Monday, January 1, 2024

The Advantages and Disadvantages of the Transmission Mode of Tilt Sensor



In today’s industrial and commercial environment, tilt sensors are increasingly used to measure and monitor the tilt angle of equipment or structures. Depending on the data transmission method, tilt meters can be divided into wired and wireless types. In this article, we’ll delve into both types of tilt sensors, including the pros and cons, and how to choose the best solution for your specific needs. 

1. Advantages&disadvantages of wired tilt sensor

Wired inclination sensor built-in high performance MCU built-in algorithm, through a high oversampling rate, improve the high frequency characteristics of the data, through the data filtering algorithm to remove unreasonable accidental error data, Kalman filter algorithm for higher precision data processing, suitable for monitoring the structure deformation monitoring field with high monitoring frequency requirements. Wired tilt meters usually use RS485 bus or other similar bus protocols to transmit inclination signals. RS485 is a serial communication protocol widely used in the field of industrial automation, which has the advantages of noise suppression and high signal quality. ER-TS-3160VO is a linear inclination sensor with an accuracy of 0.01°, its cable standard length is 1.5m, and it can output RS232 at the same time, RS485 can be customized, the measurement range can reach 0~±180°, and the impact vibration resistance is strong.

The main advantage of the wired tilt meters is that the signal stability is high, and the signal quality is not easy to be disturbed because of the wired transmission mode. In addition, wired sensors have a long service life, lower maintenance costs, and a lower failure rate. However, this sensor also has some disadvantages, such as the need to lay cables, high requirements for the field environment, may exist in some application scenarios wiring difficulties. 

2. Advantages&disadvantages of wireless tilt sensor

Wireless tilt meters have become more and more popular in recent years, and common wireless inclination sensors include NB-IoT wireless inclination sensors and LORO wireless inclination sensors. These sensors transmit tilt signals via wireless communication technology without cable connections, making them highly flexible.

The main advantages of wireless tilt sensors are their flexibility and convenience. Since no wiring is required, the sensor can be easily installed anywhere it is needed, without considering the laying of cables. In addition, wireless sensors also have the advantages of high mobility, easy expansion and maintenance. However, wireless sensors also have some disadvantages, such as signal quality may be affected by radio interference, and signal stability and reliability may not be as good as wired sensors. ER-TS-12200-Modbus is a high-precision tilt sensor using Bluetooth and ZigBee wireless transmission technology of the internet of things, eliminating the complicated wiring and noise interference caused by long cable transmission, using lithium battery power supply, good long-term stability, zero drift, can automatically enter low-power sleep mode, get rid of the dependence on the use of environment.

Generally speaking, the mass of the building structure is huge, and the rate of change of inclination is relatively small, and there is a development process. The sampling frequency of conventional structural health monitoring is not high, and once a day can meet the requirements. In this case, the choice of the wireless inclination sensors with its own battery is the most appropriate, and the installation is very convenient.

3. How to choose the most suitable tilt sensor for you according to the transmission mode

When choosing a tilt meter, you need to consider the following factors:

(1) Application scenarios: Different application scenarios have different requirements for sensors. For example, in some scenarios where long-term stability measurements are required, wired sensors may be preferred; Some use cases, such as house monitoring, basically have 220V mains power in the field, and low cost wired tilt sensors can be used. Of course, for monitoring scenarios with high acquisition frequency requirements, choosing a wired inclination sensor is a wise choice. In scenarios that require flexible deployment, easy scaling and maintenance, wireless sensors may be more suitable.

(2) Signal quality: For some application scenarios that require high-precision measurement, such as precision equipment monitoring or large-scale structure monitoring, it is necessary to choose a wired sensor with higher signal quality. For some application scenarios with low precision requirements, such as logistics and transportation, agricultural monitoring, etc., wireless sensors may be enough to meet the needs. 

(3) Cost and maintenance: For some application scenarios that require a large number of sensors to be deployed, such as large-scale facility monitoring or logistics tracking, the deployment and maintenance cost of wireless sensors may be lower. For some cost-sensitive scenarios, such as small device monitoring or small structure monitoring, the cost of wired sensors may be lower.

(4) Durability and reliability: For some scenarios that require long-term continuous operation, such as equipment monitoring and fault warning systems in petrochemical, electric power and other fields, it is necessary to choose wired sensors with higher durability and reliability. For some scenarios that require portable and temporary use, such as construction sites, agricultural monitoring, etc., wireless sensors will be more suitable. 

