A new method for measuring angular increments based on a tri-axial accelerometer and a tri-axial magnetometer

• Autorzy: Zhu X. N. , Ma M. , Cheng D. F. , Zhou Zh. J.

Identyfikatory

DOI

10.2478/arsa-2018-0005

• Języki publikacji: EN

Abstrakty

EN

Tri-axial gyroscopes used to be the only instrument used to measure the angular increments of airplanes. However, because there were no reference devices, drift and accumulation errors affected the accuracy of the estimated attitude. In this paper, we propose a novel method for measuring angular increments based on a tri-axial accelerometer and a triaxial magnetometer. Then, we mathematically proved the feasibility of the proposed method. The results of our simulation and experimental tests indicated that the proposed method accurately indicates the attitude of an airplane.

Słowa kluczowe

EN

airplane; tri-axial accelerometer; tri-axial magnetometer; method

• Wydawca: Centrum Badań Kosmicznych PAN ; De Gruyter
• Czasopismo: Artificial Satellites : Journal of Planetary Geodesy
• Rocznik: 2018
• Tom: Vol. 53, No. 1
• Strony: 47--53
• Opis fizyczny: Bibliogr. 7 poz., rys.

Twórcy

autor

Zhu X. N.

• College of Instrumentation & Electrical Engineering, Jilin University

autor

Ma M.

• College of Instrumentation & Electrical Engineering, Jilin University

autor

Cheng D. F.

• College of Instrumentation & Electrical Engineering, Jilin University

autor

Zhou Zh. J.

• College of Instrumentation & Electrical Engineering, Jilin University

Bibliografia

• [1] Lee, D. C., Moon, G., & Lee, J. C. (2002). Mechanical dither design for ring laser gyroscope. KSME international journal, 16(4), 485-491.
• [2] Titterton, D., & Weston, J. L. (2004). Strapdown inertial navigation technology (Vol. 17). IET.
• [3] Georgy, J., Noureldin, A., Korenberg, M. J., & Bayoumi, M. M. (2010). Modeling the stochastic drift of a MEMS-based gyroscope in gyro/odometer/GPS integrated navigation. IEEE Transactions on Intelligent transportation systems, 11(4), 856-872.
• [4] Gebre-Egziabher, D., Hayward, R. C., & Powell, J. D. (1998). A low-cost GPS/inertial attitude heading reference system (AHRS) for general aviation applications. Position Location and Navigation Symposium, IEEE 1998 (pp. 518-525).
• [5] De Marina, H. G., Pereda, F. J., Giron-Sierra, J. M., & Espinosa, F. (2012). UAV attitude estimation using unscented Kalman filter and TRIAD. IEEE Transactions on Industrial Electronics, 59(11), 4465-4474.
• [6] Shuster, M. D., & Oh, S. D. (2012). Three-axis attitude determination from vector observations. Journal of Guidance, Control, and Dynamics.
• [7] Hasan, A. M., Samsudin, K., Ramli, A. R., Azmir, R. S., & Ismaeel, S. A. (2009). A review of navigation systems (integration and algorithms). Australian Journal of Basic and Applied Sciences, 3(2), 943-959.

Uwagi

Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).