ROBUST UAV CONTROL SYSTEM WITH REDUNDANT NONORTHOGONAL MEASURING INSTRUMENT
DOI:
https://doi.org/10.18372/1990-5548.56.12934Keywords:
Control system, nonorthogonal configuration, rate gyroscope, redundancy, robust controllerAbstract
The paper deals with synthesis of robust system assigned for operation on unmanned aerial vehicles. A feature of the system lies in using nonorthoginal measuring instrument. Synthesis of the controller was carried out by means of the robust structural synthesis. Such an approach requires development of the mathematical model of a plant. Therefore models of longitudinal and lateral motion of an unmanned aerial vehicle` were obtained. These models take into consideration nonorthogonal redundant measuring system, which includes rate gyroscopes based on microelectromechanical systems technology. Matrices of state, control, observation in the state space were obtained using AeroSim Technology. Results of synthesied system simulation are represented. The obtained results can be useful for moving vehicles of the wide class.References
J. Cheng, J. Dong, R. Landry, and D. A. Chen, “Novel optimal configuration form redundant MEMS inertial sensors based on the orthogonal rotation method,” Sensors, vol. 14(8), pp. 13661–13678, 2014.
J. O. Nilsson, I. Skog, and P. Handel, An open-source multi inertial measurement unit (MIMU) platform. Inertial Sensors and Systems.
O. A. Sushchenko, Y. N. Bezkorovainyi, and N. D. Novytska, “Nonorthogonal redundant configurations of inertial sensors,” IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD), 2017.
A. D. Epifanov, Redundant Systems of Aircraft Control. Moscow: Mashinostroenie, 1978, 178 p. (in Russian)
O. A. Sushchenko, Y. N. Bezkorovainyi, and N. D. Novytska, “Theoretical and Experimental Assessments of Accuracy of Nonorthogonal MEMS Sensor Aarrays,” EasternEuropean Journal of Enterprise Technologies, no. 3, pp. 78–87. Год???
G. J. Holland, P. J. Webster, J. A. Curry and et al., The aerosonde robotic aircraft: a new paradigm for environmental observations, Bulletin of the American meteorological society, vol. 82, no. 5, 2001, pp. 889–901.
D. McLean, Automatic Flight Control Systems, Prentice Hall, Inc., 1990, 593 p.
J. C. Jeromel, P. L. Peres, and S. R. Souza, “Convex Analysis of Output Feedback Control Problems: Robust Stability and Performance,” IEEE Trans, on Automatic Control. vol. 41, no. 7, Jul. 1996, pp. 903–1003.
AeroSim – Aerospace Technology. Mode of direct access: AeroSimwww.aerospace-technology.com/contractors/training/aerosim/
A. A. Tunik, J. C. Kim, and C. S. Yoo, “The Parameter Optimization of Aircraft’s Control Law from the Viewpoint of Some Airworthiness Requirements,” Proceedings of the 12th Korea Automatic Control Conf. “97 КАСС”. ICASE Publ. Seoul, 1997, pp. 1651–1654.
Brian L. Stevens and Frank F., Lewis, Aircraft Control and Simulation, [2nd ed.]. John Wiley & Sons Inc., 2003, 665 р.
S. Skogestad and I. Postlethwaite, Multivariable Feedback Control, New York: Jonh Wiley, 1997, 559 p.
I. P. Egupov, Methods of Robust, Neuro-Fuzzy and Adaptive Control, Moscow: MSTU named after N.E. Bauman, 2002. (in Russian).
Downloads
How to Cite
Issue
Section
License
The scientific journal “Electronics and control systems” adheres to the principles of Open Access and provides free, immediate, and permanent access to all published materials without financial, technical, or legal barriers for readers.
All articles are published in Open Access under the Creative Commons Attribution 4.0 International (CC BY 4.0) license.
Copyright
Authors who publish their works in the journal “Electronics and control systems”:
-
retain the copyright to their publications;
-
grant the journal the right of first publication of the article;
-
agree to the distribution of their materials under the CC BY 4.0 license;
-
have the right to reuse, archive, and distribute their works (including in institutional and subject repositories), provided that proper reference is made to the original publication in the journal.