An Optimized Triad Algorithm for Attitude Determination

Author:

Zhu Xiaoning1,Ma Ming1,Cheng Defu1,Zhou Zhijian1

Affiliation:

1. College of Instrumentation & Electrical Engineering, Jilin University, Jilin Sheng , China

Abstract

Abstract 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.

Publisher

Walter de Gruyter GmbH

Reference17 articles.

1. [1] Shuster M D, S. D. O H. Three-axis attitude determination from vector observations. Journal of Guidance Control & Dynamics, 1981, 4(1).

2. [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), 455-464.10.1631/jzus.A0900725

3. [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. [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. [5] Song, L. L., Zhang, T., Liang, B., & Yang, J. (2010). Attitude determination method based on star sensor. Journal of System Simulation.

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