WO2011162614A1 - Method and system for positioning of an antenna, telescope, aiming device or similar mounted onto a movable platform - Google Patents
Method and system for positioning of an antenna, telescope, aiming device or similar mounted onto a movable platform Download PDFInfo
- Publication number
- WO2011162614A1 WO2011162614A1 PCT/NO2011/000160 NO2011000160W WO2011162614A1 WO 2011162614 A1 WO2011162614 A1 WO 2011162614A1 NO 2011000160 W NO2011000160 W NO 2011000160W WO 2011162614 A1 WO2011162614 A1 WO 2011162614A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- dome
- antenna
- patterns
- telescope
- rasters
- Prior art date
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
- H01Q1/18—Means for stabilising antennas on an unstable platform
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
- H01Q1/125—Means for positioning
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/42—Housings not intimately mechanically associated with radiating elements, e.g. radome
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
- H01Q3/08—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
Definitions
- the invention is related to a method of performing highly accurate position determination of aiming direction of an antenna, a telescope, aiming device or similar, arranged on a movable platform in a dome, or a part of a dome, and hence an accurate control of the antenna, telescope, aiming device or similar, according to the preamble of claim 1.
- the invention is also related to a system for the same according to the preamble of claim 9. Background
- An antenna arranged to follow a movable sender e.g. a satellite, will usually have a control system based on the use of the receiver's automatic gain control ("AGC - Automatic Gain control
- the AGC voltage from the receiver varies proportionally with the strength of the received signal and can therefore be used as a control signal for the antenna.
- Some systems have adaptive control applications which ensure antenna control with an optimal AGC signal at all times.
- a satellite can also be tracked by turning the antenna system in accordance with a
- the disadvantage of the AGC method is that a continuous and strong signal is required to be able to estimate the direction of the satellite. At weak signals the AGC system may easily provide wrong estimates. The AGC system is also subject to external sources of noise which may cause large errors in the position estimate. AGC controlling alone is therefore a risky strategy for controlling antennas.
- gyro or other motion sensors are normally being used. These will to a certain degree provide estimates of self-motion which can be used to correct the aiming angle of the antenna.
- Antennas of this type are often mounted in a dome to protect the installation against snow, ice and climatic influences.
- the dome will be used for accurate estimation of aiming angle for an antenna, a telescope, aiming device or similar in a simple, accurate and appropriate way. This is not known from prior publications.
- a radar antenna system comprising a wheel, cone or frustum having an axis.
- the wheel, cone or frustum has a circumferential portion adapted to engage at least one path disposed on a platform for revolving the radar array about the platform.
- a radar array is mounted on the wheel, cone or frustum, with the axis normal to a face of the radar array.
- the wheel, cone or frustum rotates about the platform as the radar array revolves around the platform during operation.
- Gray code disk to a shaft for the antenna, which Gray code disk is used to control the antenna.
- the main object of the invention is to provide a method and a system for highly accurate determination of position of aiming direction of an antenna, a telescope, aiming device or similar arranged on a movable platform in a dome or in a part of a dome, and hence accurate control of the antenna, telescope, aiming device or similar in relation to a desired target or orbit, which solves the disadvantages of prior art as mentioned above.
- a system according to the invention is stated in claim 9.
- Advantageous features of the system are stated in claims 9-24.
- Mounting antennas, telescope, aiming devices or similar in a dome or a part of a dome provides new possibilities of estimating aiming angle of an antenna, a telescope, aiming device or similar in a simple, accurate and suitable manner.
- the idea of the invention is based on arranging or providing a known raster or pattern inside the dome or a screen arranged in the dome by means of one or more light sources, and use one or more r means for reading the raster/pattern, which results in that it is possible to provide a highly accurate position determination of the aiming direction of an antenna, a telescope, aiming device or similar.
- this highly accurate position can be used to control the antenna, telescope, aiming device or similar in relation to desired target or orbit.
