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GNSS INS Integrate Navigation System GINS1000 1
GNSS INS Integrate Navigation System GINS1000 2
GNSS INS Integrate Navigation System GINS1000 3
GNSS INS Integrate Navigation System GINS1000 4

GINS1000 Single Antenna Integrated Navigation System

High precision integrated navigation system, widely used in unmanned aerial vehicle (UAV), vehicle navigation, the surface craft, ship and so on.

  • High Precision MEMS Inertial System with GPS/BD Dual-mode Satellite Navigation System
  • High Accuracy: Heading: 0.15°(rms), Attitude: 0.05° (rms), Velocity <0.15m/s, Position < 1.5m
  • Support Dynamic Fast Alignment
  • High Reliability, Strong Vibration and Shock Resistance
  • Multiple Interfaces: RS232/RS422/TTL/CAN
  • Easy to Integrate with Odometer/DVL Sensor
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Brief Introduction

GINS1000 Single Antenna Integrated Navigation System from China factory adopts high precision MEMS inertial components and integrates GPS/BD single frequency dual-mode satellite navigation system. It has a built-in magnetic heading measurement system and a height measurement solution. As a China GINS1000 Single Antenna Integrated Navigation System manufacturer, we have a special SkyMEMS new integrated navigation fusion algorithm, which can realize high sensitivity tracking and accurate positioning in open space, and it also can realize navigation applications in the city, forest, canyon terrain, etc. The system enjoys a smaller size, lighter weight, lower cost, lower power consumption, faster start-up, higher reliability, better dynamic environment adjustment, etc. It can be applied in tactical weapons and unmanned aircraft fields. It is suitable for the navigation and control of all kinds of moving objects, such as an unmanned aerial vehicle (UAV), vehicle navigation, surface craft, ship, and so on.

1. Introduction:

What is an Integrated Navigation System (INS)?
Integrated Navigation System (INS) refers to a system that makes navigation and positioning very well in a variety of environments. It is used in many unmanned aerial vehicles, unmanned surface craft, and ground vehicles. The technology is widely used in air traffic control, search and rescue, surveillance, and commercial applications.
Integrated Navigation System (INS) is the area of operation technology for guided vehicles, aircraft, and ships.
Let’s take a look at a few of the advantages of INS over other systems such as GPS or ADF:
• No need for external beacons – no receivers required! – this can be advantageous if your vehicle has anti-collision systems on board that prevent contact with objects that have not been announced by the onboard radars.
• NO external power supplies are required! – this can be advantageous if your vehicle has anti-collision systems on board that prevent contact with objects which have not been announced by the onboard radars.
• No need for fuel to make it go where you want it to go – this can be advantageous if your vehicle has anti-collision systems on board that prevent contact with objects which have not been announced by the onboard radars.
• No need for antennas or any power supply needed when you are flying in ADSB or VHF mode . . . – this can be advantageous if your vehicle has anti-collision systems on board that prevent contact with objects which have not been announced by the onboard radars.
An integrated Navigation System (INS) is one way to complete the equation when it comes to UAVs, space exploration & science missions:
• Digital maps • Automatic course adjustment • Automatic landing • Automatic take-off & landing • Tracking • Localisation • Avoidance of collisions with other aircraft • No radar emissions
What is an integrated navigation system? According to Wikipedia: “Integrated navigation system incorporates both global positioning system (GPS), inertial navigation system (INS), and attitude reference unit (ARU), all powered by an electric propulsion motor that adds downlink corrections and provides uplink corrections when using electronic velocity compensation”  The term “integrated navigation system” was first introduced into English in 2005 by Thales in France as part of its development program at the Centinela Radionavigation Centre in Andorra la Vella

Technical Specifications

Parameter　          Value

Model GINS1000-A GINS1000-B
Heading Accuracy L1/B1 single point 0.15°(rms)
Magnetic 0.5°(rms)
Attitude Roll/Pitch accuracy <0.15° degree (RMS) <0.05° degree (RMS)
Velocity Velocity accuracy <0.15m / s (RMS)
Position Position accuracy <1.5m (RMS)
Gyroscope Range ±300 °/s (or ±800 °/s optional)
Non-linearity 0.0005 0.0002
Bias stability ≤4.5°/h (allan variance) ≤0.5°/h (allan variance)
Resolution 0.03 °/s 0.003 °/s
Noise 0.3 °/s (RMS) 0.01 °/s (RMS)
Accelerometer Range ±10g  (or ±2g, ±5g, ±30g optional)
Bias ≤5mg ≤2mg
Bias  instability ≤1mg ≤0.1mg
Bias  repeatability ≤3mg ≤1mg
Non-linearity 0.05% (full range) 0.02% (full range)
Noise 400ug (RMS) 40ug (RMS)
Magnetic sensor Range 6Gauss
Resolution 120uGauss
Noise 50uGauss (RMS)
Altimeter Range 1100mbar
Resolution 0.1mbar
Absolute Accuracy 1.5mbar
Receiver Working mode BD2 B1/GPS L1
Startup Time ≤60s
Electrical Specs Power supply 9~36VDC
Power consumption ≤3W @12VDC
Electrical interface RS232/RS422/TTL/CAN (Optional)
Output rate 100~400Hz @115,200 baud rate (IMU), 100~200Hz (attitude)
Environment Conditions Working temperature -40~+70°C
Storage temperature -55~+85°C
Vibration 6.06g @ 20~2000 Hz
Shock 30g, 11 ms, 1/2 Sine
Physical Characteristics Size 57 × 57× 34.5mm
Weight ≤200grams (not include antenna)

Typical Application

GINS1000 Single Antenna 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

GINS1000 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. GINS1000 GNSS/INS Integrated Navigation System is a low-cost high performance integrated navigation system, which has been widely used in unmanned UAV Navigation.

GINS1000 GNSS/INS Integrated Navigation System widely used in ship and boat

GINS1000 GNSS/INS Integrated Navigation System is low-cost high performance integrated navigation system, which has been widely used in ship and boat.

GINS1000 GNSS/INS Integrated Navigation System widely used in small plane

GINS1000 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 GINS1000 GNSS/INS Integrated Navigation System?

GINS1000 Single Antenna 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

China GINS1000 Single Antenna Integrated Navigation System is a high performance integrated navigation system, which enjoys excellent technical advantages: – High Precision MEMS Inertial System with GPS/BD Dual-mode Satellite Navigation System – High Accuracy: Heading: 0.15°(rms), Attitude: 0.05° (rms), Velocity <0.15m/s, Position < 1.5m – Support Dynamic Fast Alignment – High Reliability, Strong Vibration and Shock Resistance – Multiple Interfaces: RS232/RS422/TTL/CAN – Easy to Integrate with Odometer/DVL Sensor GINS1000 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 China GINS1000 Single Antenna Integrated Navigation System from manufacturer. and GINS1000 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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