|

Methods in the forecasting models construction based on the evolutionary algorithms

Authors: Grigoryev L.V., Stepchenko E.I.
Published in issue: #12(89)/2023
DOI: 10.18698/2541-8009-2023-12-959


Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

Keywords: inertial navigation system, navigation system, self-organization algorithm, gyro-stabilized platform deflection angle, short-term forecast, unmanned aerial vehicle, inertial navigation system errors, correction
Published: 25.01.2024

A forecasting method was implemented. It is based on the self-organization algorithm and makes it possible to fairly accurately obtain a short-term forecast of the error of the inertial navigation system test model in the autonomous mode. Forecasting method development based on the self-organization algorithm provides a possibility to construct models of the process under consideration with a minimum or even complete absence of the a priori information. A model constructed in the inertial navigation system correction mode with the external sensors could be introduced in the offline correction mode provided that the correction signal disappears, which allows increasing the navigation information accuracy.


References

[1] Neusypin K.A. Sovremennye sistemy i metody navedeniya, navigatsii i upravleniya letatel’nymi apparatami [Modern systems and methods of guidance, navigation and control of aircraft]. Moscow, MSOU Publ., 2009, 500 p. (In Russ.).

[2] Neusypin K.A. Development of modified self-organization algorithms for correction of navigation information. Avtomatizatsiya. Sovremennye tekhnologii, 2009, no. 1, pp. 37–39. (In Russ.).

[3] Shen’ Kay, Proletarskiy A.V., Neusypin K.A. The research into correction algorithms for aircraft navigation systems. Herald of the Bauman Moscow State Technical University. Series Instrument Engineering, 2016, no. 2, pp. 28–39. (In Russ.). http://doi.org/10.18698/0236-3933-2016-2-28-39

[4] Afanas’ev V.N., Neusypin K.A. A method of compensating for dynamic errors in inertial system. Avtomat i telemekh., 1992, no. 8, pp. 19–24. (In Russ.).

[5] Neusypin K.A. The intellectual system development directions. Avtomatizatsiya i sovremennye tekhnologii, 2002, no. 12, pp. 12–16. (In Russ.).

[6] Chzhao Yan, Shen’ Sin’. Development of self-organization algorithms for navigation systems correction. Politekhnicheskiy molodezhnyy zhurnal, 2019, no. 10 (39). (In Russ.). http://dx.doi.org/ 10.18698/2541-8009-2019-10-538

[7] Neusypin K.A., Ke Fan, Sholokhov D.O. Development of algorithm to construct models using self-organization method for correction of navigational systems. Herald of the Bauman Moscow State Technical University. Series Instrument Engineering, 2010, no. 3 (80), pp. 57–67. (In Russ.).

[8] Ivakhnenko A.G., Myuller Y.Ya. Samoorganizatsiya prognoziruyushchikh modeley [Self-organization of predictive models]. Kiev, Tekhnika Publ., 1985, 224 p. (In Russ.).

[9] Tsibizova T.Yu., Nguen D.T. Algorithmic methods of navigation systems’ correction in output signal. Internet zhurnal “Naukovedenie”, 2015, vol. 7, no. 3. (In Russ.). https://dx.doi.org/10.15862/162TVN315

[10] Proletarskiy A.V., Neusypin K.A., Shen’ Kay. Algorithmic methods for correcting autonomous inertial navigation systems. Upravlenie v morskikh i aerokosmicheskikh sistemakh. 7-ya Ross. mul’tikonf. po problemam upravleniya: sb. st. [Control in marine and aerospace systems. 7th Russian multi-conference on management problems: collection of articles]. Saint Petersburg, Kontsern “TsNII “Elektropribor” Publ., 2014, pp. 637–641. (In Russ.).