- a system according to the invention for arrangement a controllable antenna, a controllable telescope, aiming device or similar arranged to a movable platform in a dome, or a part of a dome includes at least one of the following:
- one or more light sources arranged for arranging or providing one or more predefined patterns or rasters on an interior surface of the dome or a screen arranged in the dome by means of visible and/or invisible light;
- a raster or pattern control unit arranged to choose between a number of relevant patterns or rasters and being connected to a control unit of the system;
- a light source reference positioning unit arranged for defining a reference point on the screen or the interior surface of the dome, where the exact position of the reference point can be controlled by the raster or pattern control unit;
- at least one recording means arranged to the movable antenna, telescope, aiming device or similar which move together with the latter and being arranged for stereoscopic reading of one or more patterns and/or rasters established at the interior surface of the dome or a screen arranged in the dome;
- an image analyzer having different filters arranged to transform the signals from the recording means to digital signatures and parameterized presentations of the image content from each individual recoding means;
- a raster or pattern recognition unit arranged for signal processing information from each individual recoding means and transfer the particular information to the control unit of the system for further processing;
- a positioning control unit arranged to control the position of the antenna, telescope, aiming device or similar in azimuth and elevation via the movable platform by means of suitable motors and actuators;
- control unit arranged to:
- aiming angle position for the antenna, telescope, aiming device or similar, based on data from one or more of the following: the raster or pattern recognition unit, position sensors and external data related to orbit parameters, and control signals, typically AGC, from a receiver system connected to the antenna, telescope or similar, or other data sources having information for control of aiming angle position, typically GPS, Glonass or Galileo data;
- - a user interface arranged to serve as an operator panel and being arranged to present data and submit input data to the system.
- a raster or pattern which is provided or arranged by the light source on the inside of a dome or a screen arranged in the dome can be provided:
- the raster/pattern can preferably be optimized to simplify the analysis of the field of view of the recoding mean(s).
- said recoding mean(s) and light source(s) is/are arranged close to the center of the antenna, telescope, aiming device or similar, so that the light source(s) and recording mean(s) has/have substantially the same position.
- the light source and recording means can be separate units or an integral unit.
- the pattern/raster is generated in a manner so that the field of view from the recording means toward the interior surface of the dome or a screen arranged in the dome, represents a unique pattern/raster at all times. If the positioning of antenna, telescope, aiming device or similar in relation to the dome is combined with less accurate angle measurements, the need for a unique pattern/raster is less and the patterns/rasters can be repeated.
- the accurate position and orientation of the recording means and with that the antenna, telescope, aiming device or similar can be established. This is due to that the accurate direction which the recording means is aiming at in relation to the dome has been established in a unique manner, and that the rotation about the axis of the aiming direction can be established in a unique manner.
- the part of the dome which is located outside the line of sight can be used by introducing a fixed offset for azimuth and elevation in calculation of correct aiming angle.
- a method according to the invention can be summarized by the following steps:
- step d) Calculating the accurate position orientation of the recording means and also for the antenna, telescope, aiming device or similar, and in this way provide highly accurate position determination of aiming direction of the antenna, telescope, aiming device or similar, e) Using position determination of aiming direction from step d) to control the antenna, telescope, aiming device or similar in relation to desired target, orbit or polarization angle.
- Figure 1 is a principle drawing of an antenna arranged in a dome
- Figure 2 is a schematic principle drawing of a system according to the invention
- Figures 3a-d illustrate different rasters or patterns which can be arranged or provided at the interior surface of the dome or a screen arranged in the dome, and
- Figure 4 is a principle drawing of a system according to the invention arranged to an antenna in a dome.
- Figure 1 is a principle drawing of an antenna 11 arranged in a dome 12, said antenna 11 being arranged to a movable platform 13 to control of this in azimuth and elevation.
- Aiming direction 14 of an antenna is determined by position in azimuth and elevation, respectively, (P(azimuth, elevation)).
- the antenna 11 is usually arranged to be rotated 360 degrees inside the dome 12.
- the main function of the dome 12 is to protect the antenna 11 against weather and wind.
- Figure 2 is a schematic principle drawing of a system according to the invention for arrangement in a dome 12 and where an antenna 11 is arranged on a movable platform 13 to be moved in azimuth and elevation.
- the figure also illustrates the flow of signals and data in the system.
- a system includes one or more light sources in the form of e.g. a projector 21 being arranged to provide one or more predefined rasters or patterns 40 (see Figures 3a-d) at a screen (not illustrated) arranged in the dome 12, or on an interior surface 15 ( Figures 1 and 4) of the dome 12.
- the system includes a raster or pattern control unit 22 which is arranged to select between a number of relevant rasters or patterns 40 and being connected to a control unit 33 of the system.
- the light source can be arranged to provide the raster or pattern 40 by means of visible and/or invisible light.
