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A New Method for Measuring Angular Increments Based on a Tri-Axial Accelerometer and a Tri-Axial Magnetometer

A New Method for Measuring Angular Increments Based on a Tri-Axial Accelerometer and a Tri-Axial... REFERENCES[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. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Artificial Satellites de Gruyter

A New Method for Measuring Angular Increments Based on a Tri-Axial Accelerometer and a Tri-Axial Magnetometer

Zhu, X.N.; Ma, M.; Cheng, D.F.; Zhou, Zh.J.
Artificial Satellites , Volume 53 (1): 7 – Mar 1, 2018
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Publisher
de Gruyter
Copyright
© 2018 X.N. Zhu et al., published by De Gruyter Open
ISSN
2083-6104
eISSN
2083-6104
DOI
10.2478/arsa-2018-0005
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Abstract

REFERENCES[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.

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Artificial Satellites – de Gruyter

Published: Mar 1, 2018

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