CN111707256A - Comprehensive positioning navigation equipment for rapidly arranging special vehicle by aid of navigation lamp - Google Patents
Comprehensive positioning navigation equipment for rapidly arranging special vehicle by aid of navigation lamp Download PDFInfo
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- CN111707256A CN111707256A CN202010402094.0A CN202010402094A CN111707256A CN 111707256 A CN111707256 A CN 111707256A CN 202010402094 A CN202010402094 A CN 202010402094A CN 111707256 A CN111707256 A CN 111707256A
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- 238000005259 measurement Methods 0.000 claims description 27
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- 239000008358 core component Substances 0.000 description 5
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
- G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
- G01C21/165—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation combined with non-inertial navigation instruments
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining 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
- G01S19/40—Correcting position, velocity or attitude
- G01S19/41—Differential correction, e.g. DGPS [differential GPS]
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining 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
- G01S19/42—Determining position
- G01S19/48—Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining 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
- G01S19/42—Determining position
- G01S19/48—Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system
- G01S19/49—Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system whereby the further system is an inertial position system, e.g. loosely-coupled
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- Radar, Positioning & Navigation (AREA)
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- General Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- Automation & Control Theory (AREA)
- Navigation (AREA)
Abstract
The invention discloses comprehensive positioning navigation equipment for rapidly arranging special vehicles by aid of navigation lamps, and relates to the technical field of positioning navigation. According to the invention, the position information and the advancing direction information of the special vehicle are comprehensively positioned through signals of the differential Beidou satellite receiver, the single-point Beidou satellite receiver, the sideline camera, the inertial navigation module, the angle and angular velocity sensors, the laser altimeter and the like, and reliable and high-precision positioning navigation support can be provided for realizing tasks such as rapid arrangement of an airport navigation aid lamp. The invention comprehensively utilizes the Beidou satellite signals and various sensor information, has the advantages of high positioning and navigation precision, has various working modes which can be freely switched, and still has certain applicability under the conditions that the differential Beidou satellite signals are unavailable and the vision of the sideline of the airport runway is unavailable.
Description
Technical Field
The invention belongs to the technical field of positioning and navigation, and particularly relates to comprehensive positioning and navigation equipment for quickly arranging special vehicles by aid of navigation lamps.
Background
In some special application occasions, such as task scenes of airport navigation aid lamp arrangement, street lamp arrangement, lane marking and the like, special vehicles which need to execute the special tasks have high-precision positioning capability and navigation capability, and can accurately finish the tasks according to planned indexes.
Patent CN 208477375U (title: a positioning navigation device based on smart car, granted announcement date: 2019.02.25) discloses a positioning navigation device based on smart car, which comprises a shell, a rotating rod, a telescopic antenna device, a sliding block and the like, and solves the problems that the information transmission device used by the existing positioning navigation device of smart car can not transmit information well and the information transmission performance can not meet the requirements.
The design and implementation method of the integrated navigation equipment based on the Beidou navigation positioning is researched in the document 'design and implementation of the integrated navigation equipment based on the Beidou positioning' (author: Guojie; type: engineering Master academic paper; unit: Sigan electronic technology university; time: 12 months in 2018), the overall requirements of the integrated navigation equipment are introduced, the calculation of attitude information and the transmission of multi-path information for a calculation and transmission core by using an inertial navigation module are provided, and other general cases are provided on the basis.
Due to the particularity of the task, the positioning and navigation equipment of the special vehicle is required to have high positioning and navigation accuracy, the application of the positioning and navigation equipment is often limited by the use environment, various sensors are required to be integrated to provide positioning and navigation information in an auxiliary manner, and at present, no relevant literature data of the high-accuracy comprehensive positioning and navigation equipment for quickly arranging the special vehicle by the aid of the navigation lamp exists.
Disclosure of Invention
The invention mainly aims to provide comprehensive positioning navigation equipment for quickly arranging special vehicles by aid of navigation lamps, and aims to provide reliable and high-precision positioning navigation equipment for the special vehicles and provide necessary technical support for finishing given arrangement tasks of the special vehicles.
In order to achieve the purpose, the invention provides comprehensive positioning navigation equipment for quickly arranging special vehicles by aid of navigation lights based on a Beidou satellite system.