- the system does also include a light source reference position unit 23 which is able to define a reference point 24 at the screen arranged in the dome 12 or the interior surface 15 of the dome 12, where the exact position of the reference point 24 can be controlled by the raster or pattern control unit 22.
- a light source reference position unit 23 which is able to define a reference point 24 at the screen arranged in the dome 12 or the interior surface 15 of the dome 12, where the exact position of the reference point 24 can be controlled by the raster or pattern control unit 22.
- the system includes one or more recording means 25a-c, in the example a camera, which is/are arranged to the movable antenna 11 and which is/are moving together with this and providing possibility of stereoscopic reading of one or more rasters and/or patterns 40 provided at the screen or the interior surface 15 of the dome 12. As illustrated in Figure 2, the camera(s) 25a-c will then follow the movements of the antenna 11 and hence the movements of the movable platform 13.
- recording means 25a-c in the example a camera, which is/are arranged to the movable antenna 11 and which is/are moving together with this and providing possibility of stereoscopic reading of one or more rasters and/or patterns 40 provided at the screen or the interior surface 15 of the dome 12.
- the camera(s) 25a-c will then follow the movements of the antenna 11 and hence the movements of the movable platform 13.
- the recording mean(s) 25a-c and light source(s) 21 is/are arranged close to the center of the antenna 11, so that the light source(s) 21 and recording mean(s) 25a-c have substantially the same position, but this is not a requirement.
- the system includes an image analyzer 26 provided with different filters arranged to transform camera signals to digital signatures and parameterized presentations of the image content from each individual camera 25a-c.
- the system also includes a raster or pattern recognition unit 27 which is arranged to process the signal information from each individual camera 25a-c and transfer the relevant information to the system control unit 33 for further processing.
- the system includes a position control unit 28 arranged to control the antenna 11 position in azimuth and elevation by controlling the movable platform 13 through suitable motors and/or actuators, e.g. by means of a motor 29a for controlling azimuth and a motor 29b for controlling elevation.
- the position control unit 28 is preferably also provided with input about the self-motion of the system, e.g. from a MRU 30, a DP system and/or a VMM unit 31 if the antenna 11 is arranged to a vehicle or vessel in movement.
- the system also includes position control sensors 32a-b, e.g. a sensor for azimuth and a sensor for elevation, which are arranged to measure the position of the antenna 11 in azimuth and elevation, and which can provide control signals back to the position control unit 28 and the system control unit 33.
- position control sensors 32a-b e.g. a sensor for azimuth and a sensor for elevation, which are arranged to measure the position of the antenna 11 in azimuth and elevation, and which can provide control signals back to the position control unit 28 and the system control unit 33.
- Many motors are provided with sensors like this, so that data can be acquired without the use of additional sensors as described above.
- the system control unit 33 is provided with means and/or software for:
- control unit 33 is preferably provided with means and/or software for raster or pattern control, preprogramming of position and/or orbit or target, including control of the system units.
- the system also includes a user interface 37 arranged to serve as an operator panel and being arranged to present data and provide input data to the system.
- the operator panel includes e.g. keyboard, mouse, joystick etc. to operate the system.
- the user interface 37 can for example also be a touch sensitive screen, so that the operator panel is included in the user interface.
- the system can also be provided with communication means (not illustrated) to communicate with external units for remote control, so that it is not necessary to be physically present by the antenna to perform adjustments and data/information can be transmitted to the external unit in a simple manner.
- Figures 3a-d show examples of a few of many different patterns or rasters 40 which can be provided at the internal surface 14 of a dome 12 or at a screen arranged in a dome 12.
- a raster or pattern 40 which is projected by the projector 21 can be formed either by horizontal 41 or vertical lines 42.
- the raster or pattern 40 can be formed by both horizontal 41 and vertical lines 42, e.g. forming a grid where the lines can be continuous or dotted, exhibit different line width or themselves forming a raster or pattern suitable for optical recognition. Examples can be bar codes, as shown in Figure 3b, characters or numbers, as shown in Figure 3c, figures or symbols, as shown in Figure 3d or similar graphical codes.
- the raster/pattern 40 can be formed by using visible and/or invisible light. When using visible light, different colors of the pattern/raster 40 can also be used.
