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INS/GNSS Integration with Account for Timing Skew and Displacement of GNSS Antenna. Experience of Practical Realization

https://doi.org/10.17285/0869-7035.0070

Abstract

We examine two aspects specific to complex data fusion algorithms in integrated strapdown inertial navigation systems aided by global positioning systems, with their inherent spatial separation between the GNSS antenna phase center and the inertial measurement unit, as well as with the timing skew between their measurements. The first aspect refers to modifications of mathematical models used in INS/GNSS integration. The second one relates to our experience in their application in onboard airborne navigation algorithms developed by Moscow Institute of Electromechanics and Automatics

About the Authors

N. B. Vavilova
Moscow State University, Russia
Russian Federation


A. A. Golovan
Moscow State University, Russia
Russian Federation


A. V. Kozlov
Moscow State University, Russia
Russian Federation


I. A. Papusha
Moscow State University, Russia
Russian Federation


O. A. Zorina
Moscow Institute of Electromechanics and Automatics, JSCMoscow Institute of Electromechanics and Automatics, JSC, Russia
Russian Federation


E. A. Izmailov
Moscow Institute of Electromechanics and Automatics, JSC, Russia
Russian Federation


S. E. Kukhtevich
Moscow Institute of Electromechanics and Automatics, JSC, Russia
Russian Federation


A. V. Fomichev
Moscow Institute of Electromechanics and Automatics, JSC, Russia
Russian Federation


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For citations:


Vavilova N.B., Golovan A.A., Kozlov A.V., Papusha I.A., Zorina O.A., Izmailov E.A., Kukhtevich S.E., Fomichev A.V. INS/GNSS Integration with Account for Timing Skew and Displacement of GNSS Antenna. Experience of Practical Realization. Giroskopiya i Navigatsiya. 2021;29(3):52-68. (In Russ.) https://doi.org/10.17285/0869-7035.0070

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ISSN 0869-7035 (Print)
ISSN 2075-0927 (Online)