The vehicle-mounted hardware subsystem comprises a receiving and sensing part, an interface part and a processing part, wherein the receiving and sensing part comprises a differential Beidou receiver, an inertial navigation module, a steering wheel angle sensor, a wheel angular velocity sensor, a wheel center laser altimeter, a single-point Beidou receiver and a sideline camera, the interface part comprises a laser altimeter interface, an angle sensor interface, an angular velocity sensor interface and a visual equipment interface, and the processing part comprises an image processing module and a CPU control panel; the differential Beidou receiver and the single-point Beidou receiver provide special vehicle position and advancing direction measurement, the inertial navigation module provides acceleration, angular speed and angle measurement, the steering wheel angle sensor provides turning angle measurement, the wheel angle sensor provides wheel turn number measurement, the wheel angular speed sensor provides advancing speed measurement of a vehicle, the wheel center laser altimeter provides ground height of wheels, driving errors caused by wheel sinking are indirectly measured, and the sideline camera is used for detecting sidelines of an airport runway and correcting the advancing direction of a special vehicle; the image processing module is provided with the visual equipment interface and is used for accessing a visual signal of the sideline camera, and a processing result of the image processing module is transmitted to the CPU control panel; the laser altimeter interface, the angle sensor interface and the angular velocity sensor interface are arranged on the CPU control panel, the wheel center laser altimeter is connected with the CPU control panel through the laser altimeter interface, the steering wheel angle sensor and the wheel angle sensor are connected with the CPU control panel through the angle sensor interface, and the wheel angular velocity sensor is connected with the CPU control panel through the angular velocity sensor interface;
a positioning navigation algorithm is integrated in the navigation software subsystem and is used for determining the position and the advancing direction of the special vehicle;
and the display terminal subsystem is used for displaying the positioning and navigation information of the special vehicle.
The positioning navigation algorithm comprises a difference Beidou and inertial navigation combined filter, a sensor and an inertial navigation combined filter.
The integrated positioning and navigation equipment has four working modes comprising a first working mode, a second working mode, a third working mode and a fourth working mode,
the first working mode is a normal borderline mode, and refers to a positioning navigation mode in which a differential Beidou satellite signal is available and the sideline vision of the airport runway is available;
the second working mode is a normal borderless mode, and is a positioning navigation mode in which a differential Beidou satellite signal is available but airport runway sideline vision is unavailable.
The third working mode is a silent borderline mode, and refers to a positioning navigation mode in which the differential Beidou satellite signals are unavailable, but the airport runway borderline vision is available.
The fourth working mode is a silent borderless mode, and refers to a positioning navigation mode in which a differential Beidou satellite signal is unavailable and airport runway borderline vision is unavailable.
In the first working mode, the differential Beidou receiver is adopted for direct positioning, information such as speed and angle is provided with an original measurement value by the inertial navigation component, the differential Beidou and inertial navigation combined filter is adopted for a navigation algorithm, and course information is further corrected by a view field sideline.
In the second working mode, the differential Beidou receiver is adopted for direct positioning, information such as speed and angle is provided with an original measurement value by the inertial navigation component, and the differential Beidou and inertial navigation combined filter is adopted for a navigation algorithm.
In the third working mode, the single-point Beidou satellite signal is adopted to assist the multi-view vision to carry out direct positioning, the inertial navigation component provides original measurement information such as speed, angle and the like, the navigation algorithm adopts a sensor and an inertial navigation combined filter, and the course information is further corrected by a view field sideline.
And in the fourth working mode, positioning and orientation are carried out in a mode of combining a sensor and inertial navigation.
Furthermore, the four working modes can be switched, and the switching mode comprises manual switching and automatic switching.
Preferably, the steering wheel angle sensor and the wheel angle sensor use rotating code disks.
The beneficial effects of the technical scheme of the invention are mainly embodied in the following two aspects:
firstly, the differential Beidou satellite signal, the single-point Beidou satellite signal and various sensor information including a sideline camera, a steering wheel angle sensor, a wheel angular velocity sensor and the like can be comprehensively utilized, and the method has the advantages of high positioning and navigation accuracy;
secondly, the invention has a plurality of freely switchable working modes, and still has certain applicability under the conditions that the differential Beidou satellite signal is unavailable, the sideline visual signal of the airport runway is unavailable and the like.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the structures shown in the drawings without creative efforts.
FIG. 1 is a system architecture diagram of the integrated positioning and navigation device of the present invention;
FIG. 2 is a hardware configuration diagram (side view) of the invention on a special vehicle with a navigation aid light for rapid deployment;
FIG. 3 is a core component architecture diagram of the present invention;
FIG. 4 is a schematic diagram of a first mode of operation of the present invention;
FIG. 5 is a schematic diagram of a second mode of operation of the present invention;
FIG. 6 is a schematic diagram of a third mode of operation of the present invention;
FIG. 7 is a schematic diagram of a fourth mode of operation of the present invention;
fig. 8 is a schematic diagram illustrating the switching process of four working modes according to the present invention.
