WO2017026956A2 - Dispositif d'arpentage d'artillerie - Google Patents

Dispositif d'arpentage d'artillerie Download PDF

Info

Publication number
WO2017026956A2
WO2017026956A2 PCT/TR2016/000116 TR2016000116W WO2017026956A2 WO 2017026956 A2 WO2017026956 A2 WO 2017026956A2 TR 2016000116 W TR2016000116 W TR 2016000116W WO 2017026956 A2 WO2017026956 A2 WO 2017026956A2
Authority
WO
WIPO (PCT)
Prior art keywords
surveying device
enables
surveying
location
base
Prior art date
Application number
PCT/TR2016/000116
Other languages
English (en)
Other versions
WO2017026956A3 (fr
Inventor
Levent GUNER
Mustafa Ozgur ATESOGLU
Alper Demir
Onur GUNER
Murat Eren
Alper Ozturk
Original Assignee
Aselsan Elektronik Sanayi Ve Ticaret Anonim Sirketi
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 Aselsan Elektronik Sanayi Ve Ticaret Anonim Sirketi filed Critical Aselsan Elektronik Sanayi Ve Ticaret Anonim Sirketi
Publication of WO2017026956A2 publication Critical patent/WO2017026956A2/fr
Publication of WO2017026956A3 publication Critical patent/WO2017026956A3/fr

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C15/00—Surveying instruments or accessories not provided for in groups G01C1/00 - G01C13/00
    • G01C15/002—Active optical surveying means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/02—Aiming or laying means using an independent line of sight
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/06—Aiming or laying means with rangefinder
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H11/00—Defence installations; Defence devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H7/00—Armoured or armed vehicles
    • F41H7/005—Unmanned ground vehicles, i.e. robotic, remote controlled or autonomous, mobile platforms carrying equipment for performing a military or police role, e.g. weapon systems or reconnaissance sensors
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C3/00—Measuring distances in line of sight; Optical rangefinders
    • G01C3/02—Details
    • G01C3/06—Use of electric means to obtain final indication
    • G01C3/08—Use of electric radiation detectors