- the pattern/raster 40 can be established as a continuous pattern over the entire interior surface 15 of the dome 12/screen, or in sections or sectors having unique patterns/rasters (e.g. by using different colors).
- the pattern/raster 40 can also be optimized to simplify the analysis of a field of view 43 of the camera(s) 25a-d.
- Figure 4 illustrates the system according to the invention arranged to an antenna 11 arranged in a dome 12, where the system is divided in two units, a unit 38 to be arranged to the antenna 11/the movable platform 13 and a unit 39 arranged inside the dome 12 or outside the dome 12 (illustrated by dotted lines).
- the unit 38 (illustrated by dotted lines in Figure 2) includes for example the units 21-26, 29a-b and 32a-b and the unit 39 (illustrated by dotted lines in Figure 2) includes for example the units 27, 28, 30, 31 and 33-37. This is only one out of many different ways to arrange the system to an antenna 11, telescope, aiming device or similar.
- the raster/pattern 40 is preferably generated in such a way that each field of view 43 of a camera toward the interior surface 15 of the dome 12 or a screen at all times represents an unique pattern/raster 40. If the positioning of the antenna in relation to the dome 12 is combined with less accurate angle measurements, the need for a unique pattern/raster is less and the patterns/rasters can be repeated. For example information about angular measurements, such as azimuth and elevation, can be provided from the sensor means 32a-b.
- the accurate position and orientation of the camera(s) 25a-b can be found, and in this way also the position of the antenna 11 can be established.
- the rotation about the axis of the aiming direction can for example be found by analyzing horizontal lines 41 in the pattern/raster 40 and/or by using a suitable sensor in connection with the movable platform 13 for rotation of the antenna 11, and is used for controlling the polarization angle of the antenna.
- a method according to the invention can be summarized by the following steps:
- step e) Utilizing the determined position of the aiming direction from step d) to control the antenna, telescope, aiming device or similar in relation to desired target, orbit or polarization angle.
- step a) includes defining a reference point at the screen or the interior surface of the dome.
- Step b) includes recording the pattern or raster located within a field of view of the recording means. This also includes patterns or rasters which can be arranged to the interior surface of the dome or screen in advance.
- Step b) includes collection of information from external data sources, such as orbit parameters and/or orbit patterns, control signals from a receiver system, e.g. AGC, and from GPS, Glonass or Galileo data. Step b) also includes collection of information from position control sensors or directly from motors or actuators for control of the movable platform for information about elevation and azimuth.
- external data sources such as orbit parameters and/or orbit patterns
- control signals from a receiver system, e.g. AGC, and from GPS, Glonass or Galileo data.
- Step b) also includes collection of information from position control sensors or directly from motors or actuators for control of the movable platform for information about elevation and azimuth.
- Information/data from external sources are used to calculate correct position for aiming angle of the antenna in azimuth and elevation.
- the actual position is calculated by means of the grid of the dome.
- the difference between actual position and calculated position are used for control of motor operation, i.e. the motors 29a-b for aiming direction in azimuth and elevation until the deviation is minimal and within a desired tolerance.
- Step d) includes calculation of accurate position of aiming direction based on information from step b) and step c).
- Accurate positioning in relation to aiming angle in azimuth and elevation is achieved by means of optical reading of marked position in the pattern or raster, and by processing of the image information.
- the actual position for line of sight is depicted at the inside of the dome by means of a laser.
- the laser point will thus be at a location in the pattern or raster inside the dome or at the screen, and the actual position can be read as the position of the laser point referred to the pattern or raster.
- the pattern or raster can be made as long as the interior periphery of the dome, and the laser point in practice will have a very small size, the accuracy of the reading will be extremely high.
- the accuracy in the principle will be in the same order as the dispersion of the laser point at the inside of the dome.
- the method includes optimization of the arranged or provided pattern or raster for simplified analysis.
- the accuracy of the method is dependent of the length, height, and line and possibly symbol distance of the dome pattern.
- Said pattern or raster can also be arranged to the dome in advance, e.g. by painting it onto the interior surface of the dome or to the screen. It may also be an alternative to have a painted basic pattern/raster and apply new patterns on top by means of the light source(s).
- a pattern or raster does not need to be painted on the interior surface of the dome or screen, but the screen or dome can for example be provided with fixed light sources, e.g. LED lamps, which provide light spots that define a raster or pattern, e.g. a grid. This illustrates that there are many ways of providing the pattern or raster at the screen or dome.