Reference numerals: 1-vehicle head; 2, a compartment; 3-front wheel; 4-rear wheel; 5-a steering wheel; 6, a belt; 7, paving; 8, a damping platform; 9 — core Components of the invention; 10-sideline camera; 11-wheel center laser altimeter; 12-rotating code disc.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
The invention provides high-precision comprehensive positioning navigation equipment aiming at the use requirements of special vehicles with quickly arranged navigation lights. In the embodiment, the use requirements of the special vehicle are as follows:
when the special vehicle is unfolded for operation, the special vehicle is required to linearly travel along the runway direction at the speed of not less than 15 km/h;
the specific operation requirements of the special vehicle comprise: the distance between two adjacent lamps is 60m, the distance error between two adjacent lamps is less than or equal to 0.5m, the distance error in the direction vertical to the runway is less than or equal to 0.1m, and the placement error of the horizontal angle of the lamp is less than or equal to 2 degrees.
The design idea of the invention is as follows: aiming at the working characteristics of the special vehicle, corresponding sensor information (comprising a sideline camera, a steering wheel angle sensor, a wheel angular velocity sensor and the like) and differential Beidou satellite signals, single-point Beidou satellite signals and the like are combined, so that reliable and high-precision positioning navigation equipment is provided for the special vehicle.
According to the indexes provided by the background use requirements, in order to meet the index requirements, the system index requirements of the positioning navigation equipment are specifically as follows:
the point location error between the electronic map and the actual runway is less than or equal to 2cm (1 sigma);
the absolute positioning precision of a single point in the runway under the support of the Beidou differential is less than or equal to 10cm (1 sigma);
the single-point absolute positioning precision in the runway is less than or equal to 15cm (1 sigma) during wireless silence (the requirement is met within 1 hour of working time);
the direction vertical to the runway is less than or equal to 3cm (1 sigma) (multi-means assistance);
the error of the horizontal angle is less than or equal to 2 degrees (3 sigma) (the error is fully satisfied within 1 hour of working time).
In order to calculate the traveling direction and the traveling mileage of a special vehicle quickly arranged by a navigation aid lamp, the invention provides a comprehensive positioning navigation device which comprises a vehicle-mounted hardware subsystem, a navigation software subsystem and a display terminal subsystem. The vehicle-mounted hardware subsystem comprises a receiving and sensing part, an interface part and a processing part, wherein the receiving and sensing part comprises a differential Beidou receiver, an inertial navigation module, a steering wheel angle sensor, a wheel angular velocity sensor, a wheel center laser altimeter, a single-point Beidou receiver and a sideline camera, the interface part comprises a laser altimeter interface, an angle sensor interface, an angular velocity sensor interface and a visual equipment interface, and the processing part comprises an image processing module and a CPU control panel; a positioning navigation algorithm is integrated in the navigation software subsystem and is used for determining the position and the advancing direction of the special vehicle; and the display terminal subsystem is used for displaying the positioning and navigation information of the special vehicle.
The system architecture diagram of the integrated positioning navigation equipment is shown in figure 1, and the equipment adopts the following sensors for measurement: the special vehicle position and advancing direction measurement is provided by utilizing a differential Beidou receiver and a single-point Beidou receiver, the inertial navigation module provides acceleration, angular speed and angle measurement, the steering wheel angle sensor provides turning angle measurement, the wheel angle sensor provides wheel turn number measurement (odometer), the wheel angle sensor provides advancing speed measurement of a vehicle, the wheel center laser altimeter provides the ground height of the wheel, the traveling error caused by wheel depression is indirectly measured, and the sideline camera is used for detecting the sideline of an airport runway and correcting the advancing direction of the special vehicle. These measurements are redundant and calibrated to each other, and can be used simultaneously or separately.
Fig. 2 is a hardware configuration diagram of the invention on a special vehicle with a navigation aid lamp rapidly arranged, wherein 1 and 2 respectively represent a head and a carriage of the special vehicle, 3 and 4 respectively represent a front wheel and a rear wheel, 5 represents a steering wheel, 6 represents a belt, and 7 represents a road surface; a core component 9 of the invention is arranged above a vehicle head 1 through a damping platform 8; the sideline camera 10 is used for detecting the sidelines of the airport runway; the wheel center laser altimeter 11 is arranged at the positive center position of the front wheel 3 and the rear wheel 4 of the special vehicle; in the embodiment, the wheel angle sensor and the steering wheel angle sensor are both realized by adopting the rotary coded disc 12, and the rotary coded disc has the advantages of strong resolving power, high measurement precision, reliable work and the like, and is a common displacement sensor for measuring the rotating angle position of a shaft.
