Aircraft Overloads Restoration by Measuring its Velocity and Orientation Angles Based on the Nonlinear Programming Method
| Authors: Korsun O.N., Korolev A.Yu., Stulovskiy A.V. | Published: 10.10.2025 |
| Published in issue: #3(152)/2025 | |
| DOI: | |
| Category: Informatics, Computer Engineering and Control | Chapter: System Analysis, Control, and Information Processing | |
| Keywords: aircraft, signal restoration, nonlinear programming, Hermite splines, Chebyshev polynomials | |
Abstract
The paper considers application of the nonlinear programming method in solving the signal restoration problem. It assumes that the input signal could be represented as a weighted sum of elements of the given basis, after that the expansion coefficients are determined by the numerical optimization methods from the condition of the best fit to the system outputs. The problem of restoring overloads of an aircraft is solved, when the orientation angles and velocity projections in the normal coordinate system are known. Chebyshev polynomials and Hermite splines are compared as the basis for signals representation. The paper lists advantages and disadvantages of both the approaches to numerical solution of the selected problem. A modified Newton method is applied to determine the expansion coefficients. It assesses the influence of various types of measurement errors on the solution accuracy. Errors in assessing velocity projections distributed according to the normal law, constant errors in the velocities and yaw angles, as well as in the overloads boundary conditions are considered. The proposed method is not affected by constant errors in the velocity projections, and errors in the overloads boundary conditions provide a limited effect on the solution accuracy concentrated mainly at the beginning and end of the section. The solution quality deteriorates when introducing random noise into the velocity projections and constant errors into the yaw angle making it possible to compare selected methods of the signal approximation. The numerical experiment showed that the Chebyshev polynomials in the general case allow achieving a more accurate signal approximation than the cubic splines, despite the smaller number of parameters
Please cite this article in English as:
Korsun O.N., Korolev A.Yu., Stulovskiy A.V. Aircraft overloads restoration by measuring its velocity and orientation angles based on the nonlinear programming method. Herald of the Bauman Moscow State Technical University, Series Instrument Engineering, 2025, no. 3 (152), pp. 105--120 (in Russ.). EDN: NSQNYJ
References
[1] Beard R.W., McLain T.W. Small unmanned aircraft. Theory and practice. Princeton, Princeton University Press, 2012.
[2] Gregory J.W., Liu T. Introduction to flight testing. Hoboken, John Wiley & Sons, 2021.
[3] Korsun O.N., Poplavskiy B.K. Estimation of systematic errors of onboard 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. Sc. Int., 2011, vol. 50, no. 1, pp. 130--143. DOI: https://doi.org/10.1134/S1064230711010126
[4] Murray-Smith D.J. A review of inverse simulation methods and their application. Int. J. Model. Simul., 2014, vol. 34, no. 3, pp. 120--125. DOI: http://dx.doi.org/10.2316/Journal.205.2014.3.205-5906
[5] Kozyrev G.I., Yuditskikh E.O. Restoration of input signals of dynamic measuring systems using digital reverse filtering. Izmeritelnaya tekhnika, 2023, no. 5, pp. 10--16 (in Russ.). DOI: https://doi.org/10.32446/0368-1025it.2023-5-10-16
[6] Samoylenko M.V. Restoration of filter input signal by the output signal and pulse response. DSPA: voprosy primeneniya tsifrovoy obrabotki signalov, 2017, no. 2, pp. 194--198 (in Russ.). EDN: ZCGOGT
[7] Krivulin N.P. Recovering input signals of non stationary dynamical systems. Povolzhskiy region. Fiziko-matematicheskie nauki [University Proceedings. Volga Region. Physical and Mathematical Sciences], 2018, no. 3, pp. 64--78 (in Russ.).DOI: https://doi.org/10.21685/2072-3040-2018-3-6
[8] Novikov-Borodin A.V. Reconstruction and simulation of experimental data using test measurements. Instrum. Exp. Tech., 2022, vol. 65, no. 2, pp. 238--245. DOI: https://doi.org/10.1134/S0020441222020166
[9] Korsun O.N., Motlich P.A., Medvedkov A.N. Method for reconstructing aircraft overload projections from speed measurements made by the navigation system. Polet [Flight], 2021, no. 11, pp. 3--11 (in Russ.). EDN: LUTGQN
[10] Conway B.A. A survey of methods available for the numerical optimization of continuous dynamic systems. J. Optim. Theory Appl., 2012, vol. 152, no. 2, pp. 271--306. DOI: https://doi.org/10.1007/s10957-011-9918-z
[11] Luenberger D.G., Ye Y. Linear and nonlinear programming. Cham, Springer International, 2021.
[12] Rao A.V. Survey of numerical methods for optimal control. Advances in the Astronautical Sciences, 2010, vol. 135, pp. 497--528.
[13] Korsun O.N., Stulovskiy A.V. Direct method for forming the optimal open loop control of aerial vehicles. J. Comput. Syst. Sc. Int., 2019, vol. 58, no. 2, pp. 229--243. DOI: https://doi.org/10.1134/S1064230719020114
[14] Kvasov B.I. Metody izogeometricheskoy approksimatsii splaynami [Methods of isogeometric spline approximation]. Moscow, FIZMATLIT Publ., 2006.
[15] Corriou J.P. Numerical methods and optimization. Сham, Springer Nature, 2021.
[16] Corriou J.P. Numerical methods and optimization. Cham, Springer Nature, 2021.
[17] Byushgens G.S. Aerodinamika, ustoychivost i upravlyaemost sverkhzvukovykh samoletov [Aerodynamics, stability and controllability of supersonic aircrafts]. Moscow, FIZMATLIT Publ., 1998.
[18] Stengel R.F. Flight dynamics. Princeton, Princeton University Press, 2004.
[19] Korsun O.N., Stulovskiy A.V. Recovery of aircraft motion parameters using the optimal control algorithms. J. Comput. Syst. Sc. Int., 2023, vol. 62, no. 1, pp. 61--72. DOI: https://doi.org/10.1134/S1064230723010057
[20] Klein V., Morelli E.A. Aircraft system identification. Theory and practice. Reston, AIAA, 2006.
[21] Gupta R.K. Numerical methods. Fundamentals and applications. Cambridge, Cambridge University Press, 2019.
