Low-cost GNSS/INS integrated navigation system, widely used in unmanned aircraft, vehicle navigation, surface vessel, ship and so on.
GINS200 Low Cost GNSS/INS Integrated Navigation System adopts MEMS inertial components and integrates GPS/BD satellite navigation system. GINS200 has special SkyMEMS new integrated navigation fusion algorithm, which can realize high sensitivity tracking and accurate positioning in harsh environment.
The system enjoys small size, light weight, low cost, and low power consumption, fast start-up, and high reliability. It has been widely used in unmanned aircraft, vehicle navigation, the surface craft, ship and so on.
|Heading Accuracy||L1/B1 single point||0.5°(rms)|
|Attitude||Roll/Pitch accuracy||<0.3° degree (RMS)|
|Velocity||Velocity accuracy||<0.15m / s (RMS)|
|Position||Position accuracy||<5m (RMS)|
|Gyroscope||Range||±300 °/s (ODM supported)|
|Bias stability||≤8°/h (normal temperature, allan variance)|
|Accelerometer||Range||±2g ~ ±20g|
|Random walk||≤20µg (normal temperature, allan variance)|
|Receiver||Working mode||BD2 B1/GPS L1|
|Electrical Specs||Power supply||9~36VDC|
|Electrical interface||RS422 / RS232 / TTL|
|Data refreshing rate||IMU: 100~400Hz; attitude: 100Hz|
|Environment Conditions||Working temperature||-40~+80°C|
|Shock||9g/11 ms, 1000g/1ms|
|Physical Characteristics||Size||50 × 51.5× 30mm|
GINS200 GNSS/INS Integrated Navigation System is a high performance integrated navigation system, it enjoys high reliability, high stability in dynamic applications, which has been widely used in the following fields:
– Unmanned Aerial Vehicle
– Ship and Boat
– Vehicle Navigation
– Surface Craft
– Platform Stabilization
GINS200 GNSS/INS Integrated Navigation System widely used in UAV Navigation
UAV is unmanned aerial vehicle, commonly known as a drone, is an aircraft without a human pilot aboard. The flight of UAVs may operate with various degrees of autonomy: either under remote control by a human operator or autonomously by onboard computers.
The GINS200 GNSS-based Integrated Navigation System provides exceptional performance for autonomous control of aerial based platforms. With an update rate of 100~400 Hz, high bandwidth, low-latency position, and attitude measurements can be directly connected to the necessary control loops. The GINS200 calibration procedures ensure a high accuracy pitch and roll solution relative to the horizon while the onboard barometric pressure sensors provide autonomous aircraft with a more precise ability to hold altitude. The high sample rate on all the individual sensors reduce impact from unwanted vibration.
GINS200 GNSS/INS Integrated Navigation System is low cost high performance integrated navigation system, which has been widely used in unmanned UAV Navigation.
GINS200 GNSS/INS Integrated Navigation System widely used in unmanned vehicle
An Attitude and Heading Reference System, also called AHRS, it contains an IMU (3 gyroscopes, 3 accelerometers, and 3 magnetometers) and adds a central processing unit (CPU) that embeds the Extended Kalman Filter. This allows to calculate highly reliable attitude and heading relative to magnetic north, in addition to roll, pitch, and yaw.
AHRS200 AHRS module provides reliable performance with good accuracy in dynamic environment, it has been widely used in unmanned vehicles by the Chinese leading companies, now more than thousands of AHRS200 AHRS modules are used in the unamend vehicles.
GINS200 GNSS/INS Integrated Navigation System widely used in ship and boat
Maritime VSAT satellite communication require stabilized antennas that remain pointed at the satellite in order to ensure continuous data transmittal. Regulations require that pointing accuracy remain better than 0.5 degrees to maintain active transmission. This requirement demands highly accurate, precise and low latency attitude and angular rate measurements. The dynamic motion common to rough sea conditions makes this a difficult task for most industrial grade MEMS-based inertial navigation systems.
The GINS200 Integrated Navigation System for Ships assisted inertial navigation algorithm is capable of compensating for dynamic acceleration induced from the motion of the vessel while maintaining accurate orientation measurements. With a full filter state update rate of 400 Hz, the GINS200 provides extremely fast attitude and angular rate measurements, critical for closed-loop control.
