CN111924094A - Aerial wide-area geological survey system of high prototype unmanned aerial vehicle - Google Patents
Aerial wide-area geological survey system of high prototype unmanned aerial vehicle Download PDFInfo
- Publication number
- CN111924094A CN111924094A CN202010518122.5A CN202010518122A CN111924094A CN 111924094 A CN111924094 A CN 111924094A CN 202010518122 A CN202010518122 A CN 202010518122A CN 111924094 A CN111924094 A CN 111924094A
- Authority
- CN
- China
- Prior art keywords
- flight
- survey
- aerial vehicle
- unmanned aerial
- task
- 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.)
- Pending
Links
- 238000005259 measurement Methods 0.000 claims abstract description 22
- 238000007405 data analysis Methods 0.000 claims abstract description 9
- 238000013461 design Methods 0.000 claims abstract description 8
- 238000004891 communication Methods 0.000 claims abstract description 6
- 238000012544 monitoring process Methods 0.000 claims abstract description 6
- 238000007726 management method Methods 0.000 claims abstract description 4
- 238000004364 calculation method Methods 0.000 claims description 5
- 230000035939 shock Effects 0.000 claims description 5
- 238000013016 damping Methods 0.000 claims description 3
- 230000003014 reinforcing effect Effects 0.000 claims description 3
- 230000008878 coupling Effects 0.000 claims description 2
- 238000010168 coupling process Methods 0.000 claims description 2
- 238000005859 coupling reaction Methods 0.000 claims description 2
- 230000003416 augmentation Effects 0.000 abstract description 5
- 238000004458 analytical method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 206010021143 Hypoxia Diseases 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 244000144972 livestock Species 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments
- B64D43/02—Arrangements or adaptations of instruments for indicating aircraft speed or stalling conditions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
- G01D21/00—Measuring or testing not otherwise provided for
- G01D21/02—Measuring two or more variables by means not covered by a single other subclass
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Geophysics And Detection Of Objects (AREA)
Abstract
The invention discloses a highland unmanned aerial vehicle aviation wide-area geological survey system, which comprises a task system, a flight system, a measurement system, a stability augmentation system and a data analysis system, wherein the task system carries out task planning, resource management and task supervision aiming at different survey target areas, issues flight tasks to the flight system, and simultaneously receives survey effectiveness feedback of the measurement system, the flight system consists of an unmanned aerial vehicle, a communication link and a ground control station to complete the flight aerial survey tasks, the measurement system is a core functional component of wide-area geomagnetic survey and comprises a measurement part and a monitoring part, the measurement part and the monitoring part run independently to realize effective data acquisition, and the highland unmanned aerial vehicle aviation wide-area geological survey system is called DWFEMT system for short. The invention has reasonable design; the DWFEMT system uses an unmanned aerial vehicle as an operation carrier, avoids manpower transportation and heavy labor of manual hiking measuring point positioning, and greatly improves the operation efficiency.
Description
Technical Field
The invention relates to a highland unmanned aerial vehicle aviation wide-area geological survey system.
Background
The wide-area electromagnetic geological survey technology has been approved by the industry and verified by practice, the geological structure and the mineral reserve distribution of the depth of several kilometers below the earth surface can be effectively measured, the wide-area method survey needs to arrange sensors and auxiliary equipment on the ground of a given measuring point, the geotechnical structure below the earth surface can be obtained by carrying out inversion analysis on data collected by the sensors, the operation mode of carrying on shoulders limits the operation range of the wide-area survey technology in a plateau environment, the survey team faces heavy transportation burden, the sensors and the auxiliary equipment need to be transported to the measuring point, a human and livestock carrying mode is adopted under the condition of no vehicle communication, generally the measuring points are dense, the carried sensors and the auxiliary equipment need to consume great manpower and time, and in addition, many unmanned areas, high altitude, oxygen deficiency, no replenishment and difficult life guarantee are realized, such a work method cannot be handled.
Disclosure of Invention
The invention aims to provide a highland unmanned aerial vehicle aviation wide-area geological survey system to solve the technical problem.