In short, when choosing an inclination sensor, it is necessary to choose according to actual needs and specific scenarios. Both wired and wireless sensors have their own advantages and scope of application. Only by fully understanding the characteristics and application scenarios of various sensors can we make the most appropriate choice.

Application of IMU in UAV Flight Control System


High Performance Navigation MEMS IMU

Nowadays, with the development of chip, artificial intelligence and big data technology, UAV has begun the trend of intelligence, terminal and clustering. A large number of professional talents in automation, mechanical electronics, information engineering and microelectronics have been invested in UAV research and development. In a few years, UAVs have flown from military applications far away from people’s vision to ordinary people’s homes. It is undeniable that the development of flight control technology is the biggest driver of UAV changes in this decade.

Flight control is the abbreviation of flight control system, which can be regarded as the brain of aircraft. The flight control system is mainly used for flight attitude control and navigation. For flight control, it is necessary to know the current status of the aircraft, such as three-dimensional position, three-dimensional velocity, three-dimensional acceleration, three-axis angle and three-axis angular velocity. There are 15 states in total. The current flight control system uses an IMU, also known as inertial measurement unit, which is composed of three-axis gyroscope, three-axis accelerometer, three-axis geomagnetic sensor and barometer. So what is a three-axis gyroscope, a three-axis accelerometer, a three-axis geomagnetic sensor, and a barometer? What role do they play in the aircraft? What are the three axes?

The three axes of the three-axis gyroscope, three-axis accelerometer and three-axis geomagnetic sensor refer to the left and right of the aircraft, and the vertical up and down in the front and back directions, which are generally represented by XYZ. The left and right directions in the aircraft are called roll, the front and rear directions in the aircraft are called pitch, and the vertical direction is the Z axis. It is difficult for a gyroscope to stand on the ground when it does not rotate. Only when it rotates, it will stand on the ground. This is the gyro effect. According to the gyro effect, smart people invented a gyroscope. The earliest gyroscope was a high-speed rotating gyroscope, which was fixed in a frame through three flexible axes. No matter how the outer frame rotates, the high-speed rotating gyroscope in the middle always maintains a posture. The data such as the degree of rotation of the external frame can be calculated through the sensors on the three axes.

Because of its high cost and complex mechanical structure, it is now replaced by the electronic gyroscope. The advantages of the electronic gyroscope are low cost, small size and light weight, only a few grams, and its stability and accuracy are higher than those of the mechanical gyroscope. Speaking of this, you will understand the role of gyroscope in flight control. It is used to measure the inclination of the three XYZ axes.

So what does the three-axis accelerometer do? It was just said that the three-axis gyroscope is the three axes of XYZ. Now it goes without saying that the three-axis accelerometer is also the three axes of XYZ. When we start driving, we will feel a thrust behind us. This thrust is acceleration. Acceleration is the ratio of speed change to the time of occurrence of this change. It is a physical quantity describing the speed of object change. Every second power of meter. For example, when a car is stopped, its acceleration is 0. After starting, it takes 10 seconds from 0 meters per second to 10 meters per second. This is the acceleration of the car, If the vehicle travels at a speed of 10 meters per second, its acceleration is 0. Similarly, if it decelerates for 10 seconds, from 10 meters per second to 5 meters per second, its acceleration is negative. The three-axis accelerometer is used to measure the acceleration of the three axes of the aircraft XYZ.

Our daily travel is based on landmarks or memories to find our own direction. The geomagnetic sensor is a geomagnetic sensor, which is an electronic compass. It can let the aircraft know its flight direction, nose direction, and find the position of the mission and home. The barometer is used to measure the atmospheric pressure at the current position. It is known that the higher the altitude, the lower the pressure. This is why people have plateau reactions after arriving at the plateau. The barometer obtains the current altitude by measuring the pressure at different positions and calculating the pressure difference. This is the whole IMU inertial measurement unit. It plays a role in the aircraft to sense the change of the aircraft attitude, such as whether the aircraft is currently leaning forward or left and right, What is the role of the most basic attitude data, such as nose orientation and altitude, in flight control?

The most basic function of flight control is to control the balance of an aircraft when flying in the air, which is measured by IMU, sense the current inclination data of the aircraft and compile it into an electronic signal through the compiler. The signal is transmitted to the microcontroller inside the flight control through the new time of the signal. The microcontroller is responsible for the calculation. According to the current data of the aircraft, it calculates a compensation direction and angle, and then compiles the compensation data into an electronic signal, It is transmitted to the steering gear or motor. The motor or steering gear is executing the command to complete the compensation action. Then the sensor senses that the aircraft is stable, and sends the real-time data to the microcontroller again. The microcontroller will stop the compensation signal, which forms a cycle. Most flight controls are basically 10HZ internal cycles, that is, 10 refreshes per second.