The architecture diagram of the core component 9 of the invention is shown in fig. 3, and the core component mainly comprises a differential Beidou receiver, an inertial navigation module, and an interface part and a processing part in a vehicle-mounted hardware subsystem. And the image processing module is provided with a visual equipment interface and is used for accessing the visual signals of the sideline camera, and the image processing module analyzes and processes the visual signals acquired by the camera and transmits the processing result to the CPU control panel. The central processing unit is characterized in that the CPU control panel is provided with the laser altimeter interface, the angle sensor interface and the angular velocity sensor interface, the wheel center laser altimeter is connected with the CPU control panel through the laser altimeter interface, the steering wheel angle sensor and the wheel angle sensor are connected with the CPU control panel through the angle sensor interface, and the wheel angular velocity sensor is connected with the CPU control panel through the angular velocity sensor interface.
As can be seen from fig. 1, the present invention has two types of modes during operation, namely, a differential beidou mode and a silent operation mode, wherein the silent operation mode refers to a situation without differential beidou satellite signals. Considering that there are two cases of availability and unavailability of airport runway edge using edge cameras, the present invention can be subdivided into four specific modes of operation, detailed as follows:
a first operating mode: normal side line
The normal sideline working mode refers to a positioning navigation mode in which a differential Beidou satellite signal is available and sideline vision of an airport runway is available. As shown in fig. 4, in this mode, the differential compass receiver is used for direct positioning, the inertial navigation component provides an original measurement value for speed, angle and other information, the differential compass and inertial navigation combined filter is used for a navigation algorithm, and the course information is further corrected by a view field edge. This mode is also the default mode of operation when wireless signals are available.
A second working mode: normal no sideline
The normal borderless working mode refers to a positioning navigation mode in which differential Beidou satellite signals are available but borderline vision of the airport runway is unavailable. As shown in fig. 5, in this mode, the differential compass receiver is used for direct positioning, the inertial navigation component provides an original measurement value for information such as velocity and angle, and the differential compass and inertial navigation combined filter is used for the navigation algorithm. This mode is the mode of operation when the vehicle enters the middle of the airport.
The third working mode is as follows: silent sidelines
The silent borderline working mode refers to a positioning navigation mode in which differential Beidou satellite signals are unavailable, but airport runway borderline vision is available. As shown in fig. 6, during radio silence, the differential beidou satellite signal is unavailable, the single-point beidou satellite signal (beidou absolute positioning) is used to assist multi-view vision to perform direct positioning, the inertial navigation component provides original measurement information such as speed and angle, the navigation algorithm uses a sensor and an inertial navigation combination filter, and the course information is further corrected by the view field sideline.
The fourth working mode: silent borderless
The silent borderline working mode refers to a positioning navigation mode that the differential Beidou satellite signals are unavailable and the airport runway borderline vision is unavailable. As shown in fig. 7, in the wireless silence situation, the borderline vision is not available when the vehicle travels to the middle of the airport, and the positioning and orientation are performed by using the combined filtering of the sensor and the inertial navigation.
Switching of four operating modes
The four working modes can be switched, either manually or automatically, and the switching process is shown in fig. 8.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the scope of the present invention, and all modifications and equivalents of the present invention, which are made by the contents of the present specification and the accompanying drawings, or directly/indirectly applied to other related technical fields, are included in the scope of the present invention.
