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SENSOR FUSION

Research Database

Software

Projects:

Airborne
Gravimetry

GPS/INS
Coupling

ENVISAT Radar
Altimeter Calibration

Pseudolite
Research

GNSS/INS Coupling

Because of different error influences based on space segment, signal propagation, receiver technology or user environment the accuracy potential of GNSS systems is not sufficient for all applications in geodesy and navigation. Additionally the availability and data frequency can be inadequate. Therefore many navigation or surveying systems use hybrid GNSS/INS sensors to combine the only short-time stability of an inertial sensor and the long-time stability but noise behaviour of a GNSS receiver. Furthermore both sensors base on completely different principles for the determination of position, velocity and attitude. Depending on the application and the used sensor types more or less advantages in accuracy, availability, integrity and data frequency can be achieved.  

GNSS/INS systems can be characterized by their implemented coupling principle. Today basically three different methods are operational or current investigation topic: loose, tight or deep coupling.

Most GPS/INS integrations are loosely coupled, giving up a great deal of performance in return for simplicity of integration. Using this principle the position and velocity estimates of a GNSS receiver are used as observations in an INS filter for estimation of INS errors, a reduction of GPS-noise and a bridging of GPS outages are possible

        Loose coupling principle

In this case the GNSS measurements are also usable when fewer than four satellites are tracked. Knowing the INS position lost ambiguity values can be restored more quickly.

In case of high dynamic applications or in jamming environments the principle of tight-coupling becomes very interesting. Information about the receicer dynamics measured by the inertial sensor is used to support the tracking loops of the integrated navigation system.

                                            
Tight coupling principle        

An extension of this concept is the deeply coupling method. In this case the integrating navigation filter is implemented as one element of the receiver tracking loop. Using inertial information in combination with the in-phase and quadra-phase signals of the receiver signal processing an optimal controlling value for the numerical oscillator can be computed. Optimisations of signal tracking performance are the goal of this method.     

Sensor Components
GNSS/INS Applications
 

Point of contact: Prof. Bernd Eissfeller

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