This is the most basic function application of IMU in the flight control system. Without this function, once an angle is tilted, the aircraft will quickly lose balance and cause a crash.

Ericco’s MEMS IMU ER-MIMU-03 and ER-MIMU-04ER-MIMU-07 and ER-MIMU-08 have built-in high-precision advanced MEMS gyroscopes and high-performance accelerometers, which can measure linear acceleration and angular velocity of rotation from three directions, and obtain carrier attitude, velocity and displacement information through analysis. They are specially designed for high-performance applications of inertial navigation equipment such as UAV flight control. Provides excellent stability in the temperature range of – 45° C to 80° C. The advanced gyro sensor design suppresses the linear acceleration effect of shock and vibration, enabling ER-MIMU-04, ER-MIMU-07 and ER-MIMU-08 to operate in harsh environments.

In addition to the application of ERICCO’s MEMS products in UAVs, its popularity in oil drilling, mining and other application markets is also growing. MEMS technology is developing into a huge industry. Just like the great changes brought to mankind by the microelectronics industry and computer industry in the past 20 years, MEMS has also bred a profound technological change, which has had a new round of impact on human society.


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website:https://www.ericcointernational.com/inertial-measurement-units

Email: info@ericcointernational.com

WhatsApp: +8613992884879


Friday, December 29, 2023

Function and Test Analysis of Tilt Sensor Detection System



 At present, tilt sensors are widely used in construction machinery, road machinery, port machinery, lifting machinery and other construction machinery fields, which can realize real-time monitoring and control of angle-related state and attitude in the operation process of construction machinery. However, the inclinometer sensor often has defects such as nonlinear error and temperature drift error in practical application, so that the accuracy is easily affected and the measurement error is too large, which can not meet the requirements of practical application of construction machinery equipment. In addition, in the mass production process of the tilt gauge, it is easy to have the acceleration sensor installed tilt, so that the measurement angle is offset. Therefore, in order to improve the measurement accuracy of the inclinometer sensor, the product needs to be calibrated, temperature drift compensation and accuracy detection before leaving the factory to ensure that the product meets the factory standard.

1.Inclination sensordetection system

The high-precision inclinometer sensor detection system CAN intelligently control the temperature change of the thermostat, the position rotation of the servo motor and the CAN communication control with the tilt gauge. The test data can be displayed and controlled in real time through the interface designed by Labview software. The angle sensor can automate 0° angle calibration, temperature scale aging, angle linear calibration and angle error detection.

2.Inclinometer sensordetection system function

2.1 0° angle calibration function

The tilt measurement sensor detection system uses smooth marble as the cornerstone, which is not easy to shake or deform, and the plane is adjusted to the standard 0° plane by the measuring instrument. When the tilt gauge is located at 0° water level, the system controller SYMC sends 0° calibration instructions to correct the original 0° data.

2.2 Temperature bleaching aging function

The purpose of temperature drift aging test is to solve the problem that the performance of tilt sensor components is unstable with temperature changes. The specific reason is that the output of tilt sensor and speed sensor is PWM signal, and the waveform is shown in Figure 1.

Figure 1 PMW signal of acceleration sensor

The formula for calculating the output acceleration of the inclination sensor is a = (T1 /T2-0g output)/sensitivity

The output angle of tilt gauge is calculated by θ=sin-1 (a).

In the formula, 0g output and sensitivity are constants in theory, but in fact, they will change due to temperature changes in component performance. To realize temperature drift compensation correction for 0g output and sensitivity values of the tilt measurement sensor, the detection system needs to sample at least 3 typical temperature points (such as -30 ℃, 25 ℃, 60 ℃) under 0g output values and sensitivity values. The output values of the acceleration sensor at 0°, 90°, 180° and 270° were collected at each temperature point, and the output values of the acceleration sensor at other temperatures and positions were linearly corrected by piecewise linear compensation method, so as to calculate the 0g output and sensitivity values of the tilt gauge at different temperatures.