Definitions

  • the present invention relates to a novel artillery surveying device which performs the duties of creating a common coordinate system in the battlefield, determining the points which provide very precise location information, determining the necessary location and direction angles for the sensors and systems, determining the location and direction angles of the weapons system or specialized mission tools, and directing them.
  • Surveying systems are used for generating lines that are making known angles with the points in the field with known locations, and with the north.
  • the surveying systems can be studied in three groups which are the classical surveying systems (theodolites), gyroscopic systems having pendulums, and inertial navigation systems.
  • the technique that is in the classical systems is based on the basis of moving a known coordinate and direction angle of a known point, in the field, by traversing.
  • the information of the location and direction angle needs to be transferred until a desired area, with the measurements of angle and distance from the known point.
  • the angle and distance measurement devices (theodolite, total station etc.) need to be set up on a tripod, need to be made parallel to the ground, the measurement need to be taken and all these processes need to be repeated in the next measurement point.
  • this method takes too much time, and only 2 kilometers of advancement can be achieved in an hour [1].
  • the gyro-theodolite systems having a pendulum, which are set up on tripods work in the following principle: in the event that the location information is supplied to the system at the point where the measurement is going to be made, if the system is set up on a tripod and brought to be parallel to the ground using a bubble level, the angle of the line that is being looked at with the north can be found. In order to get the systems parallel to the ground at every measurement point, it is needed to wait approximately five minutes, and for the measurement for locating the north, it is needed to wait approximately between four to ten minutes. As these systems are dependent to GPS for the location information, they cannot perform measurements once the GPS is jammed.
  • the fire support means which do not have location/direction finding systems on themselves have to wait for the old fashioned surveying unit to make measurements lasting hours with theodolites for finding a location and direction reference for the new position in order to relocate from one position to another. This, in turn, increases the possibility of the units to be located.
  • the object of the invention is to develop an artillery surveying device which enables creating a common coordinate system in the battlefield, determining the points which provide very precise location information, determining the necessary location and direction angles for the sensors and systems, determining the location and direction angles of the weapons system or specialized mission tools, and directing them.
  • the most important privilege that renders the artillery surveying device from other surveying systems is that it is an authentic design which brings the superior features of the static north finder gyroscope-theodolite systems and dynamic direction finder gyroscopic systems.
  • the features of the system which render it different from other surveying systems are that it can perform surveying very fast by the virtue of the inertial navigation system, it can perform its duty in an operational state on a tripod, a backpack or a vehicle, it can carry out its duties in a short time and its high precision of finding location/direction.
  • the system can be carried and used by a single person as well as it can be integrated to various vehicles. By this way it has the ability to perform its duties in different conditions.
  • the artillery surveying device can operate without needing extra time for finding the north. It takes less than a minute of time for the system to become ready to measure. The measurements can be made by aiming to the target and pushing a single button.
  • the artillery surveying device can operate without the need of being brought parallel to the ground on a tripod.
  • the time for setting up and packing up the system is close to none.
  • the leveling time can be as much as 5 minutes. In the subject of artillery fire, where time is of vital importance, this time is very important for the survival of the personnel.
  • the need for rotation measurement devices such as encoders and the like is eliminated by measuring the angles that are made by the ground plane via the inertial navigation system.
  • the rotation axes in the surveying device do not need to be perpendicular to each other; the need for producing precision parts, and the need for calibration are eliminated.
  • the movements in the structure (tripod, platform etc.) to which the device is connected such as stretching and/or torsion do not affect the precision of measurement.
  • the system as opposed to the classical methods, does not have to advance carrying the information of the known point.
  • the current location of the system and the direction angle of place it is facing is its reference.
  • Figure 1 Front perspective view of the surveying device.
  • Figure 3 Side perspective view of the surveying device.
  • the surveying device (1) which enables creating a common coordinate system in the battlefield, determining the points which provide very precise location information, determining the necessary location and direction angles for the sensors and systems, determining the location and direction angles of the weapons system or specialized mission tools, and directing them essentially comprises; at least one sensitive plate (2),
  • At least one optical system (7) which enables aiming to the target
  • At least one distance meter (9) which enables measuring of the distance to the target
  • At least one GPS antenna 10 which enables the signals that are sent by the GPS satellites to be received
  • At least one inertial navigation system (11) which enables the calculation of the location, direction angle and the angle with respect to the earth plane, at least one control unit (12) that is adapted to run the surveying algorithms using the information coming from the distance meter (9) and the inertial navigation system (11).
  • the sensitive plate (2) of the device is connected to the two arms (4) which are present in the sides of the base (3), and which extend in vertical direction.
  • the movement of the surveying device (1) in the vertical direction is achieved by rotationally moving around an imaginary axis that is connecting the points where the arms (4) and the sensitive plate (2) are connected.
  • the movement of the surveying device (1) in the horizontal direction is achieved by rotationally moving around the axis of the shaft.
  • the fine tuning mechanism (8) that is present on the base (3) and the side arms (4) is used.
  • connection interface detail (6) and shaft (14) are present in the bottom surface of the base (3), to which the arms (4) are attached.
  • the said connection interface detail (6) and shaft (14) are used for mounting the base (3) of the surveying device (1) to the mounting interface (15).
  • the mounting interface (15) in turn, enables the surveying device (1) to be placed on various platforms and/or vehicles.
  • an optical system (7) is present on the sensitive plate (2).
  • the distance between the aimed target and the surveying device (1) is measured via a distance meter (9).
  • the said distance meter (9) is a laser distance meter (9) which has a precision of lm (meter) and a range of 20km (kilometers).
  • the distance meter (9) is an electronic distance meter which has a precision of 1cm (centimeter) and a range of 5km (kilometers).
  • the location (coordinates) of where the surveying device (1) is, its direction angle and its angles with respect to the earth plane are very precisely calculated.
  • the information coming from the inertial navigation system (1 1) and distance meter (9) they are processed by the control unit (12), and the coordinates of the targeted point and the direction angle of the line that is being looked at can be calculated.
  • the said control unit (12) can be embedded to the surveying device in one embodiment of the invention. In another embodiment of the invention, the control unit (12) can be used separately from the surveying device, in a portable manner.
  • the electrical energy that is needed for the control unit (12), inertial navigation system (1 1) and the distance meter (9) that are used in the surveying device (1) to operate, is supplied by a power supply (13).
  • the said power supply (13) can be a battery block that can be recharged by being connected to a mains supply, in one embodiment of the invention. The working principle of the invention is explained in detail below.
  • a target is aimed at by the user, preferably via the optical system (7) that is located on the top part of the sensitive plate (2).
  • the fine tuning mechanism (8) that is present on the base (3) and the side arms (4) is used.
  • the calculated coordinates and the direction angle of the line that is being looked at are transmitted to the weapons systems or to the specialized mission tools, and thus directing of these tools to the target can be achieved.
  • the inertial navigation system (11), optical system (7) and the distance meter (9) are unified on top of the sensitive plate (2) and they are enabled to work in an integrated manner, and by this virtue, the need for using theodolites in the classical surveying systems, and thus the need for bringing the theodolites parallel to the ground is eliminated. By this virtue, the measurement speed is improved significantly. By this, the time for completing the measurements at the point (getting off the vehicle, opening the rear doors, setting up on the tripod, aiming at the target point, making the measurement by pushing a single button), at which the measurements are to be made, can be less than two minutes.
  • the GPS unit of the surveying device When the GPS unit of the surveying device is jammed by an external interference, it can continue carrying out its duties by stopping for a minute every one hour, by the virtue of the "odometer" support which gives information about with which speed and how far it is being travelled.
  • the inventive surveying device (1) also comprises the features of a conventional navigation device.
  • the control unit (12) that is present on the surveying device (1), by using the maps that are loaded in its memory route planning can be made during navigation, and information such as the direction to go, route information, estimated time of arrival and remaining distance can be shown to the driver of the vehicle, on the control unit (12).

