CN113819927B - Detection system and error detection method for inclination measurement system - Google Patents

Detection system and error detection method for inclination measurement system Download PDF

Info

Publication number
CN113819927B
CN113819927B CN202111208147.6A CN202111208147A CN113819927B CN 113819927 B CN113819927 B CN 113819927B CN 202111208147 A CN202111208147 A CN 202111208147A CN 113819927 B CN113819927 B CN 113819927B
Authority
CN
China
Prior art keywords
gnss receiver
centering rod
total station
measurement unit
top center
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.)
Active
Application number
CN202111208147.6A
Other languages
Chinese (zh)
Other versions
CN113819927A (en
Inventor
臧臣戈
刘森
温小华
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.)
Suzhou Tianshuo Navigation Technology Co ltd
Original Assignee
Suzhou Tianshuo Navigation Technology Co ltd
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 Suzhou Tianshuo Navigation Technology Co ltd filed Critical Suzhou Tianshuo Navigation Technology Co ltd
Priority to CN202111208147.6A priority Critical patent/CN113819927B/en
Publication of CN113819927A publication Critical patent/CN113819927A/en
Application granted granted Critical
Publication of CN113819927B publication Critical patent/CN113819927B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C25/00Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass
    • G01C25/005Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass initial alignment, calibration or starting-up of inertial devices
    • 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
    • G01S17/00Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
    • G01S17/02Systems using the reflection of electromagnetic waves other than radio waves
    • G01S17/06Systems determining position data of a target
    • G01S17/08Systems determining position data of a target for measuring distance only
    • 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
    • G01S19/42Determining position
    • G01S19/45Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement
    • G01S19/47Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Electromagnetism (AREA)
  • Manufacturing & Machinery (AREA)
  • Length Measuring Devices With Unspecified Measuring Means (AREA)

Abstract

The invention discloses a detection system and an error detection method for an inclination measurement system, wherein the inclination measurement system comprises a GNSS receiver and a centering rod, the detection system comprises a fixing device and a detector, the GNSS receiver comprises an inertial measurement unit, and the centering rod is used for supporting the GNSS receiver; the GNSS receiver is used for acquiring attitude data of the GNSS receiver by using the inertial measurement unit after being mounted on the centering rod; the fixing device is used for fixing the centering rod and the GNSS receiver when the GNSS receiver is adjusted to the target posture according to the posture data; the detector is used for acquiring the included angle between the top center of the GNSS receiver and the connecting line of the lower end point of the centering rod and the Z axis of the inertial measurement unit under the target posture so as to acquire the measurement error of the inclination measurement system. The invention can acquire the error of the inclination measurement system, and calibrate and compensate the instrument by judging whether the error is in the allowable range, thereby improving the measurement precision.