2.3 Angular linear calibration function

The inclinometer sensor adopts linear fitting linearization measures to make the input and output signals have a linear relationship. The specific algorithm adopts two-stage quantization method, such as: take 24° and 26°, and use a straight line connection to replace the original curve; 26 degrees and 28 degrees are also connected by a straight line. The piecewise linear fitting method is adopted for the whole 360°, so that the relationship between the measured data and the actual angle is close to linear relationship. In the algorithm, the more test angle points collected, the more the curve calculated by the algorithm approximates the linear relationship. The inclinometer sensor detection system can randomly select 120 angle sample points, start from 0° angle, every 3° interval, respectively, to carry out piecewise linear fitting of the tested inclination sensor, angle calibration, and maximize the nonlinear error of the inclination sensor.

2.4 Angle detection function

The angle detection system can compare the angle value measured by the inclination sensor with the corresponding angle value detected by the encoder in the detection system, so as to calculate the measurement error of each angle position of the tilt gauge. angle detection selects 60 test sample points, and the selected angle is between the selected point of calibration angle, so as to effectively detect the accuracy of linear fitting algorithm of tilt measurement sensor. The angle resolution of the inclinometer sensor product is ±0.1°, and the accuracy of the angle encoder selected by the detection system is ±0.003°, which can make the detection error resolution reach the thousandth grade, effectively ensuring the accuracy of the system angle detection.

3.Check system test requirements

The requirements of the high-precision inclination sensor detection system in the test: ① The ambient temperature in the thermostatic box should be constant, and the change is less than 0.5 ℃; ② Ensure that the positioning of the structure shaft is consistent with the position of the sensor on the turntable, and the deviation of the angle position of 0°, 90°, 180°, 270° is less than 0.1°; ③ Ensure that the turntable will not shake when rotating, and the sensor can be firmly installed on the turntable; ④ Ensure that the support components can be adjusted in height and match the size of the thermostat; The whole device should have sufficient stiffness and will not be deformed in high and low temperature environments.

4.Check the system test results

The high precision tilt sensor detection system can test 96 board tilt sensors at a time, and the entire test cycle is 6 hours. After the 0° calibration is completed, the system conducts temperature drift aging test. Figure 2 shows the temperature drift effect data of the single-board tilt sensor at 180.5° from -30 ℃ to 80 ℃. It can be seen that the temperature drift compensation front and rear tilt sensor has obvious temperature drift performance effects.

Figure 2 Data Curve of Temperature Coefficient

After the temperature bleaching, the system calibrates 120 test angles of the inclination sensor, and the angular resolution of the inclination sensor is ±0.1°. After the calibration of the inclinometer sensor is correct, the detection system randomly selects 60 angles within 360° (which do not coincide with the angle selected by the calibration), and calculates the measurement angle of the tilt measurement sensor and the feedback angle error of the system encoder. The angle error curve formed by the deviation between the measurement angle of the inclination sensor and the feedback angle of the system encoder is shown in Figure 3.

Figure 3 Error curve of angles

After the test is completed, it can be identified from the figure that the angle error of the white curve is greater than -0.3°, which is a unqualified product and needs to be returned to the factory for processing.

Conclusion: The measurement accuracy of tilt sensor can be greatly improved by calibrating, temperature drift compensation and accuracy detection. Ericco’s ER-TS-3160VO (accuracy 0.01°) and ER-TS-12200-Modbus (0.001°) have been calibrated at 0° angle, temperature drift aging function test, angle linear calibration and angle detection before leaving the factory, so their accuracy is not easily affected, resulting in excessive measurement errors.

The application of high precision inclination sensor detection system realizes intelligent testing instead of manual testing. Production practice has proved that the test cycle of the tilt gauge is reduced from the original 9 h to 6 h, and the unmanned test can still be carried out at night, to achieve two batches of test a day, and the number of test pieces per cycle is increased from the original 60 pieces to 96 pieces, which greatly saves labor costs and improves production efficiency and product quality.

Calibration Method of Accelerometer

 Accelerometer is a kind of equipment used to measure the acceleration of objects, in order to ensure the accuracy of the data in the process of vibration and shock test and measurement, according to the frequency of use and the use of environmental conditions to determine the calibration cycle, usually half a year or one year. In some critical tests or costly destructive tests, calibration is recommended before each use. This article will introduce the calibration method and use skills of accelerometers.

1.Calibration method

The calibration of the accelerometer is the key to ensure the accuracy of its measurement results. Here are some common calibration methods:

1.1 Static Calibration

Static calibration is a calibration performed in a stationary state. Place the accelerometer on a horizontal table and record its output value. Its zero drift and sensitivity can be determined by comparing it with known gravitational acceleration values.

