HK34397A - Method and device for determining an orientation related to a mobile system particularly the line of sight in a helmet sighting - Google Patents
Method and device for determining an orientation related to a mobile system particularly the line of sight in a helmet sightingInfo
- Publication number
- HK34397A HK34397A HK34397A HK34397A HK34397A HK 34397 A HK34397 A HK 34397A HK 34397 A HK34397 A HK 34397A HK 34397 A HK34397 A HK 34397A HK 34397 A HK34397 A HK 34397A
- Authority
- HK
- Hong Kong
- Prior art keywords
- sight
- line
- cockpit
- sensor
- transmitter
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
- G01S3/02—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves
- G01S3/14—Systems for determining direction or deviation from predetermined direction
- G01S3/143—Systems for determining direction or deviation from predetermined direction by vectorial combination of signals derived from differently oriented antennae
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G3/00—Aiming or laying means
- F41G3/22—Aiming or laying means for vehicle-borne armament, e.g. on aircraft
- F41G3/225—Helmet sighting systems
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
- G01S3/02—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves
- G01S3/023—Monitoring or calibrating
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Measurement Of Length, Angles, Or The Like Using Electric Or Magnetic Means (AREA)
- Helmets And Other Head Coverings (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Measuring Magnetic Variables (AREA)
- Length Measuring Devices By Optical Means (AREA)
- Length Measuring Devices With Unspecified Measuring Means (AREA)
Abstract
A method for determining a line of sight from a sighting device mounted on a helmet provided with a sensor (2) with three orthogonal magnetic coils, in relation to a reference attached to an aircraft and having the form of a transmitter (1) having three orthogonal magnetic coils. According to the method, the cockpit is first magnetically mapped. For this purpose, sets of field measurements detected by the sensor for the fields successively produced by the transmitter's three coils for various known positions and attitudes of the sensor in the cockpit are established and memorized. Then, the cockpit is magnetically modelled on the basis of said measurements. In flight, the matrix of measurements, combined with a transmitter transmission cycle initiated when the pilot confirms a directional line of sight determined in relation to his helmet, allows the orientation of said line of sight in the aircraft reference to be accurately calculated on the basis of the model previously made. The method can be used for sighting from helicopters where the cockpit causes disturbances because of field reflexions from metal components.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9008230A FR2664044B1 (en) | 1990-06-29 | 1990-06-29 | METHOD AND DEVICE FOR DETERMINING AN ORIENTATION LINKED TO A MOBILE SYSTEM, IN PARTICULAR OF THE SIGHT LINE IN A HELMET VIEWFINDER. |
PCT/FR1991/000478 WO1992000529A1 (en) | 1990-06-29 | 1991-06-14 | Method and device for determining an orientation related to a mobile system, particularly the line of sight in a helmet sighting |
Publications (1)
Publication Number | Publication Date |
---|---|
HK34397A true HK34397A (en) | 1997-03-27 |
Family
ID=9398165
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
HK34397A HK34397A (en) | 1990-06-29 | 1997-03-20 | Method and device for determining an orientation related to a mobile system particularly the line of sight in a helmet sighting |
Country Status (9)
Country | Link |
---|---|
EP (1) | EP0536184B1 (en) |
JP (1) | JP2994463B2 (en) |
AT (1) | ATE109897T1 (en) |
CA (1) | CA2086234A1 (en) |
DE (1) | DE69103422T2 (en) |
ES (1) | ES2057902T3 (en) |
FR (1) | FR2664044B1 (en) |
HK (1) | HK34397A (en) |
WO (1) | WO1992000529A1 (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5307072A (en) * | 1992-07-09 | 1994-04-26 | Polhemus Incorporated | Non-concentricity compensation in position and orientation measurement systems |
FR2722299B1 (en) * | 1994-07-05 | 1996-08-14 | Sextant Avionique | METHOD FOR COMPENSATING FOR ELETROMAGNETIC DISTURBANCES DUE TO MAGNETIC ELEMENTS AND MOBILE CONDUCTORS, APPLIED IN PARTICULAR TO A HELMET VIEWFINDER |
US6154024A (en) * | 1998-05-22 | 2000-11-28 | Honeywell, Inc. | Metal immune magnetic tracker |
IL137520A (en) | 2000-07-25 | 2010-06-16 | Elbit Systems Ltd | Estimating position and orientation in electromagnetic systems |
CA2507639C (en) | 2002-11-29 | 2013-08-06 | Rhodia Organique Fine Limited | Chiller refrigerants |