Description

Detection system and error detection method for inclination measurement system
Technical Field
The present invention relates to a detection system and an error detection method for an inclination measurement system.
Background
In recent years, tilt measurement based on an inertial measurement unit has been increasingly popularized and applied. Through the built-in inertial measurement unit of the GNSS receiver, the attitude data of the GNSS receiver is output in real time, the direction angle, the inclined angle and the inclined direction angle of the centering rod in the inclined state are calculated, and the acquired coordinates of the phase center of the antenna of the GNSS receiver are combined, so that the coordinates of the ground point at the bottom of the inclined centering rod can be calculated.
In this inclination measurement system, there may be a series of errors that affect the calculation of the final ground point coordinates. The errors include RTK positioning errors, inertial measurement unit installation errors, centering rod and receiver connection errors, centering rod errors, and the like.
The existing inclination measurement system is complicated in error detection, and excessive detection steps are easy to cause detection errors.
Disclosure of Invention
The invention aims to overcome the defects that in the prior art, the error detection of an inclination measurement system is complicated and complicated, and the detection error is easily caused by excessive detection steps, and provides a detection system and an error detection method for the inclination measurement system, which can acquire the error of the inclination measurement system, calibrate and compensate an instrument by judging whether the error is in an allowable range, so that the measurement accuracy is improved.
The invention solves the technical problems by the following technical scheme:
a detection system for a tilt measurement system, the tilt measurement system comprising a GNSS receiver, a centering rod, a fixture, and a detector, the GNSS receiver comprising an inertial measurement unit,
the centering rod is used for supporting the GNSS receiver;
the GNSS receiver is used for acquiring attitude data of the GNSS receiver by using the inertial measurement unit after being mounted on the centering rod;
the fixing device is used for fixing the centering rod and the GNSS receiver when the GNSS receiver is adjusted to the target posture according to the posture data;
the detector is used for acquiring an included angle between a connecting line of the top center of the GNSS receiver and the lower end point of the centering rod and the Z axis of the inertial measurement unit under the target posture so as to acquire a measurement error of the inclination measurement system.
The top center of a GNSS receiver may be approximated as the receiver antenna phase center position, and ideally the line connecting the receiver upper center point and the centering stem base point should be parallel to the gravity plumb line without error.
Preferably, the fixing device is used for fixing the centering rod and the GNSS receiver when the inertial measurement unit in the GNSS receiver is adjusted to be in a horizontal state according to the attitude data;
the detector is used for acquiring the top center of the GNSS receiver and the included angle between the connecting line of the lower end point of the centering rod and the plumb line so as to acquire the measurement error of the inclination measurement system.
Preferably, the attitude data includes a heading angle, a pitch angle and a roll angle of the GNSS receiver, and the adjusting the inertial measurement unit in the GNSS receiver to a horizontal state according to the attitude data includes adjusting the pitch angle and the roll angle of the GNSS receiver to zero, and the inertial measurement unit is used for initializing before acquiring the attitude data.
Preferably, the detector comprises a total station and an operation module,
the total station is used for measuring deflection angles of the top center and the lower end point after the centering rod and the GNSS receiver are fixed by the fixing device;
the operation module is used for acquiring the included angle between the connecting line and the plumb line according to the deflection angle and the position relation between the total station and the GNSS receiver.
Preferably, the total station is used for measuring a first deflection angle of the top center and the lower end point at a first place after the centering rod and the GNSS receiver are fixed by the fixing device, the total station is also used for measuring a second deflection angle of the top center and the lower end point at a second place after the centering rod and the GNSS receiver are fixed by the fixing device, and the operation module is used for acquiring the included angle between the connecting line and the plumb line according to the first deflection angle, the second deflection angle and position data, wherein the position data comprises the position relation between the total station at the first place and the second place and the GNSS receiver.