1.2 Dynamic Calibration

Dynamic calibration is carried out when the object is moving in a straight line at uniform speed. Fix the meter on the object and record its output value during movement. The deviation can be determined by calculating the difference between its output value and the expected acceleration during movement.

1.3 Comparison Calibration

Comparative calibration is the calibration of an accelerometer by comparing it with a reference addition known to be of high accuracy. Place both of them on the same object, perform the same motion, and record their output value. By comparing the difference between the two, the error to be calibrated can be determined.

2.Using ways

Reasonable using ways can improve the measurement and analysis of the accelerometer, the following are some commonly used techniques.

2.1 Fixed Position

In the acceleration measurement, the accelerometers should be fixed on the measured object as far as possible, and ensure that its position is stable to avoid interference with the measurement result due to movement or vibration.

2.2 Increasing the sampling rate

The resolution and sensitivity of the accelerometer can be improved by increasing the sampling rate appropriately. When measuring rapid acceleration and deceleration, a higher sampling rate allows instantaneous changes to be more accurately captured.

2.3 Filter Processing

The output signal may contain noise or high-frequency vibration components, which can be filtered to reduce noise and extract useful signals. The commonly used filtering methods include low-pass filtering and high-pass filtering.

3.Calibration precautions

3.1 Installing of the Sensor

Different installation methods will significantly affect the resonant frequency of the sensor, that is, the high-frequency response of the sensor. The following figure illustrates the effect of the installation method on the resonant frequency. Screw installation is preferred, followed by hot melt adhesive or quick-drying adhesive, then double-sided adhesive and so on.

3.2 Selection of sensor cable

Calibrate the sensor cable as far as possible to choose a relatively soft cable, such as silicone or PVC cable, which can reduce the impact of the cable on the sensor, including the shaking table moving core. During the actual test, it is recommended that the cable and sensor be fixed on the same structure. Due to the limited mounting surface during the sensor calibration process, it is recommended to use a flexible cable connection.

3.3 Calibration of X axis of three-axis sensor

The X axis of most three-axis sensors is inverted, so the frequency response of the sensor X axis is usually narrower than the frequency response of the Y and Z axes. Moreover, when testing the X-axis, the top line is out, and attention needs to be paid to the fixing of the cable.

In summary:

Through the above content, you can understand the calibration method of the accelerometer, the use of skills and precautions. Ericco’s ER-QA-03A and ER-QA-01A can be calibrated using the above methods to ensure their accuracy and reliability, but also to improve the accuracy of the test and analysis.

The full text link:https://www.ericcointernational.com/application/calibration-method-of-accelerometer.html

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Thursday, December 28, 2023

How the Inertial Measurement Unit Works?

 

How the Inertial Measurement Unit Works

Inertial Measurement Unit (IMU) A device used to measure speed, direction, and gravity. Early on, IMU consisted of two sensors, accelerometer and gyroscope. Accelerometers measure inertial acceleration, while gyroscopes measure angular rotation. These sensors have three degrees of freedom and can measure from three axes. Later, IMUs introduced magnetometers, which measured the direction of magnetic forces and helped improve gyroscope readings. IMU applications include various fields such as tracking, navigation and robotics. IMU helps us determine the instantaneous position, speed, orientation and direction of movement of an object or vehicle.

1.IMU type

1.1 IMU with two sensors — This type of IMU consists of accelerometer and gyroscope. Each sensor has two or three degrees of freedom defined for the x, y, and z axes, and two sensors combined add four or six degrees of freedom. The acceleration values measured by the accelerometer and the angular velocity measured by the gyroscope are recorded separately, while the angles measured using both sensors are calibrated to obtain accurate data. If such an IMU is present around the sensor, it will not be disturbed by external magnetic fields. Its accuracy suffers due to sensor noise and gyroscope drift issues. ·

1.2 IMU with three sensors — This type of IMU consists of accelerometer, gyroscope and magnetometer. All sensors have 3 degrees of freedom, corresponding to 3 different axes, for a total of 9 degrees of freedom. The magnetometer measures yaw rotation (that is, rotation about the vertical axis) and is calibrated against gyroscope data to account for drift. It is mainly used for dynamic orientation calculation when the drift error is small. If the IMU is present inside a magnetic field, its measurements may be affected because it uses a magnetometer.

2.IMU working guidelines

2.1 Accelerometer

There are many types of accelerometers, and mechanical accelerometers and piezoelectric accelerometers are commonly used in IMU technology. Mechanical accelerometers consist of a spring-suspended mass. Measures the displacement of the mass, providing a signal proportional to the force F acting on the mass along the input axis. Calculate the acceleration acting on the device using Newton’s second law, F = ma.

