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1. 发明专利

AU2021236537A1 Object tracking system including stereo camera assembly and methods of use 未知
公开(公告)号：AU2021236537A1
公开(公告)日：2022-05-26
申请号：AU2021236537
申请日：2021-09-23
申请人： AURORA FLIGHT SCIENCES CORPORATION A SUBSIDIARY OF THE BOEING COMPANY
发明人： HEAFITZ ANDREW MARK , JANJIC IGOR
IPC分类号： G06T7/285 , G02B13/02 , G02B13/04 , G03B35/00 , G06N3/02 , G06T7/215 , H04N5/232 , H04N13/10
摘要： OBJECT TRACKING SYSTEM INCLUDING STEREO CAMERA ASSEMBLYAND METHODSOFUSE An example of the present disclosure provides a stereo camera assembly (1203) of an object tracking system (1204). The stereo camera assembly (1203) comprises a wide-angle lens camera (1222) mounted on a mounting structure (1226) and a telephoto lens camera (1224) mounted on the mounting structure (1226) such that a field of view (1232) of the telephoto lens camera (1224) is at least partially encompassed by a field of view (1230) of the wide-angle lens camera (1222). F- - - ------------- ---------- 1 I n L - - - - - - - - - - - - - - - - I

2. 发明专利

AU2021212120A1 Controlling a vehicle based on detected movement of an object 未知
公开(公告)号：AU2021212120A1
公开(公告)日：2022-04-07
申请号：AU2021212120
申请日：2021-08-06
申请人： AURORA FLIGHT SCIENCES CORPORATION A SUBSIDIARY OF THE BOEING COMPANY
发明人： CHUA ZARRIN , KEARNEY-FISCHER MARTIN
IPC分类号： G05D1/02 , G05B13/02 , G06F3/01 , G06K9/00
摘要： CONTROLLING A VEHICLE BASED ON DETECTED MOVEMENT OF A method of controlling a vehicle (102) includes detecting, by an optical sensor (104), a movement of at least one object in a field of view of the optical sensor (104). The method further includes identifying, by a processor circuit (114), a pattern based on the movement of the at least one object. The method further includes determining, by the processor circuit (114) based on the pattern, a vehicle command to be performed by the vehicle (102). -C= J -J; =~ = E 7", 1 =5_ I =~j _ L LU m -LA - -S 7iC%4 C%4

3. 发明专利

AU2021215109A1 Systems and methods for operating a vehicle in a degraded visual environment 未知
公开(公告)号：AU2021215109A1
公开(公告)日：2022-04-28
申请号：AU2021215109
申请日：2021-08-09
申请人： AURORA FLIGHT SCIENCES CORPORATION A SUBSIDIARY OF THE BOEING COMPANY
发明人： SAUNDERS JEFFREY
IPC分类号： G05D1/10 , G01S17/933 , G08G5/00 , G08G5/02 , G08G9/00
摘要： SYSTEMS AND METHODS FOR OPERATING A VEHICLE IN A DEGRADED VISUAL ENVIRONMENT In an example, a method for controlling a vehicle (10) in a degraded visual environment (212) is provided. The method includes identifying a degraded visual environment (212) corresponding to a phase of a route followed by the vehicle (101). The method includes determining, based on the phase of the route, a first segment of a trajectory of the vehicle (101) along which to search for a location with an improved navigation environment. The method includes causing the vehicle (101) to follow the first segment until: (i) identifying the improved navigation environment, or (ii) reaching an end of the first segment without identifying the improved navigation environment. The method includes determining a second segment of the trajectory based on whether the improved navigation environment has been identified. The method includes causing the vehicle (101) to follow the second segment. Ci 04co00 - ..- ) 0) M- 0 E HE 0) a, c 0)) Cl) z C: _0 0 C 0 0 0) 0)) U)) U)0 U 0 0 z ~0 CD C z > - E 0 Mm:C H 0) 0)Cj c.0( (Uc) LL 0) WCC:

4. 发明专利

AU2021273629A1 Aircraft sensor system synchronization 未知
公开(公告)号：AU2021273629A1
公开(公告)日：2022-06-30
申请号：AU2021273629
申请日：2021-11-26
申请人： AURORA FLIGHT SCIENCES CORPORATION A SUBSIDIARY OF THE BOEING COMPANY
发明人： TURALBA JOSE ANTONIO L
IPC分类号： G05D1/04 , B64C39/02 , B64D47/08 , G01C11/06 , H04N13/10
摘要： A"lN- 505 504 xR*A' ---------- -- - -x AIRCRAFT SENSOR SYSTEM SYNCHRONIZATION A method, apparatus, system, and computer program product for operating an aerial imaging system. A first altitude of a first aircraft is determined, by a computer system (210), using first images of a key point generated by the first aircraft during a flight and stereo depth triangulation. The first altitude is compared with a second altitude of a second aircraft determined by the second aircraft, by the computer system (210), to form a comparison. An offset between the first altitude and the second altitude is determined, by the computer system (210), using the comparison. At least one of the first altitude or the second altitude is adjusted based on the offset. A plurality of images of a region from the first aircraft at the first altitude and from the second aircraft at the second altitude is obtained.