Preferably, the inclination measurement system further comprises a laser range finder, the laser range finder faces to be perpendicular to the axial direction of the centering rod, the detector comprises a total station and an operation module, the laser range finder is used for measuring the ground distance of the laser range finder, after the centering rod and the GNSS receiver are fixed by the fixing device, and the ground position measured by the laser range finder is a to-be-measured point;
the total station is used for measuring the deflection angles of the top center and the lower end point on the to-be-measured point;
the operation module is used for acquiring the distance between the lower endpoint and the point to be detected according to the ground distance and the position of the laser range finder on the centering rod;
the operation module is further used for obtaining a vector of the connecting line of the top center and the lower endpoint according to the distance between the lower endpoint and the point to be measured, the height from the total station to the point to be measured and the deflection angle, and obtaining a measurement error of the inclination measurement system according to the included angle between the vector and the Z axis of the inertial measurement unit under the target posture.
The invention also provides an error detection method for an inclination measurement system, which is characterized in that the inclination measurement system comprises a GNSS receiver, a centering rod, a fixing device and a detector, wherein the GNSS receiver comprises an inertial measurement unit, and the error detection method comprises the following steps:
the centering rod supports the GNSS receiver;
the GNSS receiver acquires attitude data of the GNSS receiver by using the inertial measurement unit after being mounted on the centering rod;
the fixing device is used for fixing the centering rod and the GNSS receiver when the GNSS receiver is adjusted to the target posture according to the posture data;
the detector acquires the included angle between the connecting line of the top center of the GNSS receiver and the lower end point of the centering rod and the Z axis of the inertial measurement unit under the target attitude so as to acquire the measurement error of the inclination measurement system.
Preferably, the attitude data includes a heading angle, a pitch angle and a roll angle of the GNSS receiver, and the error detection method includes:
the inertial measurement unit is initialized before acquiring the attitude data;
the fixing device is used for fixing the centering rod and the GNSS receiver when the inertial measurement unit in the GNSS receiver is adjusted to be in a horizontal state according to the gesture data, wherein the adjusting of the inertial measurement unit in the GNSS receiver to be in the horizontal state according to the gesture data comprises the adjustment of the pitch angle and the roll angle of the GNSS receiver to be zero;
the detector acquires the top center of the GNSS receiver and the included angle between the connecting line of the lower end point of the centering rod and the plumb line so as to acquire the measurement error of the inclination measurement system.
Preferably, the detector comprises a total station and an operation module, and the error detection method comprises the following steps:
the total station measures deflection angles of the top center and the lower end point after the centering rod and the GNSS receiver are fixed by the fixing device;
and the operation module acquires the included angle between the connecting line and the plumb line according to the deflection angle and the position relation between the total station and the GNSS receiver.
Preferably, the error detection method includes:
the total station measures a first deflection angle of the top center and the lower end point at a first place after the centering rod and the GNSS receiver are fixed by the fixing device;
the total station measures a second deflection angle of the top center and the lower endpoint at a second place after the centering rod and the GNSS receiver are fixed by the fixing device;
the operation module obtains an included angle between the connecting line and the plumb line according to the first deflection angle, the second deflection angle and position data, wherein the position data comprises the position relation between the total station of the first place and the second place and the GNSS receiver.
On the basis of conforming to the common knowledge in the field, the above preferred conditions can be arbitrarily combined to obtain the preferred examples of the invention.
The invention has the positive progress effects that:
the invention can acquire the error of the inclination measurement system, and calibrate and compensate the instrument by judging whether the error is in the allowable range, thereby improving the measurement precision.
Drawings
Fig. 1 is a schematic structural diagram of a measurement system according to embodiment 1 of the present invention.
