-
公开(公告)号:EP4439108A1
公开(公告)日:2024-10-02
申请号:EP24162551.6
申请日:2024-03-11
IPC分类号: G01S1/02 , G01S19/15 , G01S19/47 , G01S19/49 , G08G5/00 , G08G5/02 , G05D1/247 , G05D1/46 , G05D1/654 , G05D105/22 , G05D107/13 , G05D1/646 , G05D109/22 , G05D111/30
CPC分类号: G01S1/02 , G01S19/15 , G01S19/49 , G01S19/47 , G08G5/025 , G08G5/0047 , G08G5/0021 , G05D1/646 , G05D1/6545 , G05D2109/2220240101 , G05D2107/1320240101 , G05D2111/3020240101 , G05D1/247 , G05D2105/2220240101 , G05D1/46
摘要: - Dispositif et système d'estimation d'une position et d'une vitesse d'un aéronef lors d'une phase d'approche permettant un atterrissage automatique.
- Le dispositif d'estimation (1) comporte une unité d'acquisition (1) d'une position courante (latGNSS, lonGNSS, hGNSS) de l'aéronef (AC) d'un système de géo-positionnement (GNSS), une unité d'acquisition (2) d'une accélération courante (an, ae, az) d'une centrale inertielle (IRS), une unité d'acquisition (3) d'un écart latéral courant (ηLOC) et d'un écart vertical courant (ηGLD) d'un dispositif d'aide à l'atterrissage (22), une unité de filtrage (4) pour estimer une vitesse non-biaisée (Vn, Ve, Vd) de l'aéronef (AC), une unité de filtrage (7) pour estimer une déviation latérale (DY) courante, une déviation verticale (DZ) courante ainsi qu'une vitesse latérale (DVY) courante et une vitesse verticale (DVZ) courante de l'aéronef (AC).-
公开(公告)号:EP4428040A1
公开(公告)日:2024-09-11
申请号:EP22889784.9
申请日:2022-10-20
申请人: DENSO CORPORATION
发明人: TAKEMURA, Yuichi , NAKATA, Shingo
CPC分类号: B64D45/00 , B64D27/24 , G05D2109/2420240101 , G05D2105/2220240101 , G05D1/6546 , G05D1/85 , B64C29/0033 , B64D27/34 , B64D31/09 , B64D31/16
摘要: A flight control device executes flight control processing for causing the eVTOL to fly. The flight control device sets an operating mode to one of fail-safe modes based on current one of normal modes when an abnormality has occurred in an eVTOL. When the operating mode at the time of occurrence of the abnormality is a vertical landing mode, the flight control device changes the operating mode to a landing continuation mode in step S105. When the operating mode at the time of occurrence of the abnormality is a vertical take-off mode, the flight control device sets the operating mode to an emergency landing mode in step S107. When the operating mode at the time of occurrence of the abnormality is a cruise mode or a hovering mode, the flight control device sets the operating mode to a resetting mode in step S108.
-
公开(公告)号:EP4417509A1
公开(公告)日:2024-08-21
申请号:EP24151966.9
申请日:2024-01-15
申请人: The Boeing Company
发明人: Morel, Mark R. , Zimmer, Neil , Flanzer, Tristan
IPC分类号: B64C17/06
CPC分类号: B64C17/06 , B64C13/00 , G01M1/10 , B64C19/00 , G05D1/495 , G05D2109/2220240101 , G05D2105/2220240101
摘要: A machine and process for control of rotation of a vehicle about an axis of the vehicle is shown. A flight control system includes control laws that control the rotation of the vehicle (100) around the axis (X,Y,Z) of the vehicle. An estimate is derived for an inertia about the axis. The estimated inertia is derived from sensed quantities of material in a component (200,202,204) of the vehicle (100). An inertia gain schedule and filter are added to enhance, using the estimated inertia, the accuracy of the control laws that control the rotation of the vehicle (1200) around the axis (X,Y,Z) of the vehicle.
-
4.
公开(公告)号:EP4411504A1
公开(公告)日:2024-08-07
申请号:EP23154246.5
申请日:2023-01-31
申请人: ABB SCHWEIZ AG
IPC分类号: G05D1/02
CPC分类号: G05D2109/3420240101 , G05D1/611 , G05D2105/2220240101 , G05D2107/2720240101
摘要: A method of controlling a vessel (10) comprising a plurality of thrusters (12a-12d), where the vessel (10) is configured to operate in a bias mode (42a, 42b) where at least two of the thrusters (12a-12d) provide thrust forces (36a-36d) at least partly in opposite thrust directions, the method comprising estimating, by a control system (14), an operational condition associated with the vessel (10); and commanding, by the control system (14) and based on the estimation, execution of a countermeasure associated with an activation of the bias mode (42a, 42b), a deactivation of the bias mode (42a, 42b) or a change of a bias level of the bias mode (42a, 42b). A control system (14) and a vessel (10) are also provided.
-
5.
公开(公告)号:EP4404015A2
公开(公告)日:2024-07-24
申请号:EP24180054.9
申请日:2016-11-03
申请人: Zoox, Inc.
