IL249929B - Autonomous takeoff and landing by an aircraft - Google Patents

Autonomous takeoff and landing by an aircraft

Info

Publication number
IL249929B
IL249929B IL249929A IL24992917A IL249929B IL 249929 B IL249929 B IL 249929B IL 249929 A IL249929 A IL 249929A IL 24992917 A IL24992917 A IL 24992917A IL 249929 B IL249929 B IL 249929B
Authority
IL
Israel
Prior art keywords
aircraft
points
generated
runway
takeoff
Prior art date
Application number
IL249929A
Other languages
Hebrew (he)
Other versions
IL249929A0 (en
Inventor
Dekel Guy
Zivan Lior
Original Assignee
Israel Aerospace Ind Ltd
Dekel Guy
Zivan Lior
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 Israel Aerospace Ind Ltd, Dekel Guy, Zivan Lior filed Critical Israel Aerospace Ind Ltd
Priority to IL249929A priority Critical patent/IL249929B/en
Publication of IL249929A0 publication Critical patent/IL249929A0/en
Priority to PCT/IL2017/051340 priority patent/WO2018127903A1/en
Publication of IL249929B publication Critical patent/IL249929B/en

Links

Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/06—Traffic control systems for aircraft, e.g. air-traffic control [ATC] for control when on the ground
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0047—Navigation or guidance aids for a single aircraft
    • G08G5/0069—Navigation or guidance aids for a single aircraft specially adapted for an unmanned aircraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0004—Transmission of traffic-related information to or from an aircraft
    • G08G5/0013—Transmission of traffic-related information to or from an aircraft with a ground station
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
    • G08G5/0021—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0047—Navigation or guidance aids for a single aircraft
    • G08G5/0065—Navigation or guidance aids for a single aircraft for taking-off
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
    • G08G5/025—Navigation or guidance aids

Abstract

According to the disclosed subject matter a runway path is generated, in real-time, as the aircraft proceeds in the general takeoff direction along the runway surface. As part of the initial stages of the takeoff process, one or more reference points are selected, where accurate positioning of the reference point is not necessary. The runway path is generated based on points which are sampled in real-time as the aircraft progresses along the runway surface. Sampling includes determining the relative position of points in relation to the one or more reference points. A line representing the runway path and extending in the general takeoff direction is generated based on the collection of sampled points. If the aircraft deviates from the intended takeoff direction and/or from the generated line, appropriate steering commands are generated for correcting the deviation and maintaining the aircraft on course.
IL249929A 2017-01-04 2017-01-04 Autonomous takeoff and landing by an aircraft IL249929B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
IL249929A IL249929B (en) 2017-01-04 2017-01-04 Autonomous takeoff and landing by an aircraft
PCT/IL2017/051340 WO2018127903A1 (en) 2017-01-04 2017-12-12 Autonomous takeoff and landing by an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IL249929A IL249929B (en) 2017-01-04 2017-01-04 Autonomous takeoff and landing by an aircraft

Publications (2)

Publication Number Publication Date
IL249929A0 IL249929A0 (en) 2017-06-29
IL249929B true IL249929B (en) 2020-09-30

Family

ID=62454698

Family Applications (1)

Application Number Title Priority Date Filing Date
IL249929A IL249929B (en) 2017-01-04 2017-01-04 Autonomous takeoff and landing by an aircraft

Country Status (2)

Country Link
IL (1) IL249929B (en)
WO (1) WO2018127903A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115273558A (en) * 2022-06-23 2022-11-01 成都民航空管科技发展有限公司 Method and system for alarming inconformity of turning at one side of aircraft after takeoff

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7364121B2 (en) * 2005-03-14 2008-04-29 The Boeing Company Methods and systems for automatically controlling aircraft takeoff rolls
US20110040431A1 (en) * 2009-08-11 2011-02-17 Honeywell International Inc. Automated take off control system and method
US8560149B1 (en) * 2012-09-20 2013-10-15 Honeywell International Inc. Systems and methods for takeoff assistance and analysis
FR3013495B1 (en) * 2013-11-15 2021-05-07 Airbus Operations Sas METHOD AND DEVICE FOR AUTOMATIC GUIDANCE OF A RUNNING AIRCRAFT.
US9406235B2 (en) * 2014-04-10 2016-08-02 Honeywell International Inc. Runway location determination

Also Published As

Publication number Publication date
WO2018127903A1 (en) 2018-07-12
IL249929A0 (en) 2017-06-29

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Legal Events

Date Code Title Description
FF Patent granted
MM9K Patent not in force due to non-payment of renewal fees