5. 发明申请

WO2018156335A3 SYSTEM AND METHOD FOR DISTRIBUTED AIRFLOW SENSING 审中-公开
公开(公告)号：WO2018156335A3
公开(公告)日：2018-08-30
申请号：PCT/US2018/016631
申请日：2018-02-02
申请人： AURORA FLIGHT SCIENCES CORPORATION
发明人： GRIFFIN, Riley , LIEU, Michael
IPC分类号： B64D45/00 , B64C3/00 , B64C13/18 , G01L13/06 , G01L15/00 , G01L9/00
摘要： Disclosed herein is a distributed pressure sensor system that quickly detects and counters changes in lift, onset of stall, and flutter. The distributed pressure sensor system may employ a plurality of integrated pressure ports distributed across the span of a wing's leading edge to gather differential pressure measurements. Based on the differential pressure measurements, the distributed pressure sensor system can estimate torque on the fuselage to provide a more efficient estimate for changes in lift, onset of stall, and/or flutter. These estimates may be applied as feedback to the aircraft's control system, thereby eliminating the latency in the existing platform dynamics.

6. 发明申请

WO2017165481A1 AIRCREW AUTOMATION SYSTEM AND METHOD 审中-公开
标题翻译： AIRCREW自动化系统和方法
公开(公告)号：WO2017165481A1
公开(公告)日：2017-09-28
申请号：PCT/US2017/023523
申请日：2017-03-22
申请人： AURORA FLIGHT SCIENCES CORPORATION
发明人： DUDA, Jessica E. , TYLKO, John , MINDELL, David , KUNZI, Fabrice , PIEDMONTE, Michael , ALLEE, John , TORGERSON, Joshua , RYAN, Jason , PADUANO, James Donald , WISSLER, John Brooke , MUSTO, Andrew , FEENSTRA, Wendy
IPC分类号： B64C13/18 , G06F3/041 , B64D45/00
摘要： An aircrew automation system that provides a pilot with high-fidelity knowledge of the aircraft's physical state, and notifies that pilot of any deviations in expected state based on predictive models. The aircrew automation may be provided as a non-invasive ride-along aircrew automation system that perceives the state of the aircraft through visual techniques, derives the aircraft state vector and other aircraft information, and communicates any deviations from expected aircraft state to the pilot.
摘要翻译：
一种机组自动化系统，为飞行员提供对飞机物理状态的高保真度知识，并基于预测模型通知飞行员任何预期状态的偏差。机组自动化可以作为非侵入式骑乘机组自动化系统提供，其通过视觉技术感知飞机的状态，导出飞行器状态向量和其他飞机信息，并向飞行员传达与预期飞行器状态的偏差。

7. 发明申请

WO2006069291A3 SYSTEM AND METHOD FOR UTILIZING STORED ELECTRICAL ENERGY FOR VTOL AIRCRAFT THRUST ENHANCEMENT AND ATTITUDE CONTROL 审中-公开
公开(公告)号：WO2006069291A3
公开(公告)日：2006-06-29
申请号：PCT/US2005/046728
申请日：2005-12-22
申请人： AURORA FLIGHT SCIENCES CORPORATION , PARKS, Robert
发明人： PARKS, Robert
IPC分类号： B64C15/12
摘要： A system and method are provided for a short take-off and landing/vertical take-off and landing aircraft that stores required take-off power in the form of primarily an electric fan engine, and secondarily in the form of an internal combustion engine, wherein the combined power of the electric fan and internal combustion engines can cause the STOL/VTOL A/C to take-off in substantially less amount of time and space than other STOL/VTOL A/C, and further wherein the transition from vertical to horizontal thrust is carefully executed to rapidly rise from the take-off position to a forward flight position, thereby minimizing the necessity for a larger electric fan engine.