Fig. 2 is a flowchart of an error detection method according to embodiment 1 of the present invention.
Fig. 3 is a schematic structural diagram of a measurement system according to embodiment 2 of the present invention.
Detailed Description
The invention is further illustrated by means of the following examples, which are not intended to limit the scope of the invention.
Example 1
Referring to fig. 1, the present embodiment provides a detection system for an inclination measurement system.
The inclination measurement system comprises a GNSS receiver 11, a centering rod 12. The detection system comprises a fixture 21 and a detector 22, and the GNSS receiver comprises an inertial measurement unit.
The centering rod is used for supporting the GNSS receiver;
the GNSS receiver is used for acquiring attitude data of the GNSS receiver by using the inertial measurement unit after being mounted on the centering rod;
the fixing device is used for fixing the centering rod and the GNSS receiver when the GNSS receiver is adjusted to the target posture according to the posture data;
the detector is used for acquiring an included angle between a connecting line of the top center of the GNSS receiver and the lower end point of the centering rod and the Z axis of the inertial measurement unit under the target posture so as to acquire a measurement error of the inclination measurement system.
For convenience of measurement and operation, the target posture in this embodiment is the vertical state of the centering rod.
Further, the fixing device is used for fixing the centering rod and the GNSS receiver when the inertial measurement unit in the GNSS receiver is adjusted to be in a horizontal state according to the attitude data;
the detector is used for acquiring the top center of the GNSS receiver and the included angle between the connecting line of the lower end point of the centering rod and the plumb line so as to acquire the measurement error of the inclination measurement system.
Specifically, the attitude data includes a heading angle, a pitch angle and a roll angle of the GNSS receiver, and the adjusting the inertial measurement unit in the GNSS receiver to a horizontal state according to the attitude data includes adjusting the pitch angle and the roll angle of the GNSS receiver to zero, and the inertial measurement unit is used for initializing before acquiring the attitude data.
The whole system of the receiver and the centering rod is adjusted to enable the pitch angle and the roll angle in the output attitude angle to approach 0, and the inertial measurement unit is considered to be in an attitude with a Z axis parallel to the plumb line of the gravity.
Further, the detector comprises a total station and an operation module.
The total station is used for measuring deflection angles of the top center and the lower end point after the centering rod and the GNSS receiver are fixed by the fixing device;
the operation module is used for acquiring the included angle between the connecting line and the plumb line according to the deflection angle and the position relation between the total station and the GNSS receiver.
The operation module can be a tablet computer or an integrated function in the receiver.
Specifically, the total station is used to measure a first deflection angle of the top center and the lower end point at a first location after the centering rod and the GNSS receiver are fixed by the fixing device.
The total station is also used for measuring a second deflection angle of the top center and the lower end point at a second place after the centering rod and the GNSS receiver are fixed by the fixing device, and the operation module is used for acquiring the included angle between the connecting line and the plumb line according to the first deflection angle, the second deflection angle and position data, wherein the position data comprises the position relation between the total station at the first place and the second place and the GNSS receiver.
Referring to fig. 2, with the above detection system, this embodiment further provides an error detection method, including:
step 100, supporting the GNSS receiver by the centering rod;
step 101, acquiring attitude data of the GNSS receiver by using the inertial measurement unit after the GNSS receiver is mounted on the centering rod;
102, the fixing device fixes the centering rod and the GNSS receiver when adjusting the GNSS receiver to the target posture according to the posture data;
and 103, the detector acquires an included angle between a connecting line of the top center of the GNSS receiver and the lower end point of the centering rod and the Z axis of the inertial measurement unit under the target posture so as to acquire a measurement error of the inclination measurement system.
Specifically, the attitude data includes a heading angle, a pitch angle and a roll angle of the GNSS receiver, and between step 100 and step 101 includes: the inertial measurement unit is initialized before acquiring the attitude data;