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Electromagnetism (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Navigation (AREA)

Abstract

La présente invention concerne un nouveau dispositif d'arpentage d'artillerie qui effectue les tâches suivantes : création d'un système de coordonnées commun sur le champ de bataille, détermination des points qui fournissent des informations de localisation très précise, détermination de l'emplacement et des angles de direction nécessaires pour les capteurs et les systèmes, détermination de l'emplacement et des angles de direction du système d'armes ou des outils de mission spécialisés, comprenant essentiellement : une plaque sensible (2), une base (3), deux bras (4) qui sont présents au niveau des côtés de la base (3), qui s'étendent dans la direction verticale, et auxquels la plaque sensible (2) est raccordée, une poignée (5) présente sur chaque bras (4), un élément particulier d'interface de connexion (6) et une tige (14) qui sont utilisés pour monter la base (3) du dispositif d'arpentage (1) sur une interface de montage (15), une interface de montage (15) qui permet au dispositif d'arpentage (1) d'être placé sur divers plates-formes et/ou véhicules, un système optique (7) qui permet de viser la cible, un dispositif de mesure de distance (9) qui permet de mesurer la distance par rapport à la cible, une antenne GPS (10) qui permet la réception des signaux envoyés par les satellites GPS, un système de navigation inertielle (11) qui permet le calcul de l'emplacement, de l'angle de direction et de l'angle par rapport au plan de la terre, une unité de commande (12) qui est conçue pour exécuter les algorithmes d'arpentage à l'aide des informations provenant du dispositif de mesure de distance (9) et du système de navigation inertielle (11).
PCT/TR2016/000116 2015-08-13 2016-08-12 Dispositif d'arpentage d'artillerie WO2017026956A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
TR201510016 2015-08-13
TR2015/10016 2015-08-13

Publications (2)

Publication Number Publication Date
WO2017026956A2 true WO2017026956A2 (fr) 2017-02-16
WO2017026956A3 WO2017026956A3 (fr) 2017-04-20

Family

ID=57796957

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/TR2016/000116 WO2017026956A2 (fr) 2015-08-13 2016-08-12 Dispositif d'arpentage d'artillerie

Country Status (1)

Country Link
WO (1) WO2017026956A2 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2849625A1 (es) * 2020-02-19 2021-08-19 Aselsan Elektronik Sanayi Ve Ticaret Anonim Sirketi Sistema de apoyo al despegue, navegacion y aterrizaje de vehiculos aereos no tripulados
CN117405101A (zh) * 2023-09-11 2024-01-16 北京国卫星通科技有限公司 惯导数据采集与分析系统

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9810405D0 (en) * 1998-05-15 1998-07-15 Measurement Devices Ltd Survey apparatus
US20070127008A1 (en) * 2005-11-08 2007-06-07 Honeywell International Inc. Passive-optical locator
US20120059575A1 (en) * 2010-02-05 2012-03-08 Honeywell International Inc. Target locator device and methods

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2849625A1 (es) * 2020-02-19 2021-08-19 Aselsan Elektronik Sanayi Ve Ticaret Anonim Sirketi Sistema de apoyo al despegue, navegacion y aterrizaje de vehiculos aereos no tripulados
CN117405101A (zh) * 2023-09-11 2024-01-16 北京国卫星通科技有限公司 惯导数据采集与分析系统

Also Published As

Publication number Publication date
WO2017026956A3 (fr) 2017-04-20

Similar Documents

Publication Publication Date Title
US11035660B2 (en) Inertial dimensional metrology
ES2826887T3 (es) Método de determinación de la actitud de vehículos con GNSS-INS basándose en una única antena
US8826550B2 (en) Geographically north-referenced azimuth determination
US20210123735A1 (en) Online leveling calibration of a geodetic instrument
US9753135B2 (en) Hand-held distance-measuring device having an angle-determining unit
US7541974B2 (en) Managed traverse system and method to acquire accurate survey data in absence of precise GPS data
US10309786B2 (en) Navigational and location determination system
ES2909510T3 (es) Aparato de posicionamiento
US20120059575A1 (en) Target locator device and methods
US20050197755A1 (en) Multi-source positioning system for work machines
US11199631B2 (en) Apparatus and methods for geo-locating one or more objects
WO2012121819A1 (fr) Système de navigation par inertie et son procédé d'initialisation/de correction
GB2516066A (en) Portable device for determining azimuth
CN106092094A (zh) 基于gnss/ins/激光测距组合定位的手持接收机及测量方法
CN103759743B (zh) 惯性测量装置方位基准传递装置及大倾角时方位确定方法
US20140249750A1 (en) Navigational and location determination system
WO2018176092A1 (fr) Système de navigation inertielle à faible coût
JP2008015531A (ja) 三次元地形マッピング
WO2017026956A2 (fr) Dispositif d'arpentage d'artillerie
US20210223042A1 (en) Geodetic instrument with a static base
US10006770B2 (en) Remote location determination system
JP2020197521A (ja) 角度測定デバイスの基準方向を判定する方法およびデバイス
RU2469271C1 (ru) Универсальная система топопривязки и навигации
CN105841700B (zh) 一种面向不动产实地测量的定位方法
US20240125597A1 (en) In-the-field leveling calibration of a surveying instrument

Legal Events

Date Code Title Description
NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 16826204

Country of ref document: EP

Kind code of ref document: A2