8. 发明申请

WO2018148248A1 UAV BOOSTER AIRCRAFT FOR TAKEOFF AND CLIMB ASSIST 审中-公开
公开(公告)号：WO2018148248A1
公开(公告)日：2018-08-16
申请号：PCT/US2018/017171
申请日：2018-02-07
申请人： AURORA FLIGHT SCIENCES CORPORATION
发明人： PARKS, Robert W. , GRIFFIN, Riley C. , COURTIN, Christopher , KAUFMAN, Amanda , CLANCY, Thomas
IPC分类号： B64C39/02 , B64D5/00
CPC分类号： B64C39/024 , B64C19/00 , B64C37/02 , B64C2201/021 , B64C2201/12 , B64C2201/141 , B64D5/00
摘要： Disclosed herein is a booster aircraft system having a host aircraft and one or more booster UAVs coupled thereto. When necessary, such as during takeoff and climb of the host aircraft, the booster UAVs operate to boost the thrust of the host aircraft. The booster UAVs are configured to detach from the host aircraft when no longer needed (e.g., at cruising altitude/speed), thus removing their weight from the host aircraft. Each booster UAV includes wings, one or more propulsors, a control system, and landing gear, which enable the booster UAV to return autonomously to a predetermined location once detached from the host aircraft to be refueled and reused.

9. 发明申请

WO2013103403A2 HARDWARE-BASED WEIGHT AND RANGE LIMITATION SYSTEM, APPARATUS AND METHOD 审中-公开
标题翻译：基于硬件的重量和范围限制系统，装置和方法
公开(公告)号：WO2013103403A2
公开(公告)日：2013-07-11
申请号：PCT/US2012/058323
申请日：2012-10-01
申请人： AURORA FLIGHT SCIENCES CORPORATION
发明人： WASHINGTON, Tom , HISAM, Thorsten , GOMEZ, Martin
IPC分类号： G06F17/00
CPC分类号： B64C13/18 , B64C2201/145 , B64D45/00 , G05D1/0055 , G08G5/0021 , G08G5/0039 , G08G5/006
摘要： The present disclosure endeavors to provide systems, methods and apparatus for ensuring aircraft compliance with governmental guidelines, such as, for example, MRCR Category II compliance. A hardware-based system may be employed to reduce range and/or payload below predetermined ranges and a payload capacities. Also provided herein are hardware-based systems, methods, and apparatus for restricting a system's range to predetermined range and/or the payload to a predetermined limit using, for example, a Application-Specific Integrated Circuit (ASIC) installed in the flight control system.
摘要翻译：本公开努力提供用于确保飞机遵守政府准则的系统，方法和装置，例如MRCR II类合规。可以采用基于硬件的系统来减小低于预定范围和有效载荷容量的范围和/或有效载荷。本文还提供了基于硬件的系统，方法和装置，其使用例如安装在飞行控制系统中的专用集成电路（ASIC）将系统的范围限制到预定范围和/或有效负载到预定极限。

10. 发明申请

WO2009036465A1 NON-PLANAR ADAPTIVE WING SOLAR AIRCRAFT 审中-公开
标题翻译：非平面自适应太阳能飞机
公开(公告)号：WO2009036465A1
公开(公告)日：2009-03-19
申请号：PCT/US2008/076462
申请日：2008-09-15
申请人： AURORA FLIGHT SCIENCES CORPORATION , PARKS, Robert
发明人： PARKS, Robert
IPC分类号： B64D27/00
CPC分类号： B64C3/16 , B64D27/24 , Y02T50/12 , Y02T50/44 , Y02T50/62
摘要： A system and method for assembling and operating a solar powered aircraft, composed of one or more modular constituent wing panels. Each wing panel includes at least one hinge interface that is configured to rotationally interface with a complementary hinge interface on another wing panel. When a first and second wing panel are coupled together via the rotational interface, they can rotate with respect to each other within a predetermined angular range. The aircraft further comprises a control system that is configured to acquire aircraft operating information and atmospheric information and use the same alter the angle between the wing panels, even if there are multiple wing panels. One or more of the wing panels can include photovoltaic cells and/or solar thermal cells to convert sol radiation energy or solar heat energy into electricity, that can be used to power electric motors.
摘要翻译：一种用于组装和操作太阳能飞行器的系统和方法，由一个或多个模块化组件翼板组成。每个翼板包括至少一个铰链接口，其被配置为与另一翼板上的互补铰链接口旋转地接合。当第一和第二翼板通过旋转接口联接在一起时，它们可以在预定角度范围内相对于彼此旋转。飞机还包括控制系统，其被配置为获取飞行器操作信息和大气信息，并且使用该控制系统改变翼板之间的角度，即使存在多个翼板。一个或多个翼板可以包括光电池和/或太阳能热电池，以将溶胶辐射能量或太阳能热能转换成电能，其可用于为电动机提供动力。

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