- fixed light sources e.g. LED lamps, which provide light spots that define a raster or pattern, e.g. a grid.
- the light source(s) and recording means can be a combined unit which handles both.
- Numerous light sources can be used, such as lasers, projectors and other that are controllable to emit different patterns/rasters.
- the light source can also be provided with different filters or different optical devices to diffract a light beam to a desired pattern.
- the provided pattern/raster can be used for calibration of other sensors related to an arrangement of an antenna, telescope, aiming device or similar arranged in a dome or a part of a dome, such as MRU, Gyro etc.
Landscapes
- Variable-Direction Aerials And Aerial Arrays (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/392,236 US20130057651A1 (en) | 2010-05-28 | 2011-05-27 | Method and system for positioning of an antenna, telescope, aiming device or similar mounted onto a movable platform |
BR112012006145-3A BR112012006145A2 (en) | 2010-05-28 | 2011-05-27 | METHOD AND SYSTEM FOR POSITIONING AN ANTENNA, TELESCOPE, AND POINTING MECHANISM ON A MOBILE PLATFORM. |
EP11798426.0A EP2577795A4 (en) | 2010-05-28 | 2011-05-27 | Method and system for positioning of an antenna, telescope, aiming device or similar mounted onto a movable platform |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NO20100779 | 2010-05-28 | ||
NO20100779A NO332068B1 (en) | 2010-05-28 | 2010-05-28 | Method and system for positioning antenna, telescope, sighting device or the like mounted on a moving platform |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2011162614A1 true WO2011162614A1 (en) | 2011-12-29 |
Family
ID=45371621
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/NO2011/000160 WO2011162614A1 (en) | 2010-05-28 | 2011-05-27 | Method and system for positioning of an antenna, telescope, aiming device or similar mounted onto a movable platform |
Country Status (5)
Country | Link |
---|---|
US (1) | US20130057651A1 (en) |
EP (1) | EP2577795A4 (en) |
BR (1) | BR112012006145A2 (en) |
NO (1) | NO332068B1 (en) |
WO (1) | WO2011162614A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE2030282A1 (en) * | 2020-09-09 | 2021-08-17 | Ntrakker Ab | Mounting arrangement for an antenna and an antenna arrangement |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NO342689B1 (en) * | 2016-05-30 | 2018-07-09 | Advanced Hydrocarbon Mapping As | Apparatus for orienting an electromagnetic field sensor, and related receiver unit and method |
US10455435B2 (en) * | 2016-09-08 | 2019-10-22 | Commscope Technologies Llc | Mobile site platform with descending capability |
US10862189B1 (en) * | 2016-11-10 | 2020-12-08 | United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration | Near earth and deep space communications system |
CN107643770A (en) * | 2017-09-15 | 2018-01-30 | 中国科学院长春光学精密机械与物理研究所 | A kind of telescope control system and method |
US11618594B2 (en) * | 2019-02-07 | 2023-04-04 | The Government Of The United States Of America As Represented By The Secretary Of The Air Force | System and method for daylight imaging of high altitude objects |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4920350A (en) * | 1984-02-17 | 1990-04-24 | Comsat Telesystems, Inc. | Satellite tracking antenna system |
EP0664499A1 (en) * | 1994-01-24 | 1995-07-26 | Hughes Aircraft Company | Gimbal control system |
US5922039A (en) * | 1996-09-19 | 1999-07-13 | Astral, Inc. | Actively stabilized platform system |
US6366253B1 (en) * | 2000-09-22 | 2002-04-02 | Hemmingsen, Ii Robert J. | Satellite antenna alignment device |
EP1353404A2 (en) * | 2002-04-10 | 2003-10-15 | Lockheed Martin Corporation | Radar system with a rotating antenna system |
US20030197655A1 (en) * | 2002-04-22 | 2003-10-23 | Mitsubishi Denki Kabushiki Kaisha | Parallel displacement/inclination measuring apparatus and antenna system |