GINS200 GNSS/INS Integrated Navigation System is low cost high performance integrated navigation system, which has been widely used in ship and boat.
Why Selecting GINS200 GNSS/INS Integrated Navigation System?
GINS200 GNSS/INS Integrated Navigation System is designed and produced by SkyMEMS, it enjoys high performance and accuracy, and high reliability. It is a popular GNSS/INS system in the market, which has the main following advantages:
GINS200 GNSS/INS Integrated Navigation System is a high-performance integrated navigation system, which enjoys excellent technical advantages:
– Low-Cost MEMS Inertial System with GPS/BD2
Dual-mode Satellite Navigation System
– High Accuracy: Yaw: 0.5° (rms), Attitude: 0.3° (rms),
Velocity <0.15m/s, Position < 5m (rms)
– Multiple Interface: RS422 / RS232 / TTL
– High Reliability, Strong Vibration Proof
– Small Size: 50 × 51.5× 30mm, <100grams
– Wide Operating Temperature: -40°C～+80°C
GINS200 GNSS/INS Integrated Navigation System adopts big brand components, advanced production craft, fully calibrated, advanced SkyMEMS algorithm, which assured that our products have real actual precise and perfect performance.
We have advanced product test team and measurement equipment, and we cherish the quality as the life of the company, all our products must pass the strictest quality control procedures, our unique 12-step quality control assures our products enjoy top level quality.
With strict cost control and massive production, we can provide the most competitive cost-effective prices, and we have abundant ODM service experience for customers around the world, that is why we can build up long term win-win cooperation with our customers.
We are continuously focusing on MEMS measurement & control technologies, and have developed the most advanced GNSS/INS Integrated Navigation System GINS200 . and GINS200 has been widely used in unmanned aerial vehicle, ship and boat, vehicle navigation, surface craft, civil plane, etc. and now more than 300 customers are using our GNSS/INS Integrated Navigation System around the world.
We have the world class production line to assure that the production procedures are scientific, precise, and normative, which also can assure our products to be fast delivered.
We have the professional technical support engineer team, which can provide 24-hour technical support and excellent after-sale service.
Serving customers with heart is the principle of SkyMEMS, Customer demand is the fundamental driving force of our development.
We treat our customers with heart, customers’ satisfaction is the direction and target of SkyMEMS. Through continuously technology innovation and service upgrading, we will realize win-win cooperation with customers.
Q: What is GNSS/INS Integrated Navigation System?
A: Global Navigation Satellite System (GNSS) receivers provide position coordinates and the velocity vector with data rates of 1 – 10 Hz. However, they require data from at least 4 GNSS satellites, which often is not the case e.g. within urban canyons of the big cities.
Navigation systems are based on accelerometers and gyroscopes, so called Inertial Navigation Systems (INS), provide position, velocity as well as attitude with data rates of typically 1 kHz. Thus, they are the primary sensors for the Guidance, Navigation and Control (GN&C) system of aircrafts, rockets and satellites. They work without any external aiding information. However due to the inherent bias errors of the inertial sensors an INS has an unbounded position error growth over time.
The fusion of both systems by means of a Kalman estimator uses the advantages of these complementary sensors, resulting in a smooth data stream of position, velocity, and attitude with high data rate, now with bounded errors. Additionally, such an Integrated Navigation System is able to calibrate the inertial sensor bias errors in flight. A tight coupling of the pseudoranges and deltaranges of the GNSS receiver with the INS data provides reliable position coordinates even if less than 4 GNSS satellites are visible. In a further step by a deep GNSS/INS integration, which couples the tracking loops of the GNSS receiver with the INS data, it is possible to track even those satellites, which are not visible for some period of time, which allows instantaneous recovery of lost satellite signals.
Q: How about the delivery time?
A: for our standard model, if we have them in stock, only need 2~3days to re-test before shipping, if it is out of stock, then need around 3 weeks to arrange the production and tests. For the ODM electronic product, if needing to modify the structure, it will need around 4~5 weeks to arrange the production and tests.
Q: How to arrange the payment?
A: about the payment, please pay to our company account, the beneficiary’s name: NANJING SKY MEMS TECHNOLOGY CO., LTD. And our email is only @skymems.com to contact with u formally. To notice this to avoid the loss.