Algorithms of increasing the calculation accuracy for an aircraft's orientation angle

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• 作者：V. V. Bulgakov ; O. N. Korsun…
• 刊名：Journal of Computer and Systems Sciences International
• 出版年：2016
• 出版时间：January 2016
• 年：2016
• 卷：55
• 期：1
• 页码：150-161
• 全文大小：668 KB
• 参考文献：1.V. N. Branets and I. P. Shmygalevskii, Use of Quaternions in Problems of Orientation of Solid Bodies (Nauka, Moscow, 1973) [in Russian].
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  5.O. N. Korsun and B. K. Poplavskii, “Estimation of systematic errors of oboard measurement of angle of attack and sliding angle based on integration of data of satellite navigation system and identification of wind velocity,” J. Comput. Syst. Sci. Int. 50, 130 (2011).CrossRef MATH
  6.GOST (State Standard) 20058-80: Aircraft Dynamics in Atmosphere. Terms, Definitions and Symbols, 1981.
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• 作者单位：V. V. Bulgakov (1) (2)
  O. N. Korsun (1) (2)
  V. S. Kulabukhov (1) (2)
  A. V. Stulovskii (1) (2)
  D. S. Timofeev (1) (2)
  
  1. Uspensky Avionica Moscow Research and Production Complex (Avionica MRPC JSC), Moscow, Russia
  2. State Scientific Research Institute of Aviation Systems (GosNIIAS), Dolgoprudnyi, Russia
  
• 刊物类别：Engineering
• 刊物主题：Control Engineering
  Russian Library of Science
  
• 出版者：MAIK Nauka/Interperiodica distributed exclusively by Springer Science+Business Media LLC.
• ISSN：1555-6530

文摘

Algorithms for calculating an aircraft’s orientation angles based on the results of the numerical integration of Poisson’s and quaternion equations are proposed. The algorithms in the presence of random errors of the matrix elements of direction cosines and quaternions are characterized by a significantly higher accuracy in comparison to the formulas for solving the formulated problem. The results of testing the mathematical modeling data under random errors, which confirm the increased accuracy of the calculation of the orientation angles, are given.