US20040007664A1 (en) * | 2002-07-08 | 2004-01-15 | Microe Systems, Inc. | Multi-track optical encoder employing beam divider |
WO2006065892A2 (en) * | 2004-12-13 | 2006-06-22 | Optical Alchemy, Inc. | Multiple axis gimbal employing nested spherical shells |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2551920B1 (en) * | 1983-09-14 | 1985-12-06 | Gall Jean Claude Le | ANTENNA STABILIZATION AND POINTING DEVICE, ESPECIALLY ON SHIP |
US5973309A (en) * | 1997-08-27 | 1999-10-26 | Trw Inc. | Target-tracking laser designation |
JP2916142B1 (en) * | 1998-08-10 | 1999-07-05 | 洋夫 岩田 | All-round spherical screen projector |
EP1819014A1 (en) * | 2001-09-28 | 2007-08-15 | Sumitomo Electric Industries, Ltd. | Radio wave lens antenna device |
US7194630B2 (en) * | 2002-02-27 | 2007-03-20 | Canon Kabushiki Kaisha | Information processing apparatus, information processing system, information processing method, storage medium and program |
JP3983573B2 (en) * | 2002-03-06 | 2007-09-26 | 富士重工業株式会社 | Stereo image characteristic inspection system |
US8275883B2 (en) * | 2002-10-08 | 2012-09-25 | My Telescope.Com | Systems and methods for accessing telescopes |
US7339731B2 (en) * | 2005-04-20 | 2008-03-04 | Meade Instruments Corporation | Self-aligning telescope |
US7614805B2 (en) * | 2006-11-07 | 2009-11-10 | Joseph Showalter | Image capture device mounting assembly for firearm |
WO2009100437A1 (en) * | 2008-02-10 | 2009-08-13 | Hemisphere Gps Llc | Antenna alignment and monitoring system and method using gnss |
US8894216B2 (en) * | 2009-12-28 | 2014-11-25 | Disney Enterprises, Inc. | Active mask projector providing diffracted light with animation and non-random patterns |
US20110167708A1 (en) * | 2010-01-12 | 2011-07-14 | Carson Cheng | Rubber Armored Rifle Scope with Integrated External Laser Sight |
-
2010
- 2010-05-28 NO NO20100779A patent/NO332068B1/en unknown
-
2011
- 2011-05-27 US US13/392,236 patent/US20130057651A1/en not_active Abandoned
- 2011-05-27 WO PCT/NO2011/000160 patent/WO2011162614A1/en active Application Filing
- 2011-05-27 BR BR112012006145-3A patent/BR112012006145A2/en not_active Application Discontinuation
- 2011-05-27 EP EP11798426.0A patent/EP2577795A4/en not_active Withdrawn
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4920350A (en) * | 1984-02-17 | 1990-04-24 | Comsat Telesystems, Inc. | Satellite tracking antenna system |
EP0664499A1 (en) * | 1994-01-24 | 1995-07-26 | Hughes Aircraft Company | Gimbal control system |
US5922039A (en) * | 1996-09-19 | 1999-07-13 | Astral, Inc. | Actively stabilized platform system |
US6366253B1 (en) * | 2000-09-22 | 2002-04-02 | Hemmingsen, Ii Robert J. | Satellite antenna alignment device |
EP1353404A2 (en) * | 2002-04-10 | 2003-10-15 | Lockheed Martin Corporation | Radar system with a rotating antenna system |
US20030197655A1 (en) * | 2002-04-22 | 2003-10-23 | Mitsubishi Denki Kabushiki Kaisha | Parallel displacement/inclination measuring apparatus and antenna system |
US20040007664A1 (en) * | 2002-07-08 | 2004-01-15 | Microe Systems, Inc. | Multi-track optical encoder employing beam divider |
WO2006065892A2 (en) * | 2004-12-13 | 2006-06-22 | Optical Alchemy, Inc. | Multiple axis gimbal employing nested spherical shells |
Non-Patent Citations (1)
Title |
---|
See also references of EP2577795A4 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE2030282A1 (en) * | 2020-09-09 | 2021-08-17 | Ntrakker Ab | Mounting arrangement for an antenna and an antenna arrangement |
SE543869C2 (en) * | 2020-09-09 | 2021-08-17 | Ntrakker Ab | Mounting arrangement for an antenna and an antenna arrangement |
Also Published As
Publication number | Publication date |
---|---|
BR112012006145A2 (en) | 2020-06-23 |
EP2577795A1 (en) | 2013-04-10 |
EP2577795A4 (en) | 2013-10-23 |
NO20100779A1 (en) | 2011-11-29 |
US20130057651A1 (en) | 2013-03-07 |
NO332068B1 (en) | 2012-06-18 |
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