Piezoelectric accelerometers work on the principle of the piezoelectric effect, which is the ability of a material to become electrically polarized when subjected to mechanical stress. PE accelerometers use a PE element with a load mass (seismic mass) attached to form a 1 DOF mass spring system. The system makes one for each direction (left and right, front and back, and up and down in a three-axis accelerometer). Transient changes in stress on the PE element produce a charge at the output terminals of the accelerometer that is proportional to the applied acceleration.

2.2 Gyroscope

Likewise, gyroscopes are also available in different types, but MEMS based gyroscopes (MEMS) are implemented in IMUs. MEMS (microelectromechanical systems) is a technology that uses micromachining technology to create miniaturized mechanical and electrical devices and structures, with sizes ranging from less than one micron to several millimeters.

Gyroscopes use the Coriolis effect, which states that in a reference frame rotating at angular velocity w, a mass m moving with velocity v experiences a force Fc = −2m(w× v). MEMS gyroscopes contain vibrating elements such as vibrating wheels and tuning fork gyroscopes to measure the Coriolis effect. The simplest geometry consists of a single mass driven at a specific speed to vibrate along the drive axis, and when an external angular rotation (secondary rotation) is applied, secondary vibrations are induced along the vertical axis due to the Coriolis force. The angular velocity can be calculated by measuring this secondary rotation.

2.3 Magnetometer

About 90% of magnetometers work using the Hall effect. The principle of the Hall effect states that when a current-carrying conductor is placed in a magnetic field, a voltage will be generated perpendicular to the direction of the magnetic field and the direction of the current.

When a constant current flows through a piece of semiconductor material, in the absence of a magnetic field, there is no potential difference at the output. However, when a vertical magnetic field is present, the direction of the current flow is disturbed, creating a potential difference between the output terminals. This voltage is called Hall voltage. Keeping the input current constant, measure the magnetic field strength proportional to the Hall voltage.

3.How to calibrate IMU during operation

IMUs combine input data from multiple different sensors to accurately measure motion. To obtain accurate values, the sensor must be calibrated rather than using raw data. Calibration parameters can be stored in the IMU’s memory and automatically reflected in the result data. Calibration can also be accomplished by using a magnetometer, which reduces directional drift (errors that accumulate over time). Some devices use proprietary sensor fusion algorithms to combine magnetometer and gyroscope data to determine the device’s orientation relative to a global reference frame. Sensor fusion is the process of using signals from two or more types of sensors to update or maintain the state of a system (direction, velocity, and displacement). Sensor fusion algorithms maintain this state using IMU accelerometer and gyroscope signals as well as signals from other sensors (such as magnetometers) or sensor systems. The most popular technique for performing sensor fusion is the Kalman filter.

The Kalman filter is an optimization algorithm for estimating the state of systems with noise and uncertainty. This filter accepts noisy imprecise measurements and it is able to estimate the current state and even predict future states with good accuracy. The Kalman filter uses all sensor axis contributions within the IMU to estimate the direction angle, thereby minimizing drift.

4 .Conclusion

In application fields, IMU is used in various tracking systems such as unmanned navigation systems, vibration control, and measurement. In unmanned navigation systems (drone, aircraft), the navigation-level IMU developed by ERICCO can independently seek north, such as ER-MIMU01 and ER-MIMU-05. Their advantages are: light weight, small size, low Cost, high performance, due to these characteristics they can be mass produced, and equipped with X, Y, Z three-axis precision gyroscope, X, Y, Z three-axis accelerometer, high resolution, can output X, Y, The original hexadecimal complement data of Z three-axis gyroscope and accelerometer (including gyroscope hexadecimal complement value temperature, angle, accelerometer hexadecimal temperature, acceleration hexadecimal complement value); It can also output floating-point dimensionless values of gyroscopes and accelerometers processed by low-level calculations. The angular velocity random walk in the gyroscope is less than 0.005, the paranoid stability is less than 0.01, and the accuracy is higher than that of other inertial navigation companies.

If you want to learn about or purchase an IMU, please contact our relevant personnel.

contact me:

website:https://www.ericcointernational.com/inertial-measurement-units

Email: info@ericcointernational.com
WhatsApp: +8613992884879

High-precision IMU is coming to help in the fields of land, sea and air

  High-precision IMU is now widely used in many fields of sea, land and air. It can provide real-time and accurate information on the carrie...