𝗦𝘁𝗿𝘂𝗴𝗴𝗹𝗶𝗻𝗴 𝘁𝗼 𝗕𝗮𝗹𝗮𝗻𝗰𝗲 𝗗𝗿𝗼𝗻𝗲 𝗦𝘁𝗮𝗯𝗶𝗹𝗶𝘁𝘆 𝗮𝗻𝗱 𝗖𝗼𝘀𝘁? 𝗠𝗲𝗲𝘁 𝘁𝗵𝗶𝘀 𝗜𝗠𝗨!

 

check detail Did you know? For precise flight control, drones need real-time data on orientation, motion, and direction. The IMU is the backbone of this process, measuring acceleration, angular velocity, roll/pitch/yaw, and more.

𝗪𝗵𝘆 𝗢𝘂𝗿 𝗘𝗥-𝗠𝗜𝗠𝗨-𝗠𝟬𝟮 𝗦𝘁𝗮𝗻𝗱𝘀 𝗢𝘂𝘁:

𝗔𝗹𝗹-𝗶𝗻-𝗢𝗻𝗲 𝗜𝗻𝘁𝗲𝗴𝗿𝗮𝘁𝗶𝗼𝗻: Combines a 𝗴𝘆𝗿𝗼𝘀𝗰𝗼𝗽𝗲(±450º/s, 2º/h bias instability), 𝗮𝗰𝗰𝗲𝗹𝗲𝗿𝗼𝗺𝗲𝘁𝗲𝗿 (±16g, 24μg stability), 𝗺𝗮𝗴𝗻𝗲𝘁𝗼𝗺𝗲𝘁𝗲𝗿 (magnetic compass), and 𝗯𝗮𝗿𝗼𝗺𝗲𝘁𝗲𝗿 (altitude control).

𝗦𝘂𝗽𝗲𝗿𝗶𝗼𝗿 𝗣𝗲𝗿𝗳𝗼𝗿𝗺𝗮𝗻𝗰𝗲: Enables precise attitude calculation, speed/displacement tracking, and dynamic stabilization—even in challenging environments.

𝗨𝗹𝘁𝗿𝗮-𝗖𝗼𝗺𝗽𝗮𝗰𝘁 𝗗𝗲𝘀𝗶𝗴𝗻: Just 𝟭𝟰𝗺𝗺 𝘁𝗵𝗶𝗰𝗸 and 𝟱𝟬𝗴 𝘄𝗲𝗶𝗴𝗵𝘁 (47×44×14mm). Perfect for seamless integration into any drone.

𝗖𝗼𝘀𝘁-𝗘𝗳𝗳𝗲𝗰𝘁𝗶𝘃𝗲 𝗦𝗰𝗮𝗹𝗮𝗯𝗶𝗹𝗶𝘁𝘆: Mass-produced with stable quality, short lead times, and budget-friendly pricing. Ideal for high-volume users!

𝗞𝗲𝘆 𝗔𝗽𝗽𝗹𝗶𝗰𝗮𝘁𝗶𝗼𝗻𝘀:

Drone stabilization & control

Navigation and positioning

Altitude management

Field testing & measurement

check detail

✈️Flight safety secrets: The core role of high-precision IMUs in aviation

 

High-precision IMU plays an irreplaceable role in the aviation field. It provides key data support for the flight control system (FCS) by providing the acceleration and angular velocity of the carrier, and combining algorithms to solve attitude, speed and position information.

Take a high-precision IMU ER-MIMU-02Mini as an example for analysis.

In the flight control system, the data provided by IMU is the basis for the autopilot to achieve precise control. The autopilot continuously adjusts the flight parameters of the aircraft based on the data of IMU to ensure the stability and safety of the flight process.

Excellent precision performance

Gyroscope bias instability is 0.03deg/hr, and angle random walk is <0.01 °/√h; accelerometer bias repeatability is 100μg, and class II non-linearity coefficient is <100μg/g². 400Hz high-frequency data output, power consumption as low as 2W.

Such high-precision measurement capabilities can accurately measure the attitude changes of aircraft in aerial photogrammetry. Using the information provided by IMU, the captured images can be accurately geometrically corrected and positioned.

This makes the drawn maps more accurate and can meet the needs of high-precision geographic information in urban planning, land surveying, geological exploration and other fields.

In the aircraft's navigation system, the high-precision IMU cooperates with other navigation equipment to form a navigation system. When the GPS signal is interfered with or fails, this IMU can switch to the main navigation data source in a short time to ensure that the aircraft's navigation system continues to provide accurate position and attitude information.

Compact and lightweight design

Adopting modular design, the size is only 40*40*42 (mini version with shell)/27*26*34 (mini version without shell and baseboard), and the weight is 80g (mini version with shell)/ 40g (mini version without shell and baseboard).