In order to achieve the purpose, the invention adopts the following technical scheme:
the utility model provides a plateau type unmanned aerial vehicle aviation wide area geological survey system, including task system, flight system, measurement system, increase steady system, data analysis system, task system carries out the task planning to the survey target area of difference, resource management and task supervise, and assign flight task to flight system, receive measurement system's survey validity feedback simultaneously, flight system comprises unmanned aerial vehicle, communication link and ground control station, in order to accomplish the flight aerial survey task, measurement system is wide area geomagnetic survey's core function part, including measuring part and monitoring part, both independent operation, in order to realize effectual data acquisition, stable system is the electromechanical module who connects wide area geomagnetic sensor and unmanned aerial vehicle platform, except that the function of fixed structure, possess the shock attenuation and subtract pendulum function, data analysis system is through original data, sensor attitude information, data analysis system, Comprehensive analysis and calculation of navigational speed information, GPS coordinate information and the like are carried out, and dynamically acquired space magnetic field information is converted into basic data for geological inversion calculation.
Preferably, the mount is installed to unmanned aerial vehicle's in the flight system bottom, and the support is installed to the mount below, and the support is the chevron design, and the cylinder is installed at the top of support, and the cylinder passes through the shaft coupling to be connected with the rotating electrical machines, and the rotating electrical machines passes through the support mounting in the mount below, and the bar magnet is installed to the bottom of support, and the both ends of bar magnet are equipped with the wire, install inertia measurement module on the bar magnet.
Preferably, the fixing frame is in a hollow square design, the reinforcing grid is installed in the middle of the fixing frame, the yaw motor installed on the base is arranged in the middle of the fixing frame, and the damping spring sleeves are installed at four corners of the fixing frame.
Compared with the prior art, the invention has the following advantages: the invention has reasonable design; the DWFEMT system realizes the aviation of a wide area method, takes an unmanned aerial vehicle as an operation carrier, avoids the manpower transportation and the heavy labor of manual on-foot measuring point positioning, and greatly improves the operation efficiency and the operation environment adaptability. Aiming at high altitude, no traffic and an anoxic environment, the DWFEMT system can efficiently realize survey of a survey area; through the stability augmentation system, the survey sensor can keep a stable posture when the unmanned aerial vehicle maneuvers under the influence of airflow, so that the effectiveness of a task is ensured, the possibility of invalid operation is reduced, the effectiveness of measurement is improved, a monitoring part of the measurement system can effectively identify an invalid task area and feed the invalid task area back to the task system, and the task neutral gear is avoided by performing supplementary measurement; unmanned aerial vehicle is along setting the straight motion to the direction of survey line, the bar magnet is with the straight motion of the gesture of horizontal perpendicular to survey line, when receiving the disturbance, though the bar magnet takes place driftage and roll motion for unmanned aerial vehicle, the attitude of bar magnet is surveyed in real time to the inertia measurement module among the stability augmentation system, the driftage through yaw motor additional survey regulation bar magnet immediately, the roll of bar magnet is regulated in the initiative additional survey of rotating electrical machines, make it keep under the gesture perpendicular with the survey line all the time, stability augmentation system passes through the shock attenuation spring sleeve and is connected with unmanned aerial vehicle, the shock attenuation spring has absorbed most high frequency vibration.
Drawings
Fig. 1 is a constitutional diagram of the aerial wide-area geological survey system of the prototype unmanned aerial vehicle.
Fig. 2 is a working schematic diagram of the aerial wide-area geological survey system of the prototype unmanned aerial vehicle. .
Fig. 3 is a working principle diagram of the measuring system of the aerial wide-area geological survey system of the prototype unmanned aerial vehicle.
Fig. 4 is an exploded view of the drone and the mount of the aerial wide-area geological survey system of the prototype drone of the invention.
Fig. 5 is an exploded view of the mounting bracket and the support of the aerial wide-area geological survey system of the prototype unmanned aerial vehicle of the invention.
Fig. 6 is a schematic view of a fixing frame of the aerial wide-area geological survey system of the prototype unmanned aerial vehicle.
Detailed Description
The invention is explained in further detail below with reference to the figures and the specific embodiments.
