Skip to main content
Log in

Possibilities of Using the Angular Navigation Equipment for Space Rockets

  • Flight Dynamics and Control of Flight Vehicles
  • Published:
Russian Aeronautics Aims and scope Submit manuscript

Abstract

The paper discusses the possibilities of using the navigation user equipment on the basis of determining the angular position of space rockets in flight taking into account the special features of the control process. The task statement is given on clarifying the angular position on the active trajectory leg and identifying the abnormal operation of the meters of inertial navigation systems on the inactive trajectory leg of the space rockets using navigation user equipment. Methodological ways for solving the tasks are proposed and substantiated.

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.

Institutional subscriptions

Similar content being viewed by others

References

  1. Baerdecker, G., Accurate Determination of Aircraft Orientation Using Multi-Antenna GPS Receivers, Giroskopiya i Navigatsiya, 2008, no. 4, pp. 21–26.

    Google Scholar 

  2. Chernov, V.Yu., Flight Control Algorithm for Gyroplatform of the Inertial Navigational System, Izv. Vuz. Av. Tekhnika, 2005, vol. 48, no. 1, pp. 51–55 [Russian Aeronautics (Engl. Transl.), vol. 48, no. 1, pp. 74–80].

    Google Scholar 

  3. Konovalov, V.P., Makatrov, A.S., Bogdanov, S.A., Gerastovskii, V.F., Kutsevalov, A.T., and Chaplinskii, V.S., Securing Global and Operative Control and Direction of Upper-Stage Rockets of a Space Craft, Izv. Vuz. Privolzhskii Region. Tekhnicheskie Nauki, 2013, no. 2, pp. 130–139.

    Google Scholar 

  4. Inertial Control System, URL: https://bigenc.ru/technology_and_technique/text/2001368#.

  5. Bogachev, S.A., Kozlov, V.V., and Skripnikov, A.N., The Use of Satellite Navigation Equipment to Control the Angular Position of Accelerated Blocks, Trudy 15i vsepossiiskoi nauchno-prakticheskoi konferentsii RARAN (Proc. 15th All-Russia Sc.-Practical Conf. of the Russian Academy of Rocket and Artillery Sciences (RARAN)), St. Petersburg: NPO SM, 2012, pp. 445–449.

    Google Scholar 

  6. Evstifeev, M.I. and Chelpanov, I.B., Improving Mechanical Performance of MEMS Gyros, Giroskopiya i Navigatsiya, 2013, no. 1, pp. 119–133 [Gyroscopy and Navigation (Engl. Transl.), 2013, vol. 4, no. 3, pp. 174–180].

    Google Scholar 

  7. Peshekhonov, V.G., Gyroscopic Systems: Current Status and Prospects, Giroskopiya i Navigatsiya, 2011, no. 1, pp. 3–16 [Gyroscopy and Navigation (Engl. Transl.), 2011, vol. 2, no. 3, pp. 111–118].

    Google Scholar 

  8. Averkiev, N.F., Vlasov, S.A., Salov, V.V., and Kiselev, V.V., Route Optimization of the Aircraft Flight, Izv. Vuz. Av. Tekhnika, 2016, vol. 59, no. 3, pp. 22–27 [Russian Aeronautics (Engl. Transl.), vol. 59, no. 3, pp. 474–479].

    Google Scholar 

  9. Poplevin, A.S., Motion Control of the Accelerated Blocks According to the Navigation Information of the Satellite Navigation System, Vestnik Samarskogo Universiteta, 2010, no. 2, pp. 191–197.

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to A. N. Skripnikov.

Additional information

Russian Text © The Author(s), 2020, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2020, No. 1, pp. 33–39.

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Averkiev, N.F., Bogachev, S.A. & Skripnikov, A.N. Possibilities of Using the Angular Navigation Equipment for Space Rockets. Russ. Aeronaut. 63, 33–40 (2020). https://doi.org/10.3103/S1068799820010055

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.3103/S1068799820010055

Keywords

Navigation