IL240373B - Constraints driven autonomous aircraft navigation - Google Patents

Constraints driven autonomous aircraft navigation

Info

Publication number
IL240373B
IL240373B IL240373A IL24037315A IL240373B IL 240373 B IL240373 B IL 240373B IL 240373 A IL240373 A IL 240373A IL 24037315 A IL24037315 A IL 24037315A IL 240373 B IL240373 B IL 240373B
Authority
IL
Israel
Prior art keywords
flight
aircraft
aircraft navigation
autonomous aircraft
constraint
Prior art date
Application number
IL240373A
Other languages
Hebrew (he)
Other versions
IL240373A0 (en
Inventor
Rozenberg Ohad
Original Assignee
Israel Aerospace Ind Ltd
Rozenberg Ohad
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=55022916&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=IL240373(B) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Israel Aerospace Ind Ltd, Rozenberg Ohad filed Critical Israel Aerospace Ind Ltd
Priority to IL240373A priority Critical patent/IL240373B/en
Publication of IL240373A0 publication Critical patent/IL240373A0/en
Priority to PCT/IL2016/050835 priority patent/WO2017021955A1/en
Publication of IL240373B publication Critical patent/IL240373B/en

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/10Simultaneous control of position or course in three dimensions
    • G05D1/101Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • G05D1/106Change initiated in response to external conditions, e.g. avoidance of elevated terrain or of no-fly zones
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B7/00Radio transmission systems, i.e. using radiation field
    • H04B7/14Relay systems
    • H04B7/15Active relay systems
    • H04B7/185Space-based or airborne stations; Stations for satellite systems
    • H04B7/18502Airborne stations
    • H04B7/18506Communications with or from aircraft, i.e. aeronautical mobile service
    • H04B7/18508Communications with or from aircraft, i.e. aeronautical mobile service with satellite system used as relay, i.e. aeronautical mobile satellite service
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00UAVs characterised by their flight controls
    • B64U2201/10UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
    • B64U2201/104UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS] using satellite radio beacon positioning systems, e.g. GPS

Abstract

The presently disclosed subject matter is related to avoidance of violation of a flight constraint by an autonomously controlled aircraft. Responsive to information indicative of a flight constraint, a bank angle which allows the aircraft to proceed towards a desired destination along a flight path without violating the flight constraint is calculated; and instructions to aerial control devices for guiding the aircraft along the flight path are generated accordingly.
IL240373A 2015-08-05 2015-08-05 Constraints driven autonomous aircraft navigation IL240373B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
IL240373A IL240373B (en) 2015-08-05 2015-08-05 Constraints driven autonomous aircraft navigation
PCT/IL2016/050835 WO2017021955A1 (en) 2015-08-05 2016-07-31 Constraints driven autonomous aircraft navigation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IL240373A IL240373B (en) 2015-08-05 2015-08-05 Constraints driven autonomous aircraft navigation

Publications (2)

Publication Number Publication Date
IL240373A0 IL240373A0 (en) 2015-11-30
IL240373B true IL240373B (en) 2020-05-31

Family

ID=55022916

Family Applications (1)

Application Number Title Priority Date Filing Date
IL240373A IL240373B (en) 2015-08-05 2015-08-05 Constraints driven autonomous aircraft navigation

Country Status (2)

Country Link
IL (1) IL240373B (en)
WO (1) WO2017021955A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6133506B2 (en) * 2014-04-17 2017-05-24 エスゼット ディージェイアイ テクノロジー カンパニー リミテッドSz Dji Technology Co.,Ltd Flight control for flight restricted areas
EP4198672A1 (en) 2015-03-31 2023-06-21 SZ DJI Technology Co., Ltd. Open platform for restricted region
CN110362098B (en) * 2018-03-26 2022-07-05 北京京东尚科信息技术有限公司 Unmanned aerial vehicle visual servo control method and device and unmanned aerial vehicle
CN111381602B (en) * 2018-12-29 2023-09-19 杭州海康威视数字技术股份有限公司 Unmanned aerial vehicle flight control method and device and unmanned aerial vehicle
CN109947123B (en) * 2019-02-27 2021-06-22 南京航空航天大学 Unmanned aerial vehicle path tracking and autonomous obstacle avoidance method based on sight guidance law
CN110296698B (en) * 2019-07-12 2023-04-28 贵州电网有限责任公司 Unmanned aerial vehicle path planning method taking laser scanning as constraint

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8538673B2 (en) * 2008-10-31 2013-09-17 Czech Technical University In Prague System and method for planning/replanning collision free flight plans in real or accelerated time
US9262933B2 (en) * 2009-11-13 2016-02-16 The Boeing Company Lateral avoidance maneuver solver
US8798922B2 (en) * 2012-11-16 2014-08-05 The Boeing Company Determination of flight path for unmanned aircraft in event of in-flight contingency

Also Published As

Publication number Publication date
WO2017021955A1 (en) 2017-02-09
IL240373A0 (en) 2015-11-30

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