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Brand Name : Kacise
Model Number : KSIMU01D
Place of Origin : China (Mainland)
Certification : certificate of explosion-proof, CE
MOQ : 1pcs
Packaging Details : each unit has individual box and all boxes are packed in standard packages or customers requests available
Delivery Time : 5-8 working days
Payment Terms : T/T, Western Union, MoneyGram
Supply Ability : 1000 Pieces per Week
Weight : ≤100g
Heading : ±180deg
Supply voltage : 5DC±5%V
MTBF : 10Kh MTBF
Power consumption : ≤0.5W @5V DC
Pitch : ±90deg
Nonlinearity : ≤0.1%
Operating temperature : -40℃~+70℃
The KSIMU01D is a superior low-cost inertial measurement device that is designed for navigation, control and dynamic measurement. The product's sealed design can ensure exceptional angular velocity and acceleration measurements for a moving carrier in difficult situations.
This series comes with many features that include low power consumption, wide operating temperature range, wide bandwidth, small size, and fast startup. These attributes make the KSIMU01D ideal for many applications including automotive electronics, aircraft guidance and control, attitude reference system, platform stabilization, robot, antenna stabilization and other systems.
The KSIMU01D is built with precision and can accurately measure the motion of a device with effectiveness even in harsh environments.
● Low cost, small size
● Operating temperature -40°C ~ +85°C
● Wide power input, digital output
● Strong structure and reliability
Parameter | KSIMU01D | |
Power supply parameter | ||
Supply voltage | 5DC±5%V | |
Power consumption | ≤0.5W @5V DC | |
Product performance | ||
Size | Ф39.5×22mm Ф39.5×28.5mm 26.5×26.5×23.5mm | |
Attitude | Weight | ≤100g |
Heading | ±180deg | |
Roll | ±180deg | |
Pitch | ±90deg | |
Pitch Accuracy | 0.3deg | |
Gyroscope | Full Scale | ±200(optional)deg/s |
bias | ≤±0.1deg/s | |
bias stability | ≤10deg/s | |
bias repeatability | ≤0.3deg/s | |
Nonlinearity | ≤0.1% | |
Accelerometer | Full Scale | ≤0.3°/h |
bias | ≥500Hz | |
bias stability | 170g±10g | |
Nonlinearity | ≤0.1% | |
MTBF | 10Kh MTBF | |
Output Interface | Digital RS422 | |
Update rate(user settable) | 200 Hz@460800 | |
Environment | ||
Operating temperature | -40℃~+70℃ | |
Storage temperature | -55℃~+85℃ | |
Vibration | 6 g @ 20~2000 Hz | |
Shock | 8000 g , 0.5 ms, 1/2 Sine |
Automotive electronics refer to the various electronic systems and devices found in modern automobiles. These systems provide functions such as controlling engine performance, improving safety, and enhancing entertainment and communication. Automotive electronics play a vital role in enhancing the overall functionality and user experience of modern automobiles, and many new advancements are being made in this field on an ongoing basis.
Aircraft guidance and control refers to the various electronic systems and devices used to guide and control aircraft. These systems include autopilots, flight management systems, and navigation equipment. They are essential for ensuring safe and efficient flight operations, and many advancements have been made in this field in recent years, such as the development of GPS-guided navigation systems.
An attitude reference system is a type of electronic system used to determine the orientation of an aircraft or spacecraft in flight. These systems use various sensors and devices to measure factors such as altitude, heading, and pitch, and can provide pilots and operators with important information about the aircraft's position and trajectory. Attitude reference systems are critical for safe and efficient flight operations.
Platform stabilization refers to the use of electronic systems and devices to stabilize platforms such as cameras, radar systems, and telescopes. These systems can compensate for movements caused by factors such as wind, vibrations, and changes in altitude, and help to maintain a steady alignment and focus. Platform stabilization is essential for obtaining accurate and reliable data from many types of equipment.
Robot and antenna stabilization refer to the use of electronic systems and devices to stabilize robots and antennas. These systems can help to compensate for movements caused by external factors such as wind, motion, and vibrations, and can help to maintain precise positioning and alignment. This is essential for many types of applications, such as robotic manufacturing and satellite communication.
Our Electronic Gyroscope Sensor is designed with precision to provide reliable performance for your applications. Our support includes detailed product documentation, an extensive online knowledge base, and troubleshooting guides to help you resolve any issues you may encounter.
We are committed to the satisfaction of our customers and strive to provide exceptional after-sales support. Should you have any feedback or suggestions, we welcome your input as it helps us to continuously improve our products and services.
Product Packaging:
The Electronic Gyroscope Sensor comes securely packaged in an anti-static bag to prevent any electrostatic discharge during handling. The bag is then placed in a custom-fit foam insert that snugly holds the sensor in place, ensuring maximum protection against physical shocks and vibrations. This foam is encased in a sturdy cardboard box which is sealed and labeled with the product information and handling instructions. The packaging has been designed to be compact while offering the best possible protection for the sensitive electronics inside.
Shipping:
Once the Electronic Gyroscope Sensor is packaged, it is ready for shipping. The boxed product is placed in a secondary, larger cardboard box with additional cushioning material to fill any void space, minimizing movement during transit. Fragile stickers are applied to the outer box to alert couriers that the contents require careful handling. The package is then sealed with heavy-duty packing tape and dispatched using a reliable shipping service that provides a tracking number. Customers will receive their tracking information via email to monitor their package's journey until delivery.
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Inertial Measurement Unit Nonlinearity ≤0.1% Heading ±180deg Strong Structure And Reliability Images |