An optimized TRIAD algorithm for attitude determination

• Autorzy: Zhu Xiaoning , Ma Ming , Cheng Defu , Zhou Zhijian

Identyfikatory

DOI

10.1515/arsa-2017-0005

• Języki publikacji: EN

Abstrakty

EN

The classic TRIAD was used to obtain the attitude of air vehicles. However, the accuracy was dominated by the sensor noise and the calculation order. To improve that in this paper, a new method based on weighting the vectors summation and difference was proposed. Then both simulation and experiment verified the advantages of the optimized algorithm.

Słowa kluczowe

EN

air vehicle; TRIAD; algorithm; method; satellites

• Wydawca: Centrum Badań Kosmicznych PAN ; De Gruyter
• Czasopismo: Artificial Satellites : Journal of Planetary Geodesy
• Rocznik: 2017
• Tom: Vol. 52, No. 3
• Strony: 41--47
• Opis fizyczny: Bibliogr. 17 poz., rys., tab.

Twórcy

autor

Zhu Xiaoning

• College of Instrumentation & Electrical Engineering, Jilin University, China, 130000

autor

Ma Ming

• College of Instrumentation & Electrical Engineering, Jilin University, China, 130000

autor

Cheng Defu

• College of Instrumentation & Electrical Engineering, Jilin University, China, 130000

autor

Zhou Zhijian

• College of Instrumentation & Electrical Engineering, Jilin University, China, 130000

Bibliografia

• [1] Shuster M D, S. D. O H. Three-axis attitude determination from vector observations. Journal of Guidance Control & Dynamics, 1981, 4(1).
• [2] Han, K., Wang, H., & Jin, Z. H. (2010). Magnetometer-only linear attitude estimation for bias momentum pico-satellite. Journal of Zhejiang University-SCIENCE A, 11(6), 455-464.
• [3] Van, d. H. J. C. (2009). Progress in satellite attitude determination and control. Transactions of the Japan Society for Aeronautical & Space Sciences Space Technology Japan, 57(666), 191-198.
• [4] Çelik, O., & Hajiyev, C. (2013). A comparison of attitude determination methods for small satellites. International Conference on Recent Advances in Space Technologies (pp.261-264). IEEE.
• [5] Song, L. L., Zhang, T., Liang, B., & Yang, J. (2010). Attitude determination method based on star sensor. Journal of System Simulation.
• [6] Marina, H. G. D., Pereda, F. J., Giron-Sierra, J. M., & Espinosa, F. (2016). UAV attitude estimation using unscented Kalman filter and triad. IEEE Transactions on Industrial Electronics, 59(11), 4465-4474.
• [7] Li, Y. and Yuan, J. (2005). Attitude determination using GPS vector observations, GNSS World of China 33(3): 51-56.
• [8] Junior, F. G., & Tosin, M. C. (2007). The attitude determination problem from two reference vectors - a description of the triad algorithm and its attitude covariance matrix. Semina : Ciências Exatas e Tecnológicas, 28(1).
• [9] Ryzhkov, L. M., Ozhoh, M. V., & Prokopovych, O. V. (2014). Analysis of attitude determination algorithm TRIAD errors. IEEE, International Conference on Methods and Systems of Navigation and Motion Control (pp.176-181). IEEE.
• [10] Hao, C., & Tan, J. B. (2008). Improved triad algorithm for spacecraft attitude determination. Journal of System Simulation.
• [11] Markley, F. L. (2008). Optimal attitude matrix from two vector measurements. Journal of Guidance Control & Dynamics, 31(3), 765-768.
• [12] Cordeiro, T. F. K., Costa, J. P. C. L. D., Júnior, R. T. D. S., So, H. C., & Borges, G. A. (2016). Improved kalman-based attitude estimation framework for uavs via an antenna array. Digital Signal Processing, 59, 49-65.
• [13] Hadri, A. E., Benziane, L., Seba, A., & Benallegue, A. (2016). Sensors model based data fusion using complementary filters for attitude estimation and stabilization. IEEE International Conference on Robotics and Automation (pp.2978-2983). IEEE.
• [14] Vetrella, A. R., Fasano, G., Accardo, D., & Moccia, A. (2016). Differential GNSS and vision-based tracking to improve navigation performance in cooperative multi-uav systems. Sensors, 16(12).
• [15] Wang, Y., Chang-Siu, E., Brown, M., Tomizuka, M., Almajed, M. I., & Alsuwaidan, B. N. (2012). Three Dimensional Attitude Estimation via the Triad Algorithm and a TimeVarying Complementary Filter. ASME 2012, Dynamic Systems and Control Conference Joint with the Jsme 2012, Motion and Vibration Conference (pp.157-165).
• [16] Wang, Y. (2015). Attitude control and estimation. Dissertations & Theses - Gradworks.
• [17] Baritzhack, I. Y., & Harman, R. R. (1997). Optimized triad algorithm for attitude determination. Journal of Guidance Control & Dynamics, 20(1), 208-211.

Uwagi

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