step 102 specifically comprises: the fixing device is used for fixing the centering rod and the GNSS receiver when the inertial measurement unit in the GNSS receiver is adjusted to be in a horizontal state according to the gesture data, wherein the adjusting of the inertial measurement unit in the GNSS receiver to be in the horizontal state according to the gesture data comprises the adjustment of the pitch angle and the roll angle of the GNSS receiver to be zero;
step 103 specifically comprises: the detector acquires the top center of the GNSS receiver and the included angle between the connecting line of the lower end point of the centering rod and the plumb line so as to acquire the measurement error of the inclination measurement system.
Further, the detector includes a total station and an operation module, and step 103 includes:
the total station measures deflection angles of the top center and the lower end point after the centering rod and the GNSS receiver are fixed by the fixing device;
and the operation module acquires the included angle between the connecting line and the plumb line according to the deflection angle and the position relation between the total station and the GNSS receiver.
Specifically, step 103 includes:
the total station measures a first deflection angle of the top center and the lower end point at a first place after the centering rod and the GNSS receiver are fixed by the fixing device;
the total station measures a second deflection angle of the top center and the lower endpoint at a second place after the centering rod and the GNSS receiver are fixed by the fixing device;
the operation module obtains an included angle between the connecting line and the plumb line according to the first deflection angle, the second deflection angle and position data, wherein the position data comprises the position relation between the total station of the first place and the second place and the GNSS receiver.
In this embodiment, the positional relationship includes a distance between the total station and the GNSS receiver.
Example 2
This embodiment is substantially the same as embodiment 1, except that:
referring to fig. 3, the inclination measurement system further includes a laser rangefinder 13, the laser rangefinder 13 faces to be perpendicular to the axial direction of the centering rod, the detector includes a total station and an operation module, the laser rangefinder is used for measuring a ground distance 14 on which the laser rangefinder faces after the centering rod and the GNSS receiver are fixed by the fixing device, and a ground position measured by the laser rangefinder is a point 15 to be measured;
the total station 22 is used for measuring the deflection angle 18 of the top center 16 and the lower end point 17 on the to-be-measured point;
the operation module is used for acquiring the distance 19 between the lower endpoint and the point to be measured according to the ground distance 14 and the position of the laser range finder on the centering rod;
the operation module is further configured to obtain a vector of the connection line between the top center and the lower endpoint according to a distance 19 between the lower endpoint and the point to be measured, a height 20 between the total station and the point to be measured, and the deflection angle 18, and obtain a measurement error of the inclination measurement system according to an included angle between the vector and a Z axis of the inertial measurement unit under the target posture.
The vector can have two solution values, and the minimum value of the included angle between the vector and the Z axis of the inertial measurement unit is taken as the calculated quantity, or the two solution values are verified through the top center and the point to be tested to obtain a vector result.
With the above detection system, the error detection method of the present embodiment includes:
the total station measures the deflection angles of the top center and the lower end point on the to-be-measured point;
the operation module acquires the distance between the lower endpoint and the point to be detected according to the ground distance, the gesture data and the position of the laser range finder on the centering rod;
the operation module obtains a vector of a connecting line of the top center and the lower endpoint according to the distance between the lower endpoint and the point to be measured, the height from the total station to the point to be measured and the deflection angle, and obtains a measurement error of the inclination measurement system according to an included angle between the vector and a Z axis of the inertial measurement unit under the target posture.
While specific embodiments of the invention have been described above, it will be appreciated by those skilled in the art that these are by way of example only, and the scope of the invention is defined by the appended claims. Various changes and modifications to these embodiments may be made by those skilled in the art without departing from the principles and spirit of the invention, but such changes and modifications fall within the scope of the invention.

