AU2001281272A1 - Attitude determination using a global positioning system - Google Patents

Attitude determination using a global positioning system

Info

Publication number
AU2001281272A1
AU2001281272A1 AU2001281272A AU8127201A AU2001281272A1 AU 2001281272 A1 AU2001281272 A1 AU 2001281272A1 AU 2001281272 A AU2001281272 A AU 2001281272A AU 8127201 A AU8127201 A AU 8127201A AU 2001281272 A1 AU2001281272 A1 AU 2001281272A1
Authority
AU
Australia
Prior art keywords
positioning system
global positioning
attitude determination
attitude
determination
Prior art date
Legal status (The legal status 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 status listed.)
Abandoned
Application number
AU2001281272A
Inventor
Laurence H. Mutuel
Jason L. Speyer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
University of California
Original Assignee
University of California
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 University of California filed Critical University of California
Publication of AU2001281272A1 publication Critical patent/AU2001281272A1/en
Abandoned legal-status Critical Current

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
    • G05D1/08Control 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
    • G05D1/0816Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0825Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using mathematical models
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/165Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation combined with non-inertial navigation instruments
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/53Determining attitude
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S5/00Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
    • G01S5/02Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
    • G01S5/0247Determining attitude
AU2001281272A 2000-08-11 2001-08-13 Attitude determination using a global positioning system Abandoned AU2001281272A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US22491600P 2000-08-11 2000-08-11
US60224916 2000-08-11
PCT/US2001/025456 WO2002014890A2 (en) 2000-08-11 2001-08-13 Attitude determination using a global positioning system

Publications (1)

Publication Number Publication Date
AU2001281272A1 true AU2001281272A1 (en) 2002-02-25

Family

ID=22842755

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001281272A Abandoned AU2001281272A1 (en) 2000-08-11 2001-08-13 Attitude determination using a global positioning system

Country Status (3)

Country Link
US (1) US6580389B2 (en)
AU (1) AU2001281272A1 (en)
WO (1) WO2002014890A2 (en)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7269460B2 (en) * 2003-02-28 2007-09-11 Medtronic, Inc. Method and apparatus for evaluating and optimizing ventricular synchronization
US20050114023A1 (en) * 2003-11-26 2005-05-26 Williamson Walton R. Fault-tolerant system, apparatus and method
US20060074558A1 (en) * 2003-11-26 2006-04-06 Williamson Walton R Fault-tolerant system, apparatus and method
JP5127128B2 (en) * 2004-12-21 2013-01-23 韓國電子通信研究院 Camera position and orientation information correction method and apparatus
US8305265B2 (en) 2007-05-29 2012-11-06 Toyon Research Corporation Radio-based direction-finding navigation system using small antenna
US20080303714A1 (en) * 2007-05-29 2008-12-11 Ezal Kenan O Compact single-aperture antenna and navigation system
TWI374257B (en) * 2008-04-29 2012-10-11 Ind Tech Res Inst Method for modifying navigation information and navigation apparatus using the same
FR2955934B1 (en) * 2010-01-29 2012-03-09 Eurocopter France ESTIMATION STABILIZED IN TURNING ANGLES OF PLATES OF AN AIRCRAFT
US8779971B2 (en) 2010-05-24 2014-07-15 Robert J. Wellington Determining spatial orientation information of a body from multiple electromagnetic signals
US9090263B2 (en) * 2010-07-20 2015-07-28 GM Global Technology Operations LLC Lane fusion system using forward-view and rear-view cameras
WO2012119132A2 (en) 2011-03-02 2012-09-07 Aerovironment, Inc. Unmanned aerial vehicle angular reorientation
CN102621565B (en) * 2012-04-17 2013-12-04 北京航空航天大学 Transfer aligning method of airborne distributed POS (Position and Orientation System)
US9910130B2 (en) * 2014-02-10 2018-03-06 The Boeing Company Geo-location using known target co-calibration
US10031234B1 (en) 2015-04-03 2018-07-24 Interstate Electronics Corporation Global navigation satellite system beam based attitude determination
US10024973B1 (en) 2015-04-03 2018-07-17 Interstate Electronics Corporation Global navigation satellite system spoofer identification technique
CN106547275A (en) * 2015-09-17 2017-03-29 西安翔舟航空技术有限公司 A kind of new rotor class unmanned plane is automatically positioned control method
US10545246B1 (en) 2016-07-08 2020-01-28 Interstate Electronics Corporation Global navigation satellite system spoofer identification technique based on carrier to noise ratio signatures
CN109144081A (en) * 2017-06-16 2019-01-04 袁兵 Unmanned plane during flying attitude control method based on Kalman filtering
US10725182B2 (en) 2018-01-04 2020-07-28 Interstate Electronics Corporation Systems and methods for providing anti-spoofing capability to a global navigation satellite system receiver

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4754280A (en) * 1982-09-10 1988-06-28 The Charles Stark Draper Laboratory, Inc. Attitude sensing system
IL130227A0 (en) 1996-12-05 2000-06-01 Parvez Shabbir Ahmed Autonomous on-board orbit control/maintenance system for satellites

Also Published As

Publication number Publication date
US6580389B2 (en) 2003-06-17
WO2002014890A3 (en) 2002-05-10
WO2002014890A2 (en) 2002-02-21
US20020021243A1 (en) 2002-02-21

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