This compact and lightweight design is crucial for the aviation field, which is extremely sensitive to weight and space. It can effectively reduce the load of equipment such as drones and aircraft, and improve flight performance and efficiency.

Powerful integration and compatibility

It can be customized by OEM, has good integration and compatibility, and can be easily integrated into various systems.

Simple operation can connect to the system and obtain IMU data. At the same time, by removing the baseboard shell, the size and weight of the IMU can be greatly reduced.

👉For more data sheet : https://lnkd.in/gMMrsg8N

❤you can also take a screenshot and send it directly to this email address to ask : ericco188@ericcointernational.com

 

       GNSS satellite refresh rate is low and the signal is easily blocked or interrupted, resulting in GNSS signal loss. The integrated navigation system of GNSS+INS can make up for these problems, and the high-precision INS can keep working in a short time when GNSS loses lock.

GNSS+INS combined navigation is widely used in large unmanned aerial vehicles, mobile mapping, geographic information collection, urban intelligent transportation and other applications due to its sustainable navigation, high precision and high autonomy.

Our integrated navigation ER-GNSS/MINS-01 has ultra-high precision at the surveying and mapping level. It can provide continuous and high-precision position, velocity and attitude (roll, pitch and yaw) information.

**Mapping-level high-precision navigation**

The integrated navigation information provided has a roll and pitch accuracy of up to 0.01° and post-processing of 0.004°. The heading can reach 0.05°, 0.01° after post-processing, and the speed accuracy can reach 0.03m/s.

Supports RTK positioning, can automatically identify RTCM, and enter RTK state.

In the case of RTK interruption for 30 seconds, the roll and pitch accuracy can be maintained at 0.01°, and the heading accuracy can be maintained at 0.01°. The position is maintained at 0.2m and the height is maintained at 0.08m.

**High-precision core components**

Built-in high-performance navigation-grade MEMS gyroscope and accelerometer, the gyroscope measurement range is ±200°/s, and the bias instability is <0.02°/h. The accelerometer measurement range is ±60g, and the bias instability (Allen curve) is <2ug.

**Full-band full-system**

The built-in dual-antenna positioning and orientation GNSS module supports all major global satellite navigation systems (GPS/BDS/GLONASS/Galileo/QZSS), and can perform high-precision and rapid positioning and orientation. At the same time, it is compatible with all frequency points, and can obtain the best positioning effect at any location in the world.

The built-in satellite receiver has strong anti-interference ability, can still provide accurate positioning in complex electromagnetic environments, and also supports a variety of communication interfaces.

**Small size and light weight**

The size is only 65×70×45.5mm, the weight is less than 300g, and the aluminum alloy shell is used to ensure reliability. And the operating temperature range can reach -40°C to 80°C, which is suitable for most working environments.

❗ For more information, please indicate in the “Ask for a Quote” box at the bottom of the page that you learned about this GNSS+INS integrated navigation from boggle.（https://www.ericcointernational.com/inertial-navigation-system/mems-inertial-navigation-system/mapping-level-ultra-precision-gnss-mems-ins.html）
👉 You can also take a screenshot and send it directly to this email address: ericco188@ericcointernational.com

From attitude to flight control, IMU protects drone flight in all aspects

 

IMU provides key flight data for drones, which can help drones achieve multiple functions such as attitude control, navigation, flight control, etc. The data provided is used by the flight control system to generate control instructions, make quick responses during flight, maintain stability, and achieve precise flight control.

Now we have an IMU ER-MIMU-03Mini, which is small in size, light in weight, and has low power consumption, which is very suitable for drones that pursue long-range and lightweight.

**Small size, easy to install**

The volume is 40*40*42 (with shell)/27*26*34 (without shell), and the weight is 120g (with shell)/80g (without shell). The compact and small design can be easily installed in the drone.

**High-precision sensor**

The built-in gyroscope has a measurement range of 400º/s, bias instability (1σ 25℃) <0.3 º/h, and angular velocity random walk <0.125°/√h. The accelerometer has a measurement range of 30g, bias stability (10s 1σ) <50ug, and bias repeatability is 100ug.

The measured data supports the flight control system to detect the attitude changes of the drone in real time. The data provided by the IMU, combined with other sensor data, helps determine the position and direction of the drone.

**OEM Customization Service**

This IMU adopts modular design, and we also provide OEM customization service.

The IMU can be connected to the user system and obtain data with simple operation, without using the 15-pin plug we provide. At the same time, by removing the bottom plate shell, the size and weight of our product can be greatly reduced.

In summary, IMU is an indispensable component of the UAV flight control system, ensuring that the UAV can fly stably and accurately perform flight missions.