Claims (9)

1. A detection system for an inclination measurement system, characterized in that the inclination measurement system comprises a GNSS receiver and a centering rod, the detection system comprises a fixture and a detector, the GNSS receiver comprises an inertial measurement unit,
the centering rod is used for supporting the GNSS receiver;
the GNSS receiver is used for acquiring attitude data of the GNSS receiver by using the inertial measurement unit after being mounted on the centering rod;
the fixing device is used for fixing the centering rod and the GNSS receiver when the GNSS receiver is adjusted to the target posture according to the posture data;
the detector is used for acquiring an included angle between a connecting line of the top center of the GNSS receiver and the lower end point of the centering rod and the Z axis of the inertial measurement unit under the target attitude so as to acquire a measurement error of the inclination measurement system;
the fixing device is used for fixing the centering rod and the GNSS receiver when the inertial measurement unit in the GNSS receiver is adjusted to be in a horizontal state according to the attitude data;
the detector is used for acquiring the top center of the GNSS receiver and the included angle between the connecting line of the lower end point of the centering rod and the plumb line so as to acquire the measurement error of the inclination measurement system.
2. The detection system of claim 1, wherein the attitude data includes heading, pitch and roll angles of a GNSS receiver, and wherein adjusting an inertial measurement unit within the GNSS receiver to a horizontal state based on the attitude data includes adjusting the pitch and roll angles of the GNSS receiver to zero, the inertial measurement unit being configured to initialize prior to acquiring the attitude data.
3. The detection system of claim 1, wherein the detector comprises a total station and an arithmetic module,
the total station is used for measuring deflection angles of the top center and the lower end point after the centering rod and the GNSS receiver are fixed by the fixing device;
the operation module is used for acquiring the included angle between the connecting line and the plumb line according to the deflection angle and the position relation between the total station and the GNSS receiver.
4. The inspection system of claim 3 wherein the total station is configured to measure a first deflection angle of the top center and the lower end point at a first location after the centering rod and the GNSS receiver are secured by the fixture, and is further configured to measure a second deflection angle of the top center and the lower end point at a second location after the centering rod and the GNSS receiver are secured by the fixture, the computing module being configured to obtain the angle of the link from the plumb line based on the first deflection angle, the second deflection angle, and position data, the position data including a positional relationship of the total station and the GNSS receiver at the first location and the second location.
5. The inspection system of claim 1 further comprising a laser rangefinder oriented perpendicular to the axis of the centering rod, the inspection system comprising a total station and an operation module, the laser rangefinder configured to measure a ground distance of the laser rangefinder after the centering rod and the GNSS receiver are secured by the securing device, the ground position measured by the laser rangefinder being the point to be inspected;
the total station is used for measuring the deflection angles of the top center and the lower end point on the to-be-measured point;
the operation module is used for acquiring the distance between the lower endpoint and the point to be detected according to the ground distance and the position of the laser range finder on the centering rod;
the operation module is further used for obtaining a vector of the connecting line of the top center and the lower endpoint according to the distance between the lower endpoint and the point to be measured, the height from the total station to the point to be measured and the deflection angle, and obtaining a measurement error of the inclination measurement system according to the included angle between the vector and the Z axis of the inertial measurement unit under the target posture.
6. An error detection method for detecting an inclination measurement system by a detection system, wherein the inclination measurement system comprises a GNSS receiver and a centering rod, the detection system comprises a fixture and a detector, the GNSS receiver comprises an inertial measurement unit, the error detection method comprising:
the centering rod supports the GNSS receiver;
the GNSS receiver acquires attitude data of the GNSS receiver by using the inertial measurement unit after being mounted on the centering rod;
the fixing device is used for fixing the centering rod and the GNSS receiver when the GNSS receiver is adjusted to the target posture according to the posture data;
the detector acquires an included angle between the top center of the GNSS receiver and the connecting line of the lower end point of the centering rod and the Z axis of the inertial measurement unit under the target attitude so as to acquire a measurement error of the inclination measurement system;
the error detection method further comprises the following steps:
the fixing device is used for fixing the centering rod and the GNSS receiver when the inertial measurement unit in the GNSS receiver is adjusted to be in a horizontal state according to the attitude data;
the detector acquires the top center of the GNSS receiver and the included angle between the connecting line of the lower end point of the centering rod and the plumb line so as to acquire the measurement error of the inclination measurement system.
7. The error detection method of claim 6, wherein the attitude data includes heading, pitch and roll angles of a GNSS receiver, the error detection method comprising:
the inertial measurement unit is initialized before acquiring the attitude data;
the fixing device is used for fixing the centering rod and the GNSS receiver when the inertial measurement unit in the GNSS receiver is adjusted to be in a horizontal state according to the gesture data, wherein the adjusting of the inertial measurement unit in the GNSS receiver to be in the horizontal state according to the gesture data comprises the adjustment of the pitch angle and the roll angle of the GNSS receiver to be zero;
the detector acquires the top center of the GNSS receiver and the included angle between the connecting line of the lower end point of the centering rod and the plumb line so as to acquire the measurement error of the inclination measurement system.
8. The error detection method according to claim 7, wherein the detector includes a total station and an operation module, the error detection method comprising:
the total station measures deflection angles of the top center and the lower end point after the centering rod and the GNSS receiver are fixed by the fixing device;
and the operation module acquires the included angle between the connecting line and the plumb line according to the deflection angle and the position relation between the total station and the GNSS receiver.
9. The error detection method of claim 8, wherein the error detection method comprises:
the total station measures a first deflection angle of the top center and the lower end point at a first place after the centering rod and the GNSS receiver are fixed by the fixing device;
the total station measures a second deflection angle of the top center and the lower endpoint at a second place after the centering rod and the GNSS receiver are fixed by the fixing device;
the operation module obtains an included angle between the connecting line and the plumb line according to the first deflection angle, the second deflection angle and position data, wherein the position data comprises the position relation between the total station of the first place and the second place and the GNSS receiver.
CN202111208147.6A 2021-10-18 2021-10-18 Detection system and error detection method for inclination measurement system Active CN113819927B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202111208147.6A CN113819927B (en) 2021-10-18 2021-10-18 Detection system and error detection method for inclination measurement system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202111208147.6A CN113819927B (en) 2021-10-18 2021-10-18 Detection system and error detection method for inclination measurement system

