Skip to main content
Log in

Method of Improving the Noise Resistance of Automatic Control Systems

  • FLIGHT DYNAMICS AND CONTROL OF FLIGHT VEHICLES
  • Published:
Russian Aeronautics Aims and scope Submit manuscript

Abstract

The paper considers the indirect measurement of disturbance based on the output parameters of the control object using its mathematical model and the disturbance compensation in order to improve the automatic control system noise resistance. The method proposed is applied to aircraft attitude motion control systems. The issues of such systems synthesis are considered. Modeling results are given.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9

Similar content being viewed by others

REFERENCES

  1. Dobrolenskii, Yu.P., Dinamika poletov v nespokoinoi atmosfere (Flight Dynamics in Turbulent Atmosphere), Moscow: Mashinostroenie, 1969.

    Google Scholar 

  2. Gus’kov, Yu.P. and Zagainov, G.I., Upravlenie poletom samoletov (Aircraft Flight Control), Moscow: Mashinostroenie, 1980.

    Google Scholar 

  3. Menskii, B.M., Printsip invariantnosti v avtomaticheskom regulirovanii i upravlenii (The Invariance Principle in Automatic Regulation and Control), Moscow: Mashinostroenie, 1972.

    Google Scholar 

  4. Rodnishchev, N.E., Romanenko, L.G., and Denisov, K.G., To Estimation of Control Law Parameters for the Lateral Motion of Aircraft Taking into Account Wind Disturbances, Izv. Vuz. Av. Tekhnika, 2015, vol. 58, no. 4, pp. 44–49 [Russian Aeronautics (Engl. Transl.), vol. 58, no. 4, pp. 407–412].

    Google Scholar 

  5. Beard, R.W. and McLain, T.W., Small Unmanned Aircraft: Theory and Practice, Princeton University Press, 2012.

    Book  Google Scholar 

  6. Petunin, V.I. and Frid, A.I., Noise Immunity of Automatic GTE Control Systems with a Selector at Channel Switching Modes, Izv. Vuz. Av. Tekhnika, 2007, vol. 50, no. 4, pp. 44–47 [Russian Aeronautics (Engl. Transl.), vol. 50, no. 4, pp. 409–414].

    Google Scholar 

  7. Petunin, V.I., Logiko-dinamicheskie sistemy s selektivnym vyborom kanalov upravleniya aviatsionnymi ob’ektami (Logical Dynamic Systems with Selective Choice of Control Channels for Aviation Objects), Moscow: Innovatsionnoe Mashinostroenie, 2018.

    Google Scholar 

  8. Bodner, V.A., Sistemy upravleniya letatel’nymi apparatami (Aircraft Control Systems), Moscow: Mashinostroenie, 1973.

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to V. I. Petunin.

Additional information

Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2020, No. 4, pp. 65 - 71.

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Petunin, V.I., Neugodnikova, L.M. Method of Improving the Noise Resistance of Automatic Control Systems. Russ. Aeronaut. 63, 627–634 (2020). https://doi.org/10.3103/S1068799820040091

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.3103/S1068799820040091

Keywords

Navigation