SG11202000769QA - Asymmetric can-based communication for aerial vehicles - Google Patents

Asymmetric can-based communication for aerial vehicles

Info

Publication number
SG11202000769QA
SG11202000769QA SG11202000769QA SG11202000769QA SG11202000769QA SG 11202000769Q A SG11202000769Q A SG 11202000769QA SG 11202000769Q A SG11202000769Q A SG 11202000769QA SG 11202000769Q A SG11202000769Q A SG 11202000769QA SG 11202000769Q A SG11202000769Q A SG 11202000769QA
Authority
SG
Singapore
Prior art keywords
asymmetric
based communication
aerial vehicles
aerial
vehicles
Prior art date
Application number
SG11202000769QA
Inventor
Parsa Dormiani
Brian Viele
Original Assignee
Wing Aviation Llc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wing Aviation Llc filed Critical Wing Aviation Llc
Publication of SG11202000769QA publication Critical patent/SG11202000769QA/en

Links

Classifications

    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L12/00—Data switching networks
    • H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
    • H04L12/40—Bus networks
    • H04L12/40169—Flexible bus arrangements
    • H04L12/40176—Flexible bus arrangements involving redundancy
    • H04L12/40195—Flexible bus arrangements involving redundancy by using a plurality of nodes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/503—Fly-by-Wire
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/04—Aircraft not otherwise provided for having multiple fuselages or tail booms
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0055—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
    • G05D1/0077—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements using redundant signals or controls
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/10—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/10—Wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/80—Vertical take-off or landing, e.g. using rockets
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L12/00—Data switching networks
    • H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
    • H04L12/40—Bus networks
    • H04L12/40169—Flexible bus arrangements
    • H04L12/40176—Flexible bus arrangements involving redundancy
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L12/00—Data switching networks
    • H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
    • H04L12/40—Bus networks
    • H04L2012/40208—Bus networks characterized by the use of a particular bus standard
    • H04L2012/40215—Controller Area Network CAN
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L12/00—Data switching networks
    • H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
    • H04L12/40—Bus networks
    • H04L2012/40267—Bus for use in transportation systems
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L12/00—Data switching networks
    • H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
    • H04L12/40—Bus networks
    • H04L2012/40267—Bus for use in transportation systems
    • H04L2012/4028—Bus for use in transportation systems the transportation system being an aircraft
SG11202000769QA 2017-07-27 2018-07-27 Asymmetric can-based communication for aerial vehicles SG11202000769QA (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/661,974 US10382225B2 (en) 2017-07-27 2017-07-27 Asymmetric CAN-based communication for aerial vehicles
PCT/US2018/044001 WO2019023527A1 (en) 2017-07-27 2018-07-27 Asymmetric can-based communication for aerial vehicles

Publications (1)

Publication Number Publication Date
SG11202000769QA true SG11202000769QA (en) 2020-02-27

Family

ID=63371767

Family Applications (1)

Application Number Title Priority Date Filing Date
SG11202000769QA SG11202000769QA (en) 2017-07-27 2018-07-27 Asymmetric can-based communication for aerial vehicles

Country Status (6)

Country Link
US (2) US10382225B2 (en)
EP (1) EP3658457B1 (en)
CN (2) CN116331473A (en)
AU (1) AU2018307808B2 (en)
SG (1) SG11202000769QA (en)
WO (1) WO2019023527A1 (en)

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US11136118B2 (en) * 2018-08-30 2021-10-05 Amazon Technologies, Inc. Six degree of freedom aerial vehicle control methods responsive to motor out situations
US11097834B2 (en) 2019-02-19 2021-08-24 Honeywell International Inc. Fly-by-wire systems and related operating methods
WO2020180381A1 (en) 2019-03-01 2020-09-10 United Technologies Advanced Projects, Inc. Indicators for hybrid electrical powerplants
EP3931098A4 (en) 2019-03-01 2022-11-16 Pratt & Whitney Canada Corp. Normal mode operation of hybrid electric propulsion systems
US11597526B2 (en) 2019-04-25 2023-03-07 Pratt & Whitney Canada Corp. Control systems for hybrid electric powerplants
US11273906B2 (en) * 2019-05-10 2022-03-15 Honeywell International Inc. Redundant fly-by-wire systems with fault resiliency
CN111045451B (en) * 2019-12-16 2022-10-18 西安航空学院 Control system of aircraft and aircraft
EP4078322A1 (en) * 2020-05-04 2022-10-26 Auterion AG System and method for software-defined drones
US11794917B2 (en) 2020-05-15 2023-10-24 Pratt & Whitney Canada Corp. Parallel control loops for hybrid electric aircraft
US11958622B2 (en) 2020-05-15 2024-04-16 Pratt & Whitney Canada Corp. Protection functions
CN112147928B (en) * 2020-09-15 2022-02-25 北京神州飞航科技有限责任公司 Dual-CAN-bus multi-redundancy hot backup flight control computer system and method
CN112491678A (en) * 2020-11-16 2021-03-12 无锡锐科光纤激光技术有限责任公司 Digital level transmission circuit and method
EP3998200B1 (en) * 2021-02-19 2024-04-24 Lilium eAircraft GmbH Fault tolerant aircraft flight control system
US20220306294A1 (en) * 2021-03-25 2022-09-29 Textron Systems Corporation Flight control arrangement using separate fixed-wing and vtol control modules
US11435761B1 (en) * 2021-07-23 2022-09-06 Beta Air, Llc System and method for distributed flight control system for an electric vehicle
CN113848977B (en) * 2021-10-09 2023-12-22 广东汇天航空航天科技有限公司 Aircraft control method and system and flight controller
WO2023062751A1 (en) * 2021-10-13 2023-04-20 株式会社Acsl Controller and drone system
CN114281744A (en) * 2021-12-23 2022-04-05 北京天融信网络安全技术有限公司 CAN bus relay circuit, control method, device and electronic equipment

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Also Published As

Publication number Publication date
EP3658457B1 (en) 2022-01-26
US20190334741A1 (en) 2019-10-31
US10382225B2 (en) 2019-08-13
EP3658457A1 (en) 2020-06-03
CN111132900B (en) 2022-12-27
AU2018307808B2 (en) 2021-04-22
WO2019023527A1 (en) 2019-01-31
US11240062B2 (en) 2022-02-01
US20190036732A1 (en) 2019-01-31
CN111132900A (en) 2020-05-08
CN116331473A (en) 2023-06-27
AU2018307808A1 (en) 2020-03-05

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