If you are interested in this and would like to know its data sheet.
Check the details (please indicate in the email that the IMU you saw from Blogger)
：https://www.ericcointernational.com/inertial-measurement-units/mems-inertial-measurement-unit/high-precision-navigation-stable-control-mems-imu.html
You can also take a screenshot and send it directly to this email address: ericco188@ericcointernational.com

Drone construction must-see

 Multiple sensor integration, high cost performance, stable flight

With the rapid development of the drone industry, high performance and low cost have become the goals that manufacturers are competing for.

The sensors of drones are crucial to ensure the stability, accuracy and environmental adaptability of drones. IMU is an important sensor of drones, located in the core position, which can ensure the normal operation of device functions and navigation.

We have an IMU ER-MIMU-M02 that integrates accelerometers, gyroscopes, magnetic compasses and air pressure sensors. It has excellent performance and low cost, meeting user needs.

**Multiple sensor integration**

The gyroscope has a measurement range of ±450º/s and a bias instability of 2 º/h;

The accelerometer has a measurement range of 16g ​​and a bias instability of 24μg (Allen variance);

The gyroscope and accelerometer provide angular velocity and acceleration, which can be used to calculate the attitude, velocity, displacement and other information of the drone. It helps the flight control system to achieve precise control and maintain a stable attitude and balance in a dynamically changing environment.

The magnetometer has a measurement range of ±2.5Gauss; it can measure the strength and direction of the magnetic field and provide the direction of magnetic north.

The barometer has a pressure range of 450~1100mbar; by measuring the atmospheric pressure, the data provided can assist the drone in navigation and rise to the required height.

**Lightweight and thin design**

This IMU has a volume of 47×44×14mm, a thickness of only 14mm, and a weight of 50g. It is extremely light and thin and can be easily integrated into any device.

**High cost performance, mass production**

It can be produced in a short cycle, large batches, and large scale with stable quality, which is especially suitable for users with large demand and limited budget.

If you are interested in this and would like to know its data sheet.

For more information, please indicate in the “Ask for a Quote” box at the bottom of the page that you learned about this North Finder from Blogger.

：https://www.ericcointernational.com/inertial-measurement-units/mems-inertial-measurement-unit/er-imu-m02-inertial-measurement-unit.html

You can also take a screenshot and send it directly to this email address: ericco188@ericcointernational.com

The most cost-effective choice: full-frequency, full-system positioning and orientation

 

The GNSS integrated navigation system can make up for the shortcomings of GNSS when the signal is blocked or interrupted and the problem of low satellite refresh rate, aiming to improve the accuracy and reliability of navigation.

Our integrated navigation ER-GNSS/MINS-05 is the most cost-effective one. It has high reliability and reasonable price. It can provide continuous and high-precision position, heading, speed and attitude information.

**High-precision positioning and orientation**

The product has a highly reliable and low-cost MEMS gyroscope (measurement range is ±450°/s, bias instability <2°/h) and accelerometer (measurement range is ±16g, bias instability <25ug).

The integrated navigation information provided has a roll and pitch accuracy of up to 0.1° and post-processing of 0.03°. The heading can reach 0.1°, 0.05° after post-processing, and the speed accuracy can reach 0.03m/s.

RTK interruption for 30 seconds, the roll and pitch accuracy can be maintained at 0.03°, and the heading accuracy can be maintained at 0.06°.

**Full-band full-system**

The built-in dual-antenna positioning and directional GNSS module supports all major global satellite navigation systems and is compatible with multiple frequency points to ensure the best positioning results anywhere in the world.

Supports RTK positioning, automatically identifies RTCM, and enters RTK state.

**Strong anti-interference ability**

The built-in satellite receiver has strong anti-interference ability, can still provide accurate positioning in complex electromagnetic environments, and supports multiple communication interfaces.

**Small size and light weight**

The size is only 65×70×45.5mm, the weight is less than 240g, and the aluminum alloy shell ensures the reliability of the product.

The operating temperature range can reach -40°C to 80°C, and the low power consumption design of 5W is suitable for most working environments.

**Multi-field application**

It is suitable for large and medium-sized unmanned aerial vehicles, flight recorders, intelligent unmanned vehicles and roadbed positioning and orientation, etc.

If you are interested in this and would like to know its data sheet.

Please inbox me/PM or Connect with me

For more information, please indicate in the “Ask for a Quote” box at the bottom of the page that you learned about this North Finder from Blogger.: https://www.ericcointernational.com/inertial-navigation-system/mems-inertial-navigation-system/cost-efficient-gnss-aided-mems-ins.html

You can also take a screenshot and send it directly to this email address: ericco188@ericcointernational.com