SG11201404978TA - Safe emergency landing of a uav - Google Patents

Safe emergency landing of a uav

Info

Publication number
SG11201404978TA
SG11201404978TA SG11201404978TA SG11201404978TA SG11201404978TA SG 11201404978T A SG11201404978T A SG 11201404978TA SG 11201404978T A SG11201404978T A SG 11201404978TA SG 11201404978T A SG11201404978T A SG 11201404978TA SG 11201404978T A SG11201404978T A SG 11201404978TA
Authority
SG
Singapore
Prior art keywords
uav
emergency landing
safe emergency
safe
landing
Prior art date
Application number
SG11201404978TA
Inventor
Reuven Godel
Roy Mor
Eyal Ben-Shachar
Original Assignee
Elbit Systems Ltd
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 Elbit Systems Ltd filed Critical Elbit Systems Ltd
Publication of SG11201404978TA publication Critical patent/SG11201404978TA/en

Links

Classifications

    • 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
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • 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
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/40—Landing characterised by flight manoeuvres, e.g. deep stall
    • 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
    • G05D1/0072—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements to counteract a motor failure
    • 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
    • G05D1/0088—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot characterized by the autonomous decision making process, e.g. artificial intelligence, predefined behaviours
    • 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
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • G05D1/105—Simultaneous control of position or course in three dimensions specially adapted for aircraft specially adapted for unpowered flight, e.g. glider, parachuting, forced landing
    • 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
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • G05D1/106—Change initiated in response to external conditions, e.g. avoidance of elevated terrain or of no-fly zones
    • 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]
SG11201404978TA 2012-02-26 2013-02-21 Safe emergency landing of a uav SG11201404978TA (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IL218327A IL218327A (en) 2012-02-26 2012-02-26 Safe emergency landing of a uav
PCT/IL2013/050157 WO2013124852A1 (en) 2012-02-26 2013-02-21 Safe emergency landing of a uav

Publications (1)

Publication Number Publication Date
SG11201404978TA true SG11201404978TA (en) 2014-09-26

Family

ID=46467097

Family Applications (1)

Application Number Title Priority Date Filing Date
SG11201404978TA SG11201404978TA (en) 2012-02-26 2013-02-21 Safe emergency landing of a uav

Country Status (8)

Country Link
US (1) US9274529B2 (en)
EP (1) EP2817689B1 (en)
CN (1) CN104246641B (en)
IL (1) IL218327A (en)
PL (1) PL2817689T3 (en)
RU (1) RU2568510C1 (en)
SG (1) SG11201404978TA (en)
WO (1) WO2013124852A1 (en)

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Also Published As

Publication number Publication date
EP2817689A1 (en) 2014-12-31
CN104246641B (en) 2017-03-15
WO2013124852A1 (en) 2013-08-29
CN104246641A (en) 2014-12-24
EP2817689A4 (en) 2016-01-06
PL2817689T3 (en) 2017-08-31
US9274529B2 (en) 2016-03-01
EP2817689B1 (en) 2016-12-14
IL218327A (en) 2013-05-30
RU2568510C1 (en) 2015-11-20
IL218327A0 (en) 2012-06-28
US20150153740A1 (en) 2015-06-04

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