IPC分类号: G05D1/00
CPC分类号: G01S5/0018 , G01S5/16 , G08G1/205 , G01S17/87 , G01S7/4972 , G01S13/865 , G01S13/867 , G01S13/87 , G08G1/20 , G01S2013/932220200101 , G01S2013/931620200101 , G06V20/56 , B60L3/0015 , B60L2260/3220130101 , B60L2240/62220130101 , B60Q1/503 , B60Q1/507 , B60Q1/549 , B60Q1/508 , G01C21/3881 , G01C21/3848 , G01C21/3867 , G08G1/164 , G05D2105/2220240101 , G05D2107/1320240101 , G05D2109/1020240101 , G05D1/2249 , G05D1/226 , G05D1/6987 , G05D1/2246
摘要: Various embodiments relate generally to autonomous vehicles and associated mechanical, electrical and electronic hardware, computer software and systems, and wired and wireless network communications to provide map data for autonomous vehicles. In particular, a method may include accessing subsets of multiple types of sensor data, aligning subsets of sensor data relative to a global coordinate system based on the multiple types of sensor data to form aligned sensor data, and generating datasets of three-dimensional map data. The method further includes detecting a change in data relative to at least two datasets of the three-dimensional map data and applying the change in data to form updated three-dimensional map data. The change in data may be representative of a state change of an environment at which the sensor data is sensed. The state change of the environment may be related to the presence or absences of an object located therein.
-
公开(公告)号:EP4187342B1
公开(公告)日:2024-07-17
申请号:EP21290078.1
申请日:2021-11-30
IPC分类号: G05D1/224 , G05D1/227 , G05D105/22 , G05D107/13 , G05D109/10
CPC分类号: G05D1/227 , G05D1/2279 , G05D2109/1020240101 , G05D2107/1320240101 , G05D2105/2220240101 , G05D1/2247
-
公开(公告)号:EP4380115A3
公开(公告)日:2024-06-26
申请号:EP24158679.1
申请日:2015-12-14
IPC分类号: G05D1/226 , G05D1/227 , G07C9/00 , B60W50/12 , B60W10/10 , B60W10/18 , B60W10/20 , B60W50/00 , H04L12/403
CPC分类号: B60W50/12 , B60W2050/000620130101 , B60W2050/007120130101 , B60W2050/009120130101 , B60W2050/009420130101 , H04L12/403 , B60W10/18 , B60W10/20 , B60W10/10 , B60W2556/4520200201 , B60W2556/5520200201 , G05D2109/1020240101 , G05D2105/2220240101 , G05D2107/1320240101 , G05D1/227 , G05D1/2265
摘要: A system and method for interfacing an autonomous or remote control drive-by-wire controller with a vehicle's control modules. Vehicle functions including steering, braking, starting, etc. are controllable by wire via a control network. A CAN architecture is used as an interface between the remote/autonomous controller and the vehicle's control modules. A CAN module interface provides communication between a vehicle control system and a supervisory, remote, autonomous, or drive-by-wire controller. The interface permits the supervisory control to control vehicle operation within pre-determined bounds and using control algorithms.
-
8.
公开(公告)号:EP4385818A1
公开(公告)日:2024-06-19
申请号:EP23213417.1
申请日:2023-11-30
发明人: Inoue, Hiroshi
CPC分类号: B63H21/22 , B63H25/04 , B63C3/12 , B60P3/1075 , G05D2109/3420240101 , G05D1/661 , G05D2107/8420240101 , G05D2105/2220240101 , G05D1/248
摘要: A trailering support device capable of facilitating trailering for loading of a hull onto a trailer. The trailering support device performs automatic vessel steering control so as to move the hull toward the trailer, estimates, based on a content of the automatic vessel steering control, a position and an azimuth of the hull at a predetermined timing after start of the automatic vessel steering control, detects the position, a steering angle and the azimuth, of the hull, respectively compares the position and the azimuth estimated with the position and the azimuth detected at the predetermined timing, and determines, based on a comparison result, whether the loading of the hull onto the trailer is performable, and in a case where it is determined that the loading of the hull onto the trailer is not performable, notifies of that matter.
-
公开(公告)号:EP4329342A3
公开(公告)日:2024-05-22
申请号:EP24151120.3
申请日:2021-02-10
IPC分类号: H04W4/40
CPC分类号: H04W4/40 , G05D2109/1020240101 , G05D2105/2220240101 , G05D2107/1320240101 , G05D1/2265 , G05D1/227
摘要: A method is performed by a first server communicatively connected to a network for supporting tele-operated driving of a vehicle. The method includes receiving a request from a tele-operated driving application client by the client device in the vehicle for teleoperated driving support. The client processes the request and sends a trigger request for teleoperated driving to the first server. This request includes a trigger and information for supporting a tele-operated driving event.
The first server processes the request to identify a second server for providing support for the Tele-operated driving event, wherein the processing is based on parameters of the network for providing tele-operated driving support. Finally the first server will set-up a tele-operated driving session between the second server and the application client. The first server may also predict whether a tele-operated driving event is likely in a future time period based on prediction information obtained from one or more of the vehicle, the second server, a network server, and a third party application server.-
公开(公告)号:EP4438468A1
公开(公告)日:2024-10-02
申请号:EP22915522.1
申请日:2022-10-31
发明人: KOJIMA, Toru
CPC分类号: B64C13/18 , G08G5/02 , G05D2109/2520240101 , G05D2107/2720240101 , G05D1/606 , G05D1/6542 , G05D1/652 , G05D1/244 , G05D2111/1020240101 , G05D2105/2220240101
摘要: This automatic takeoff/landing system for a vertical takeoff/landing aircraft comprises: a relative wind information acquisition unit that acquires the direction of relative wind at a moving object; and a control unit that executes takeoff/landing control to cause the vertical takeoff/landing aircraft to takeoff/land at a landing target point provided on the moving object. The control unit, during takeoff/landing of the vertical takeoff/landing aircraft, executes the takeoff/landing control on the basis of the direction of the relative wind acquired by the relative wind information acquisition unit, in a state in which the aircraft heading of the vertical takeoff/landing aircraft is caused to face the direction of the relative wind.
-
-
-
-
-
-
-
-
-