As shown in figures 1-6, a highland unmanned aerial vehicle aviation wide area geological survey system comprises a task system, a flight system, a measurement system, a stability augmentation system and a data analysis system, wherein the task system carries out task planning, resource management and task supervision aiming at different survey target areas, assigns flight tasks to the flight system and simultaneously receives survey effectiveness feedback of the measurement system, the flight system consists of an unmanned aerial vehicle, a communication link and a ground control station to complete the flight aerial survey tasks, the measurement system is a core functional component of wide area geomagnetic survey and comprises a measurement part and a monitoring part which operate independently to realize effective data acquisition, the stability system is an electromechanical module connecting a wide area geomagnetic sensor and an unmanned aerial vehicle platform, and has the functions of shock absorption and swing reduction besides the function of fixed structure, and the data analysis system carries out the functions of original data, Comprehensive analysis and calculation of sensor attitude information, navigational speed information, GPS coordinate information and the like, dynamically acquired space magnetic field information is converted into basic data for geological inversion calculation, a highland unmanned aerial vehicle aviation wide area geological survey system is called DWFEMT system for short, a fixed frame 2 is installed at the bottom of an unmanned aerial vehicle 1 in a flight system, a support 3 is installed below the fixed frame 2, the support 3 is in a herringbone design, a roller 5 is installed at the top of the support 3, the roller 5 is connected with a rotating motor 6 through a coupler, the rotating motor 6 is installed below the fixed frame 2 through a support, a magnetic rod 7 is installed at the bottom of the support 3, leads 9 are arranged at two ends of the magnetic rod 7, an inertia measurement module 8 is installed on the magnetic rod 7, the fixed frame 2 is in a hollow square design, a reinforcing grid is installed in the middle of the fixed frame 2, a yaw motor 4 installed on a base is arranged, four corners of the fixed frame 2 are provided with damping spring sleeves 10.
The foregoing is a preferred embodiment of the present invention, and it will be apparent to those skilled in the art that variations, modifications, substitutions and alterations can be made in the embodiment without departing from the principles and spirit of the invention.
Claims (3)
1. The utility model provides a plateau type unmanned aerial vehicle aviation wide area geological survey system, including the task system, flight system, measurement system, increase steady system, data analysis system, a serial communication port, task system carries out the task planning to different survey target area, resource management and task supervise, and assign flight task to flight system, receive measurement system's survey validity feedback simultaneously, flight system comprises unmanned aerial vehicle, communication link and ground control station, in order to accomplish flight aerial survey task, measurement system includes measuring part and monitoring part, both independently operate, in order to realize effectual data acquisition, stable system is the electromechanical module who connects wide area geomagnetic sensor and unmanned aerial vehicle platform, except that the fixed function of structure, possess the shock attenuation and subtract pendulum function, data analysis system is through original data, sensor attitude information, speed information, the data analysis system is through to original data, sensor attitude information, speed information, the survey of a flight, And comprehensively analyzing and calculating GPS coordinate information and the like, and converting the dynamically acquired space magnetic field information into basic data for geological inversion calculation.
2. The system of claim 1, wherein a fixing frame is installed at the bottom of the unmanned aerial vehicle in the flight system, a support is installed below the fixing frame, the support is of a herringbone design, a roller is installed at the top of the support, the roller is connected with a rotating motor through a coupling, the rotating motor is installed below the fixing frame through a support, a magnetic rod is installed at the bottom of the support, wires are arranged at two ends of the magnetic rod, and an inertia measurement module is installed on the magnetic rod.
