DATA-WARE OF PRECISION ATTITUDE AND HEADING REFERENCE SYSTEM
DOI:
https://doi.org/10.18372/2306-1472.76.13154Keywords:
attitude and heading reference system, data-ware, inertial navigation, multimode systemAbstract
Purpose: The paper focuses on features of data-ware of precision attitude and heading reference systems, which can be applied in the high-precision applications, for example, navigation of marine vehicles. The main goal is to create the data-ware adapted to functioning of the multi-mode navigation system. Methods: To solve the given problem the methods of the inertial navigation, automatic control theory including servo systems and methods of statistical processing of information are used. Results: The data-ware of the precision attitude and heading reference system is developed taking into consideration different modes of the system and interrelation between them. The basic expressions of data-ware for the high precision multimode attitude and heading reference system are obtained. The general block-scheme of operating algorithm of the system is given. Conclusions: The results of development of data-ware of the precision attitude and heading reference system taking into consideration presence of some operating modes are represented. Obtained results can be useful for design of precision navigation systems of the moving vehicles of the wide class.
References
Sushchenko O.A. (2017) Mathematical model of attitude and heading reference system with biaxial platform. Proceedings of the National Aviation University, no. 1, pp. 31–41. doi: 10.18372/2306-1472.71.11745.
Sushchenko O.A. (2017) Mathematical model of triaxial multimode attitude and heading reference system. Proceedings of the National Aviation University, no. 2, pp. 31–41. doi: 10.18372/2306-1472.71.11745.
Sushchenko O.A. (2017) Design of robust navigation laws and stabilization contours of precision attitude and heading reference system. Proceedings of the National Aviation University, no. 3, pp. doi: 10.18372/2306-1472.72.11981.
Sushchenko O. A. (2017) Simulation of precision attitude and heading reference perturbed by environmental disturbances. Proceedings of the National Aviation University, no. 4, pp. 44–51. doi:10.18372/2306-1472.73.12170.
Hilkert J.M. (2008) Inertially stabilized platform technology. IEEE Control Systems Magazine, vol. 28, no. 1, pp. 26 – 46. doi:0.1109/MCS.2007.910256.
Wang H.G., Williams T.G. (2008) Strategic inertial navigation systems. IEEE Control Systems Magazine, vol. 28, no. 1, pp. 65 – 85. doi: 10.1109/ MCS.2007.910206
Amitava Bose, K.N. Bhat, Thomas Kurian. (2014) Fundamentals of navigation and inertial sensors, PHI Learning, 312 p.
Sokolov V.S., Pogorelov V.A. (2016) Stoxastyicheskaya ocenka, upravlenyie i ydentyfykacyya v visokotochnix navygacyonnix systemax [Stochastic estimation, control and identification in high-precision navigation systems].Moscow, Fizmatlit, 264 p.
Farrell J., Barth M. (2013)The Global Positioning System & Inertial Navigation, USA, McCraw-Hill, 333p.
Rivkin S.S. (1978) Stabylyzatsyya yzmerytel'nikh ustroystv na kachayushchemsya osnovanyy [Stabilization of measuring devices on swinging base]. Moscow, Nauka, 239 p.
Lawrence A. (1998) Modern inertial technology: navigation, guidance and control, New York, Springer-Verlag, 512 p. doi:10.1007/978-1-4684-0444-9