellite in orbit. A receiver can be located on an aircraft to receive an apparent satellite signal. The method can include determining at least two characteristic signatures of the signal including a power level, and indicating the apparent satellite signal is a spoofed satellite signal.

    METHOD OF ASSESSING A PILOT EMOTIONAL STATE

    公开(公告)号:US20220284737A1

    公开(公告)日:2022-09-08

    申请号:US17751037

    申请日:2022-05-23

    IPC分类号: G06V40/20 A61B5/18 G10L25/63

    摘要: A method 140 of assessing an operator emotional state 131 and sending an alert 144 based on the emotional state 131. The method 140 includes tracking 141 during a time period, using at least one sensor 103, 105, 106, 112, 117, one of an image sensor data, voice data or a biometric parameter of an operator. Determining 142, using a controller 120 that is operatively connected to at least one sensor 103, 105, 106, 112, 117, a probability of a likely emotional state 131 from a list of emotional states 131 of an operator based on one of the image sensor data, voice data or the biometric parameter. Comparing 143, using a processor, the probability of one of the likely emotional states 131 of the operator with a baseline emotional state 131 of the operator. Sending 144, using the controller 120, an alert if most likely emotional state deviates from the baseline emotional state by a predetermined threshold.

    Pitch control assembly
    15.
    发明授权

    公开(公告)号:US11407494B2

    公开(公告)日:2022-08-09

    申请号:US16541726

    申请日:2019-08-15

    摘要: A method of controlling a propeller assembly, having a blade, piston end cap, and piston, with a pitch control unit, having a transfer bearing and a blade angle unit, the method comprising: axially moving a transfer tube relative to and circumscribing the transfer bearing, and sensing an axial movement of the transfer tube with the blade angle unit.

    Environment specific input protection

    公开(公告)号:US11242132B2

    公开(公告)日:2022-02-08

    申请号:US16014659

    申请日:2018-06-21

    摘要: One example aspect of the present disclosure relates to a method for assessing input. The method can include determining a state of the aerial vehicle. The method can include obtaining data indicative of an expected operator input based on the determined state. The method can include obtaining data indicative of an actual operator input. The method can include determining a state of operator behavior based on the expected operator input and the actual operator input. The method can include determining a control action for the aerial vehicle based on the determined state of the aerial vehicle and the determined state of the operator behavior. The method can include implementing the control action.

    SYSTEMS AND METHODS FOR MOBILE DEVICE ENABLED ROTOR TRACK AND BALANCE

    公开(公告)号:US20210394920A1

    公开(公告)日:2021-12-23

    申请号:US16907647

    申请日:2020-06-22

    IPC分类号: B64D43/00 B64F5/60 H04L29/08

    摘要: A handheld mobile device may be configured for use within a cockpit or cabin of an aircraft. The handheld mobile device may include a display and memory that includes an application configured to utilize the display. The handheld mobile device may also include a processor coupled to the memory. The application, via the processor, may be configured to receive aircraft-specific configuration data. The application may also receive, from a tracker module, input data corresponding to blade height and position. The application may additionally receive airframe vibration data from an accelerometer module. The application may further calculate recommendations regarding track and balance. The application may also further output, via the display, the track and balance recommendations.

    Aircraft component monitoring system

    公开(公告)号:US11161624B2

    公开(公告)日:2021-11-02

    申请号:US15598595

    申请日:2017-05-18

    IPC分类号: B64D45/00 G06F30/20 G01M17/00

    摘要: Systems and methods for determining aircraft component phase position are provided. In one embodiment, a method can include receiving a set of data from a data acquisition system associated with a component. The method can include identifying a plurality of phase reference points based, at least in part, on the set of data. Each phase reference point can be indicative of a phase position of the component relative to the data acquisition system at a respective point in time. The method can include generating a model based, at least in part, on the plurality of phase reference points. The model can be indicative of the phase position of the component relative to the data acquisition system at a plurality of times. The method can include determining the phase position of the component at one or more points in time based, at least in part, on the model.