Publications (2)

Publication Number Publication Date
CN113819927A CN113819927A (en) 2021-12-21
CN113819927B true CN113819927B (en) 2024-04-12

Family

ID=78920562

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202111208147.6A Active CN113819927B (en) 2021-10-18 2021-10-18 Detection system and error detection method for inclination measurement system

Country Status (1)

Country Link
CN (1) CN113819927B (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102207380A (en) * 2011-06-09 2011-10-05 中国人民解放军第二炮兵工程学院 High-precision horizontal axis tilt error compensation method
CN102680001A (en) * 2012-05-16 2012-09-19 南京信息工程大学 Inclination correction device for centering rod
CN108732595A (en) * 2018-04-12 2018-11-02 石家庄铁路职业技术学院 A kind of RTK rover receiver of integrated inertial navigation and magnetometer
CN109425325A (en) * 2017-08-22 2019-03-05 杭州通泰测绘有限公司 A kind of multi-rise building object inclination measurement method
CN109814133A (en) * 2019-03-07 2019-05-28 上海华测导航技术股份有限公司 GNSS receiver inclinometric system, method, apparatus and storage medium

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10466050B2 (en) * 2014-06-06 2019-11-05 Carlson Software, Inc. Hybrid total station with electronic leveling

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102207380A (en) * 2011-06-09 2011-10-05 中国人民解放军第二炮兵工程学院 High-precision horizontal axis tilt error compensation method
CN102680001A (en) * 2012-05-16 2012-09-19 南京信息工程大学 Inclination correction device for centering rod
CN109425325A (en) * 2017-08-22 2019-03-05 杭州通泰测绘有限公司 A kind of multi-rise building object inclination measurement method
CN108732595A (en) * 2018-04-12 2018-11-02 石家庄铁路职业技术学院 A kind of RTK rover receiver of integrated inertial navigation and magnetometer
CN109814133A (en) * 2019-03-07 2019-05-28 上海华测导航技术股份有限公司 GNSS receiver inclinometric system, method, apparatus and storage medium

Also Published As

Publication number Publication date
CN113819927A (en) 2021-12-21

Similar Documents

Publication Publication Date Title
US9605962B2 (en) Inclination sensor
CN103063203B (en) Geodetic surveying system and method for operating geodetic surveying system
WO2018129865A1 (en) Tilt measurement method for rtk measuring receiver
US7764365B2 (en) Combination laser detector and global navigation satellite receiver system
US20060271298A1 (en) Method for correcting a 3D location measured by a tracking system assuming a vertical offset
CN109655079B (en) Method for measuring coordinate system from star sensor to prism coordinate system
CN104011502B (en) Automatically the measurement of the level
CN112964252B (en) Positioning method and system based on inertial measurement unit and RTK receiver
CN107063201A (en) Carry the accurate depth measurement erecting device of integration and its system of calibration system
CN104297771B (en) GNSS device and method for precisely and quickly measuring elevation
US8289528B2 (en) Tilt sensor for a measuring instrument
US20180217263A1 (en) Rover And Rover Measuring System
CN103658721A (en) Visual axis calibration method of off-axis camera
CN114858140B (en) Point cloud coordinate transformation method and device for deep-buried tunnel structural surface based on target device
CN205449052U (en) Device for measuring building inclination angle by laser
CN108775899B (en) Deep mining well up-down coordinate system connection method based on pseudolite and inertia information
CN201983799U (en) High-accuracy detection and demarcation device of inertia orientation equipment
CN113819927B (en) Detection system and error detection method for inclination measurement system
CN108917789B (en) Inclinometer orthogonality evaluation method based on relative included angle of pitch axis and roll axis
CN106482743B (en) A kind of rapid detection method of relative position measurement equipment
CN201955098U (en) High-precision detection and calibration device for inertia orientation equipment
CN107478209B (en) The detection method of Super High axial control network
US11385052B2 (en) Surveying instrument
CN113311401A (en) Calibration verification component, system and method
CN206670633U (en) Carry the integrated accurate depth measurement erecting device and its system of calibration system

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
CB02 Change of applicant information

Address after: Unit E2-601, Artificial Intelligence Industrial Park, No. 88, Jinjihu Avenue, Suzhou Industrial Park, China (Jiangsu) Pilot Free Trade Zone, Suzhou City, Jiangsu Province, 215000

Applicant after: Suzhou Tianshuo Navigation Technology Co.,Ltd.

Address before: Room 305, building 1, 1228 Jinhu Road, China (Shanghai) pilot Free Trade Zone, Pudong New Area, Shanghai, 201206

Applicant before: Shanghai Jingrong Network Technology Co.,Ltd.

CB02 Change of applicant information
GR01 Patent grant
GR01 Patent grant