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Russian Aeronautics

, Volume 61, Issue 2, pp 311–315 | Cite as

To the Problem of Estimating the Angle of Attack of an Aircraft by the Kalman Filter

  • A. A. GolovanEmail author
  • A. V. Sharonov
Flight Dynamics and Control of Flight Vehicles
  • 7 Downloads

Abstract

The paper considers the problem of estimating the angle of attack of an aircraft only by indications of accelerometers that are rigidly set on its fuselage. This task is posed as a task of “realization”, when the structure and the order of linearized model of the estimation problem is unknown. The possibility of solving this problem is analyzed.

Keywords

angle of attack Hankel matrix Ho–Kalman algorithm 

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References

  1. 1.
    Ganeev, F.A., Synthesis of a Structure and a Transformation Algorithm for the Aircraft Time-of-Flight Ion-Marking Airspeed and Angle of Attack Sensor, Izv.Vuz. Av. Tekhnika, 2006, vol. 50, no. 4, pp. 53–56 [Russian Aeronautics (Engl. Transl.), vol. 50, no. 4].Google Scholar
  2. 2.
    Ganeev, F.A. and Soldatkin, V.M., Optimization of Electrode System for the Aircraft Time-of-Flight Ion-Marking Airspeed and Angle of Attack Sensor, Izv. Vuz. Av. Tekhnika, 2011, vol. 54, no. 1, pp. 51–54 [Russian Aeronautics (Engl. Transl.), vol. 54, no. 1, pp. 71–76].Google Scholar
  3. 3.
    Maksimov, A.K., Indirect Method of Definition of Aerodynamic Angles: Angle of Attack and Angle of Sliding, Trudy MAI, 2015, no. 84, pp. 1–23.Google Scholar
  4. 4.
    Ostroslavskii, I.V. and Strazheva, I.V., Dinamika poleta. Ustoichivost’ i upravlyaemost’ letatel’nykh apparatov (Dynamics of Flight. Stability and Controllability of Aircraft), Moscow: Mashinostroenie, 1965.Google Scholar
  5. 5.
    Parusnikov, N.A., Morozov, V.M., and Borzov, V.I., Zadacha korrektsii v inetsial’noi navigatshii (Correction Problem in the Inertial Navigation), Moscow: Izd. MGU, 1982.Google Scholar
  6. 6.
    Kalman, R.E., Falb. P.L., and Arbib M.A., Topics in Mathematical System Theory, New York: McGraw-Hill, 1969.zbMATHGoogle Scholar
  7. 7.
    Pushkov, S.G. and Gorelik, A.A., Use of the Interval Analysis Methods for Calculation of Dimension of Finite-Dimensional Realization of Linear Dynamic System, Vestnik OGU, 2010, no. 9 (115), pp. 59–64.Google Scholar
  8. 8.
    Ho, B.L. and Kalman, R.E., Effective Construction of Linear State-Variable Models from Input-Output Functions, Regelungstechnik, 1966, vol. 14, no. 12, pp. 545–548.zbMATHGoogle Scholar
  9. 9.
    De Schutter, B., Minimal State-Space Realization in Linear System Theory: An Overview, Journal of Computational and Applied Mathematics, 2000, vol. 121, no. 1–2, pp. 331–354.MathSciNetCrossRefzbMATHGoogle Scholar
  10. 10.
    Sovremennye metody i sredstva izmereniya parametrov gravitatsionnogo polya Zemli (Modern Techniques and Facilities of Parameters Measurement of the Earth’s Gravitational Field), Peshekhonov, V.G, Ed., St.-Petersburg: TzNII Electropribor, 2017.Google Scholar

Copyright information

© Allerton Press, Inc. 2018

Authors and Affiliations

  1. 1.Lomonosov Moscow State UniversityMoscowRussia
  2. 2.Moscow Aviation Institute (National Research University)MoscowRussia

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