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WO2003067351A3 - Stabilisation and control of aircraft and other objects - Google Patents

Stabilisation and control of aircraft and other objects Download PDF

Info

Publication number
WO2003067351A3
WO2003067351A3 PCT/GB2003/000588 GB0300588W WO03067351A3 WO 2003067351 A3 WO2003067351 A3 WO 2003067351A3 GB 0300588 W GB0300588 W GB 0300588W WO 03067351 A3 WO03067351 A3 WO 03067351A3
Authority
WO
WIPO (PCT)
Prior art keywords
aircraft
control
stabilisation
objects
disclosed
Prior art date
Application number
PCT/GB2003/000588
Other languages
French (fr)
Other versions
WO2003067351A2 (en
Inventor
Phil Jermyn
Original Assignee
Levitation Technologies Ltd
Phil Jermyn
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
Priority claimed from GB0202899A external-priority patent/GB0202899D0/en
Priority claimed from GBGB0225661.8A external-priority patent/GB0225661D0/en
Application filed by Levitation Technologies Ltd, Phil Jermyn filed Critical Levitation Technologies Ltd
Priority to AU2003244415A priority Critical patent/AU2003244415A1/en
Publication of WO2003067351A2 publication Critical patent/WO2003067351A2/en
Publication of WO2003067351A3 publication Critical patent/WO2003067351A3/en

Links

Classifications

    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63HTOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00Toy aircraft; Other flying toys
    • A63H27/04Captive toy aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02Initiating means
    • B64C13/16Initiating means actuated automatically, e.g. responsive to gust detectors
    • B64C13/20Initiating means actuated automatically, e.g. responsive to gust detectors using radiated signals
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00Measuring arrangements characterised by the use of optical techniques
    • G01B11/26Measuring arrangements characterised by the use of optical techniques for measuring angles or tapers; for testing the alignment of axes
    • G01B11/27Measuring arrangements characterised by the use of optical techniques for measuring angles or tapers; for testing the alignment of axes for testing the alignment of axes
    • G01B11/272Measuring arrangements characterised by the use of optical techniques for measuring angles or tapers; for testing the alignment of axes for testing the alignment of axes using photoelectric detection means
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Toys (AREA)

Abstract

Disclosed is a method of control and stabilisation of aircraft particularly, but not exclusively, to control of miniature aircraft such as model or toy aircraft (102). In one aspect pitch and roll may be controlled by a simple method of signalling to or from a reference location orbeacon (104,106) in a number of different ways. Both height and lateral position may be controlled. In a further aspect, polarised light may be used to determine the relative rotation of the aircraft. Additionally, preferred aircraft and associated features are disclosed.
PCT/GB2003/000588 2002-02-07 2003-02-07 Stabilisation and control of aircraft and other objects WO2003067351A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2003244415A AU2003244415A1 (en) 2002-02-07 2003-02-07 Stabilisation and control of aircraft and other objects

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
GB0202899A GB0202899D0 (en) 2002-02-07 2002-02-07 Aircraft stabilisation and control
GB0202899.1 2002-02-07
GB0225661.8 2002-11-04
GBGB0225661.8A GB0225661D0 (en) 2002-11-04 2002-11-04 Control system for use with flying craft and other remote elements

Publications (2)

Publication Number Publication Date
WO2003067351A2 WO2003067351A2 (en) 2003-08-14
WO2003067351A3 true WO2003067351A3 (en) 2003-12-11

Family

ID=27736190

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB2003/000588 WO2003067351A2 (en) 2002-02-07 2003-02-07 Stabilisation and control of aircraft and other objects

Country Status (2)

Country Link
AU (1) AU2003244415A1 (en)
WO (1) WO2003067351A2 (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0225661D0 (en) * 2002-11-04 2002-12-11 Levitation Technologies Ltd Control system for use with flying craft and other remote elements
ES2305560T3 (en) 2002-09-23 2008-11-01 Captron Electronic Gmbh MEASUREMENT AND STABILIZATION SYSTEM FOR MECHANICALLY CONTROLLED VEHICLES.
DE10258545B4 (en) * 2002-09-23 2008-01-24 Stefan Reich Method and system for stabilizing a translation motion size of a missile
DE102007054126A1 (en) 2007-11-11 2009-05-20 Stefan Reich Unmanned gyroplane for advertising or other display purposes, e.g. sports events or demonstrations, has rigid connecting body formed in elongated manner, where two lift generating rotor devices are provided and spaced at connecting body
US8639400B1 (en) 2012-09-26 2014-01-28 Silverlit Limited Altitude control of an indoor flying toy
US8577520B1 (en) 2012-09-26 2013-11-05 Silverlit Limited Altitude control of an indoor flying toy
US9170435B2 (en) 2013-03-12 2015-10-27 Ge Aviation Systems Llc Method of forming a grid defining a first relative reference frame
JP6207746B2 (en) 2014-05-30 2017-10-04 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 Aircraft attitude control method and apparatus
CN106032166B (en) * 2015-03-12 2018-12-04 优利科技有限公司 Aircraft and overturning method thereof
GB201517378D0 (en) * 2015-10-01 2015-11-18 Snelflight Ltd Guidance system for aircraft and method of use thereof
FR3043337A1 (en) * 2015-11-10 2017-05-12 Parrot DRONE HAVING A TORQUE PROPULSION SUPPORT.
CN107031830A (en) * 2017-05-12 2017-08-11 西华酷农无人机产业园运营有限公司 It is a kind of can be according to the unmanned plane of wind direction self-adjusting balance
FR3085314B1 (en) * 2018-08-28 2020-10-23 Psa Automobiles Sa POSITION DETECTION SYSTEM OF A FIRST MOBILE MACHINE IN RELATION TO A SECOND MACHINE, BY POLARIZED PHOTONS

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3620448A (en) * 1969-09-25 1971-11-16 Honeywell Inc Clock-thermostat system
US5672086A (en) * 1994-11-23 1997-09-30 Dixon; Don Aircraft having improved auto rotation and method for remotely controlling same
WO1999010235A1 (en) * 1997-08-26 1999-03-04 Jermyn Phillip M Helicopter with a gyroscopic rotor and rotor propellers to provide vectored thrust
US6259975B1 (en) * 1998-04-21 2001-07-10 Eurocopter Flight control system for an aircraft particularly for a helicopter

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3620448A (en) * 1969-09-25 1971-11-16 Honeywell Inc Clock-thermostat system
US5672086A (en) * 1994-11-23 1997-09-30 Dixon; Don Aircraft having improved auto rotation and method for remotely controlling same
WO1999010235A1 (en) * 1997-08-26 1999-03-04 Jermyn Phillip M Helicopter with a gyroscopic rotor and rotor propellers to provide vectored thrust
US6259975B1 (en) * 1998-04-21 2001-07-10 Eurocopter Flight control system for an aircraft particularly for a helicopter

Also Published As

Publication number Publication date
WO2003067351A2 (en) 2003-08-14
AU2003244415A1 (en) 2003-09-02

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