Claims (9)
1. A comprehensive positioning navigation device for a special vehicle with a navigation aid lamp arranged quickly comprises a vehicle-mounted hardware subsystem, a navigation software subsystem and a display terminal subsystem,
the vehicle-mounted hardware subsystem comprises a receiving and sensing part, an interface part and a processing part, wherein the receiving and sensing part comprises a differential Beidou receiver, an inertial navigation module, a steering wheel angle sensor, a wheel angular velocity sensor, a wheel center laser altimeter, a single-point Beidou receiver and a sideline camera, the interface part comprises a laser altimeter interface, an angle sensor interface, an angular velocity sensor interface and a visual equipment interface, and the processing part comprises an image processing module and a CPU control panel; the differential Beidou receiver and the single-point Beidou receiver provide special vehicle position and advancing direction measurement, the inertial navigation module provides acceleration, angular speed and angle measurement, the steering wheel angle sensor provides turning angle measurement, the wheel angle sensor provides wheel turn number measurement, the wheel angular speed sensor provides advancing speed measurement of a vehicle, the wheel center laser altimeter provides ground height of wheels, driving errors caused by wheel sinking are indirectly measured, and the sideline camera is used for detecting sidelines of an airport runway and correcting the advancing direction of a special vehicle; the image processing module is provided with the visual equipment interface and is used for accessing a visual signal of the sideline camera, and a processing result of the image processing module is transmitted to the CPU control panel; the laser altimeter interface, the angle sensor interface and the angular velocity sensor interface are arranged on the CPU control panel, the wheel center laser altimeter is connected with the CPU control panel through the laser altimeter interface, the steering wheel angle sensor and the wheel angle sensor are connected with the CPU control panel through the angle sensor interface, and the wheel angular velocity sensor is connected with the CPU control panel through the angular velocity sensor interface;
a positioning navigation algorithm is integrated in the navigation software subsystem and is used for determining the position and the advancing direction of the special vehicle;
and the display terminal subsystem is used for displaying the positioning and navigation information of the special vehicle.
2. The integrated positioning and navigation device for the special vehicle with the navigation aid lamp arranged rapidly as claimed in claim 1, wherein the positioning and navigation algorithm comprises a differential Beidou and inertial navigation combination filter, a sensor and an inertial navigation combination filter.
3. The integrated positioning and navigation device of a special vehicle with fast-arrangement navigation lights as claimed in claim 1, wherein the integrated positioning and navigation device has four operation modes, including a first operation mode, a second operation mode, a third operation mode and a fourth operation mode,
the first working mode is a normal borderline mode, and refers to a positioning navigation mode in which a differential Beidou satellite signal is available and the sideline vision of the airport runway is available;
the second working mode is a normal borderless mode, and is a positioning navigation mode in which a differential Beidou satellite signal is available but airport runway sideline vision is unavailable.
The third working mode is a silent borderline mode, and refers to a positioning navigation mode in which the differential Beidou satellite signals are unavailable, but the airport runway borderline vision is available.
The fourth working mode is a silent borderless mode, and refers to a positioning navigation mode in which a differential Beidou satellite signal is unavailable and airport runway borderline vision is unavailable.
4. The integrated positioning and navigation device of the special vehicle with the navigation aid lamps arranged rapidly as claimed in claim 1 or 3, wherein in the first operation mode, the direct positioning adopts a differential Beidou receiver, information such as speed and angle is provided by an inertial navigation component to be a raw measurement value, a navigation algorithm adopts a combined filter of differential Beidou and inertial navigation, and course information is further corrected by a view field sideline.
5. The integrated positioning and navigation device for special vehicles with navigation aid lamps arranged rapidly as claimed in claim 1 or 3, wherein in the second operation mode, the direct positioning uses a differential Beidou receiver, the information of speed, angle and the like is provided by an inertial navigation component to obtain raw measurement values, and the navigation algorithm uses a combined filter of differential Beidou and inertial navigation.
6. The integrated positioning and navigation equipment for the special vehicle with the navigation aid lamps arranged rapidly as claimed in claim 1 or 3, wherein in the third operating mode, the single-point Beidou satellite signal is used for assisting the multi-view vision to perform direct positioning, the inertial navigation component provides original measurement information such as speed and angle, the navigation algorithm adopts a sensor and an inertial navigation combination filter, and the course information is further corrected by the view field sideline.
7. The integrated positioning and navigation device for the special vehicle with the navigation lights arranged rapidly as claimed in claim 1 or 3, wherein in the fourth operation mode, the positioning and orientation are performed by means of combined filtering of a sensor and inertial navigation.
8. The integrated positioning and navigation device for the special vehicle with the navigation lights arranged rapidly as claimed in claim 1 or 3, wherein the four operation modes can be switched, and the switching mode includes manual switching and automatic switching.
9. The integrated positioning and navigation device of a special vehicle with fast-arrangement navigation lights as claimed in claim 1, wherein the steering wheel angle sensor and the wheel angle sensor employ rotating code discs.
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CN112987786A (en) * | 2021-02-26 | 2021-06-18 | 山东鹰格信息工程有限公司 | Beidou-based navigation aid facility calibration method and device, storage medium and robot |
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