3. The system of claim 2, wherein the mount is a hollow square design, a reinforcing grid is installed in the middle of the mount, a yaw motor is installed in the middle of the mount, and damping spring sleeves are installed at four corners of the mount.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010518122.5A CN111924094A (en) | 2020-06-09 | 2020-06-09 | Aerial wide-area geological survey system of high prototype unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010518122.5A CN111924094A (en) | 2020-06-09 | 2020-06-09 | Aerial wide-area geological survey system of high prototype unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111924094A true CN111924094A (en) | 2020-11-13 |
Family
ID=73316512
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010518122.5A Pending CN111924094A (en) | 2020-06-09 | 2020-06-09 | Aerial wide-area geological survey system of high prototype unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111924094A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102385071A (en) * | 2011-10-25 | 2012-03-21 | 杨镜明 | Aerial survey device and method for geomagnetic field intensity |
| CN103792436A (en) * | 2014-02-21 | 2014-05-14 | 北京森馥科技股份有限公司 | On-line electromagnetic radiation long-term monitoring system |
| CN103941297A (en) * | 2014-04-21 | 2014-07-23 | 中国科学院地质与地球物理研究所 | Aeromagnetic measuring device and method based on fixed-wing unmanned aerial vehicle |
| CN104535941A (en) * | 2014-12-04 | 2015-04-22 | 上海卫星装备研究所 | Satellite magnetic test external interference magnetic field closed-loop control method under geomagnetic environment |
| CA2833380A1 (en) * | 2013-11-12 | 2015-05-12 | Marius Moszczynski | Method of geophysical surveying |
| CN204536438U (en) * | 2014-12-31 | 2015-08-05 | 北京森馥科技股份有限公司 | Vehicular electromagnetic radiation on-Line Monitor Device and on-line monitoring system |
-
2020
- 2020-06-09 CN CN202010518122.5A patent/CN111924094A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102385071A (en) * | 2011-10-25 | 2012-03-21 | 杨镜明 | Aerial survey device and method for geomagnetic field intensity |
| CA2833380A1 (en) * | 2013-11-12 | 2015-05-12 | Marius Moszczynski | Method of geophysical surveying |
| CN103792436A (en) * | 2014-02-21 | 2014-05-14 | 北京森馥科技股份有限公司 | On-line electromagnetic radiation long-term monitoring system |
| CN103941297A (en) * | 2014-04-21 | 2014-07-23 | 中国科学院地质与地球物理研究所 | Aeromagnetic measuring device and method based on fixed-wing unmanned aerial vehicle |
| CN104535941A (en) * | 2014-12-04 | 2015-04-22 | 上海卫星装备研究所 | Satellite magnetic test external interference magnetic field closed-loop control method under geomagnetic environment |
| CN204536438U (en) * | 2014-12-31 | 2015-08-05 | 北京森馥科技股份有限公司 | Vehicular electromagnetic radiation on-Line Monitor Device and on-line monitoring system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104122597B (en) | A kind of unmanned plane boat Magnetic Detection System and method | |
| AU2002221398B2 (en) | Gravity gradiometry | |
| AU2011206865B2 (en) | Stabilization system for sensors on moving platforms | |
| CN102628959B (en) | Captive balloon-carried type wireless telemetric seismic instrument system | |
| CN108366118A (en) | A kind of real-time mapping system of distributed unmanned plane based on cloud computing | |
| CN103941297A (en) | Aeromagnetic measuring device and method based on fixed-wing unmanned aerial vehicle | |
| CN207133659U (en) | A kind of unmanned vehicle tele-control system | |
| CN109541704B (en) | Three-axis fluxgate aeromagnetic measurement system and correction compensation method | |
| US10838099B1 (en) | Multi-mode data observation method based on unmanned aerial vehicle formation for semi-airborne electromagnetic surveying | |
| WO2006037237A1 (en) | Unmanned airborne vehicle for geophysical surveying | |
| CN107167814A (en) | Airborne telemetering system | |
| CN107515003A (en) | A kind of method for planning the aircraft patrolling power transmission lines line of flight | |
| JP6847603B2 (en) | Separation evaluation method for overhead transmission lines, separation evaluation device, separation evaluation program, and display method of separation evaluation data | |
| CN107478233A (en) | A kind of geological prospecting path planning method and system | |
| CN114993263B (en) | High-precision unmanned aerial vehicle mapping system for building based on level point positioning | |
| CN111924094A (en) | Aerial wide-area geological survey system of high prototype unmanned aerial vehicle | |
| RU201918U1 (en) | Geophysical Survey Device | |
| CN213566522U (en) | Suspension type unmanned aerial vehicle aeromagnetic detection device and nacelle thereof | |
| CN206096945U (en) | Flight measurement control module reaches unmanned vehicles who contains it | |
| CN206773189U (en) | Airborne telemetering system | |
| CN113885560B (en) | Unmanned aerial vehicle cluster ground-air transient electromagnetic measurement method suitable for landslide rapid investigation | |
| CN205450276U (en) | Quick mapping device of laser radar | |
| CN208092248U (en) | A kind of wireless seismic detector data acquisition equipment based on unmanned plane | |
| CN113204055A (en) | Aviation electromagnetic method measurement system based on unmanned aerial vehicle | |
| CN209961213U (en) | Survey and drawing point sampling device for plant protection operation real-time panoramic display of plot boundary |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20201113 |