Multipurpose Remotely Piloted Aircraft System Integrated Navigation System Development and Testing

• Autorzy: Petrovich-Kharchenko V. , Ilnytska S.
• Języki publikacji: EN

Abstrakty

EN

The paper presents development of prototype of integrated inertial-satellite navigation system that contains 3-axis accelerometers, gyros, magnetometers, barometric altimeter and GNSS (Global Navigation Satellite System) receiver. Navigation system testing procedure by means of flight at airdrome at small remotely piloted aircraft system (RPAS) is described, and data processing details with results are submitted. These results received from the data post-processing had approved the efficiency of integrated navigation system functioning in normal navigation mode, i.e. during availability of GNSS measurements. It has been shown as well that after approximately 10 s of autonomous MEMS inertial navigation system (INS) functioning accuracy of velocity and position calculation degrades significantly.

Słowa kluczowe

EN

remotely piloted aircraft system (RPAS); integrated navigation system; strapped down inertial navigation system (SINS); global navigation satellite system (GNSS); MEMS sensor; logistic

• Wydawca: Międzynarodowa Wyższa Szkoła Logistyki i Transportu we Wrocławiu
• Czasopismo: Logistics and Transport
• Rocznik: 2013
• Tom: Vol. 19, No. 3
• Strony: 85--90
• Opis fizyczny: Bibliogr. 11 poz., rys.

Twórcy

autor

Petrovich-Kharchenko V.

• National Aviation University, Ukraine

autor

Ilnytska S.

• National Aviation University, Ukraine

Bibliografia

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• [10] Larin V.B. About correction of inertial navigation system functioning / A.A. Tunik, V.B. Larin // Problems of control and informatics. – 2010. – №4. – P. 130–142.
• [11] Kharchenko V.P. Analysis of the efficiency of algorithms of integrated inertialsatellite navigation system / V.P. Kharchenko, S.I. Ilnytska // Mechanics of gyroscopic systems. Scientific-technical digest of Kyiv Polytechnic university. Edition 22. Kyiv 2010 – P. 32–43.