JP4577196B2 (en) * | 2005-11-30 | 2010-11-10 | 株式会社島津製作所 | Magnetic mapping apparatus and its mounting position correction method |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2458838A1 (en) * | 1979-06-06 | 1981-01-02 | Thomson Csf | DEVICE FOR MEASURING THE RELATIVE ORIENTATION OF TWO BODIES AND CORRESPONDING STEERING SYSTEM |
US4287809A (en) * | 1979-08-20 | 1981-09-08 | Honeywell Inc. | Helmet-mounted sighting system |
US4688037A (en) * | 1980-08-18 | 1987-08-18 | Mcdonnell Douglas Corporation | Electromagnetic communications and switching system |
DE3326254A1 (en) * | 1983-07-21 | 1985-01-31 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | Direction-finding receiver with several direction-finding channels |
GB2173079B (en) * | 1985-03-29 | 1988-05-18 | Ferranti Plc | Cursor display control apparatus |
DE3834331A1 (en) * | 1988-10-08 | 1990-04-12 | Rohde & Schwarz | HIGH-FREQUENCY DIARING PROCESS FOR MOBILE USE, IN PARTICULAR IN MOTOR VEHICLES |
-
1990
- 1990-06-29 FR FR9008230A patent/FR2664044B1/en not_active Expired - Fee Related
-
1991
- 1991-06-14 AT AT91910960T patent/ATE109897T1/en active
- 1991-06-14 WO PCT/FR1991/000478 patent/WO1992000529A1/en active IP Right Grant
- 1991-06-14 ES ES91910960T patent/ES2057902T3/en not_active Expired - Lifetime
- 1991-06-14 DE DE69103422T patent/DE69103422T2/en not_active Expired - Fee Related
- 1991-06-14 JP JP3510740A patent/JP2994463B2/en not_active Expired - Fee Related
- 1991-06-14 CA CA002086234A patent/CA2086234A1/en not_active Abandoned
- 1991-06-14 EP EP91910960A patent/EP0536184B1/en not_active Expired - Lifetime
-
1997
- 1997-03-20 HK HK34397A patent/HK34397A/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
CA2086234A1 (en) | 1991-12-30 |
EP0536184A1 (en) | 1993-04-14 |
EP0536184B1 (en) | 1994-08-10 |
DE69103422T2 (en) | 1994-12-01 |
FR2664044B1 (en) | 1993-05-14 |
ATE109897T1 (en) | 1994-08-15 |
ES2057902T3 (en) | 1994-10-16 |
DE69103422D1 (en) | 1994-09-15 |
FR2664044A1 (en) | 1992-01-03 |
JP2994463B2 (en) | 1999-12-27 |
JPH06501543A (en) | 1994-02-17 |
WO1992000529A1 (en) | 1992-01-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CA1311273C (en) | Direct current position measuring device | |
US2471315A (en) | Aircraft trainer for aerial gunners | |
IL102218A0 (en) | Tracker employing a rotating electromagnetic field | |
HK34397A (en) | Method and device for determining an orientation related to a mobile system particularly the line of sight in a helmet sighting | |
CN208297709U (en) | It is a kind of for demarcating the device of round three axis fluxgate magnetometer sensors | |
EP0229468A3 (en) | Magnetic flux detector correction system | |
GOATHAM | An evaluation of the Royal Air Force Shorts Tucano Navigation Instruments Trainer: The NAVIT(M. S. Thesis) | |
CN210375087U (en) | Head rotation angle measuring device | |
Board et al. | Communicating with computers in human terms | |
POLZELLA et al. | Aircrew training devices: Utility and utilization of advanced instructional features, phase 4(Final Summary Report, Oct. 1984- Mar. 1987) | |
CN1054157A (en) | Target information transmission system | |
Hamid | Orientation to authority versus independence of thought in Malayan and New Zealand students | |
Polzella et al. | Aircrew training devices: Utility and utilization of advanced instructional features | |
LEATHAM et al. | A digital lead computing optical sight model[Final Report] | |
Aleva | Field of view effects upon a simulated flight and target acquisition task | |
Polzella et al. | Aircrew training devices: Utility and utilization of advanced instructional features. Phase III: Electronic warfare trainers(Final Report, May- Sep. 1984) | |
RESSEGUIER | Preguidance and piloting with the aid of composite inertial sensors | |
Page | AcSim: Aircraft simulation program with application to flight profile generation | |
Langley et al. | Automatic flightpath calculation and position reporting using a single VOR receiver and a microprocessor system | |
HARRINGTON | Design of a control system to stabilize the aft fuselage of a B-52 bomber in the presence of a random wind gust[M. S. Thesis] | |
BAZANOV | Image of flight article discussed(spatial orientation perception by flight crews flight training) | |
BASARGIN et al. | A hypersonic ballistic facility | |
BEYER et al. | Experimental investigation of a helmet mounted sight/display for helicopter | |
ORMEROD | A system of training in aviation physiology and human factors for Army and Navy helicopter aircrew | |
HOLMES | Control and display concepts for combat aircraft(head-up displays and helmet display sight system) |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PC | Patent ceased (i.e. patent has lapsed due to the failure to pay the renewal fee) |