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GPS Aided Inertial Navigation System GINS3000 1
GPS Aided Inertial Navigation System GINS3000 2
GPS Aided Inertial Navigation System GINS3000 3
GPS Aided Inertial Navigation System GINS3000 4

GINS3000 Airborne GPS Aided Inertial System

high-performance airborne GPS aided inertial system, widely used in unmanned aircraft, vehicle navigation, surface craft, ship, and so on.

  • High-Performance MEMS Inertial System with GPS/GLONASS Satellite Navigation System
  • High Accuracy: Yaw: 0.5° (1σ), Attitude: 0.23° (1σ), Velocity <0.05~0.1m/s, Position < 5m (L1/L2 single point), <8cm (RTK), Heave: <15cm (1σ)
  • RS422 Interface, 100Hz Data Output Rate
  • High Reliability, Strong Vibration Proof
  • Advanced SkyMEMS Data Fusion Algorithm
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Brief Introduction

GINS3000 high performance GNSS/INS integrated navigation system adopts MEMS inertial components and integrates GPS/GLONASS satellite navigation system, it adopts advanced SkyMEMS integrated navigation fusion algorithm, which can realize high sensitivity tracking and accurate positioning in harsh environment. GINS3000 can output 3D attitude (yaw, roll and pitch) angles as well as acceleration, angular rage, magnetic strength, temperature, and heave, etc.

The system enjoys small size, light weight, competitive price, and low power consumption, and high reliability. It has been widely used in unmanned aircraft, vehicle navigation, the surface craft, ship and so on.

Technical Specifications

Parameter　          ValueRemarks

Heading Accuracy L1/L2 single point 0.5° velocity > 20Km/h, 1σ
Magnetic 1° 1σ
Roll/Pitch Accuracy Real-Time with GNSS aiding <0.23° 1σ
without GNSS <0.5° 1σ
Velocity Accuracy Velocity accuracy 0.05~0.1m / s
Position Accuracy L1/L2 single point <5m
RTK <8cm
Heave Accuracy RTK <15cm Wave period 0 to 20s,1σ
Gyroscope Range 400°/s
Bias stability 20°/h
Non-linearity 0.001
Bandwidth 100Hz
Accelerometer Range 10g
Bias stability 0.5mg
Non-linearity 0.002
Bandwidth 100Hz
Magnetic sensor Range 2 Gauss
Noise 0.6 mGauss
Receiver Working mode GPS L1 C/A, L2C, L2P(Y); GLONASS L1/L2
Cold start 180s
Warm start 3-5s
Electrical Specs Power supply 6~12VDC
Current 250mA connect with external GNSS antenna
Power consumption ≤2W
Electrical interface RS422
Data refreshing rate 100Hz
Environment Conditions Working temperature  -40~+85°C
Storage temperature  -55~+85°C
Vibration 6.06g  (rms) 20Hz to 2KHz, random
Shock 7000g 1/2 sine 2ms
IP rating IP66
MTBF 5,000hours
Physical Characteristics Size 78*66*36mm
Weight 220grams
Data / power connector J30J-9ZK
GNSS antenna connector SMA Male

Typical Application

GINS3000 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

GINS3000 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.

GINS3000 GNSS/INS Integrated Navigation System is a low-cost high performance integrated navigation system, which has been widely used in unmanned UAV Navigation.

With its compact design, low power consumption, and high accuracy, the MADS1000 has become a popular choice for UAV navigation applications. It offers superior performance compared to traditional single-antenna systems, making it ideal for use in challenging environments where GPS signals may be weak or unavailable.

In addition to its exceptional performance, the MADS1000 multi-antenna attitude determination system has been designed with ease of integration in mind. It features simple interfaces and a small form factor, making it easy to integrate into existing systems or new designs. Furthermore, it comes with a user-friendly software interface that enables users to customize the system to meet their specific requirements.

Overall, the MADS1000 multi-antenna attitude determination system represents a significant advancement in UAV navigation technology. Its advanced multi-antenna technology, combined with high accuracy and ease of integration, makes it an excellent choice for a wide range of industries and applications. Whether you are looking to improve the efficiency of your UAV fleet or enhance the safety of your operations, the MADS1000 is the perfect solution for your needs.

GINS3000 GNSS/INS Integrated Navigation System widely used in ship and boat

GINS3000 GNSS/INS Integrated Navigation System is low-cost high performance integrated navigation system, which has been widely used in ship and boat.

GINS3000 GNSS/INS Integrated Navigation System widely used in small plane

GINS3000 GNSS/INS Integrated Navigation System is low cost high performance integrated navigation system, which has been widely used in civil planes.

 

Product Advantages

Why Selecting GINS3000 GNSS/INS Integrated Navigation System?

GINS3000 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:

  1. High Accuracy, High Performance and Powerful Functions

GINS3000 GNSS/INS Integrated Navigation System is a high performance integrated navigation system, which enjoys excellent technical advantages:

– High Performance MEMS Inertial System with

GPS/GLONASS Satellite Navigation System

– High Accuracy: Yaw: 0.5° (1σ), Attitude: 0.23° (1σ),

Velocity <0.05~0.1m/s, Position < 5m (L1/L2 single

point), <8cm (RTK), Heave: <15cm (1σ)

– RS422 Interface, 100Hz Data Output Rate

– High Reliability, Strong Vibration Proof

– Advanced SkyMEMS Data Fusion Algorithm

GINS3000 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.

  1. Aerospace Level Reliability, 12-step Strictest Quality Control

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.

  1. Competitive Price, ODM supported

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.

  1. Successful Applications in Tens of Fields, 300+ Customers are Using

We are continuously focusing on MEMS measurement & control technologies, and have developed the most advanced GNSS/INS Integrated Navigation System GINS3000. and GINS3000 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.

  1. World-class Production Line, Fast Delivery

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.

  1. Service with Heart, Professional Technical Support

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.

FAQ

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.

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