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    SYSTEMS AND METHODS FOR UNMANNED AERIAL VEHICLE SIMULATION TESTING
    2.
    发明申请
    SYSTEMS AND METHODS FOR UNMANNED AERIAL VEHICLE SIMULATION TESTING 审中-公开

    公开(公告)号：WO2022221289A2

    公开(公告)日：2022-10-20

    申请号：PCT/US2022/024438

    申请日：2022-04-12

    Applicant: IRIS AUTOMATION, INC.

    Inventor： GALINDO, Patricio Alejandro ,  SCHAFER, Eric ,  RAVISHANKAR, Nikhilesh

    IPC: G06F11/36 ,  B64C2201/127 ,  B64C2201/141 ,  B64C39/024 ,  G05D1/101 ,  G06F11/3664 ,  G06F11/3684 ,  G08G5/003

    Abstract: Systems and methods for generating testing and training cases for a simulator based on simulated events are disclosed. The system can monitor an input from a first simulation of a first test case, and detect, based on the input from the first simulation, a target condition resulting from the first test case. The system can identify, based on the target condition, first simulation parameters of the first test case associated with the target condition. The system can generate a second test case having second simulation parameters by modifying the first simulation parameters of the first test case, and output the second test case to a flight autonomy system. The system can provide the generated test cases for the flight autonomy system and can monitor the real-time performance of the simulation of the flight autonomy system.

    SYSTEM OF MULTI-SWARM DRONE CAPTURING
    3.
    发明申请
    SYSTEM OF MULTI-SWARM DRONE CAPTURING 审中-公开

    公开(公告)号：WO2022005903A1

    公开(公告)日：2022-01-06

    申请号：PCT/US2021/039159

    申请日：2021-06-25

    Applicant: SONY GROUP CORPORATION ,  CHENG-YI, Liu

    Inventor： CHENG-YI, Liu

    IPC: G06T7/55 ,  G06D1/12 ,  B64C39/02 ,  B64D47/08 ,  B64C2201/127 ,  B64C2201/143 ,  B64C39/024 ,  G05D1/0094 ,  G05D1/104 ,  G05D1/12 ,  G06F3/012 ,  G06F3/013 ,  G06T2207/30201 ,  G06T7/74 ,  G08G5/0013 ,  H04N5/232

    Abstract: A system of multi-view imaging of an environment through which a target moves includes pluralities of drones, each drone having a drone camera. A first plurality of drones moves to track target movement, capturing a corresponding first plurality of images of the target's face, making real time determinations of the target's head pose and gaze from the captured images and transmitting the determinations to a second plurality of drones. The second plurality of drones moves to track target movement of the target, with drone camera poses determined at least in part by the head pose and gaze determinations received from the first plurality of drones, in order to capture a second plurality of images of portions of the environment in front of the target. Post-processing of the second plurality of images allows generation of a first-person view representative of a view of the environment seen by the target.

    INTERNALLY DAMPED CROSSBAR ASSEMBLY HAVING ELASTOMERIC ISOLATOR
    8.
    发明申请
    INTERNALLY DAMPED CROSSBAR ASSEMBLY HAVING ELASTOMERIC ISOLATOR 审中-公开

    公开(公告)号：WO2021126354A1

    公开(公告)日：2021-06-24

    申请号：PCT/US2020/056135

    申请日：2020-10-16

    Applicant: RAYTHEON COMPANY

    Inventor： MILLER, Kirk A. ,  THOMAS, Sean G.

    IPC: F16F15/08 ,  G03B15/00 ,  B64D47/08 ,  B64C2201/123 ,  B64C2201/127 ,  F16F2222/02 ,  F16F2224/025 ,  F16F2230/0047 ,  G01C21/18 ,  G03B17/561

    Abstract: A crossbar assembly (30a, 30b) for facilitating isolation of a sensor assembly from vibration of a payload mounting system on a vehicle comprises an outer crossbar segment (60), an inner crossbar segment (66), and an isolator (38a, 38b). The inner crossbar segment (66) comprises a payload mount interface (36a, 36b) operable to mount to a payload mount (22), and an inner isolator interface (67) operable to mount to an isolator (38a, 38b). The outer crossbar segment (60) comprises a structure interface (34a, 34b) to mount to a structure, and an outer isolator interface (61) operable to mount to the isolator (38a, 38b). The isolator (38a, 38b) can be supported by the outer and inner crossbar segments (60, 66). The isolator (38a, 38b) comprises an elastomeric component (50) operable to elastically deform in response to relative movement between the outer and inner crossbar segments (60, 66). The isolator (38a, 38b) operates to partially decouple the outer crossbar segment (60) from the inner crossbar segment (66) and dampen vibrations propagating between the outer and inner crossbar segments (60, 66).

    DRONE AIRCRAFT WITH MAGNETIC CONSTRUCT
    10.
    发明申请
    DRONE AIRCRAFT WITH MAGNETIC CONSTRUCT 审中-公开

    公开(公告)号：WO2021053600A2

    公开(公告)日：2021-03-25

    申请号：PCT/IB2020/058711

    申请日：2020-09-18

    Applicant: KANDASAMY, Dushan

    Inventor： KANDASAMY, Dushan

    IPC: B64C39/06 ,  G01P13/02 ,  B64C25/62 ,  B64C39/02 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/162 ,  B64C39/024 ,  B64C39/062

    Abstract: The present invention discloses a drone, comprising a cyclical hull with one or more cyclical rings, an external structure, and a piezoelectric system. The external structure comprises a fixed wing and a rotary turbine construction. The external structure is securely and rotationally connected to the cyclic ring. The external structure is configured to rotate exponentially around the cyclical hull, thereby enabling a stabilization capability of the drone to forward in the desired direction. The piezoelectric system is mounted on the cyclical hull for efficiently analyzing onward wind direction, thereby effectively rotating the external structure at high speeds to enable the structural integrity of the drone. The drone further comprises one or more locking systems to unlock the cyclical rotational turbine based on an alert received from the piezoelectric system. Further, the drone comprises a camera for capturing a surrounding view of the drone.

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