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Modeling the motion of an uncompensated gyrostabilized platform in the Rodrigues-Hamilton parameters

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  • Flight Dynamics and Control of Flight Vehicles
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Abstract

We construct a model of triaxial gyrostabilizer platform motion at the force stabilization regime. The Rodrigues-Hamilton parameters have been chosen as kinematic parameters describing the changes in the gyrostabilized platform state vector. The advantages of using the model constructed in the initial attitude control systems of inertial navigation systems as compared with the existing ones are shown.

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Authors and Affiliations

  1. Rostov Military Institute of Rocket Forces, Rostov-on-Don, Russia

    V. A. Pogorelov, E. G. Chub & K. Yu. Yakovlev

Authors
  1. V. A. Pogorelov
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  2. E. G. Chub
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  3. K. Yu. Yakovlev
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Additional information

Original Russian Text © V.A. Pogorelov, E.G. Chub, K.Yu. Yakovlev, 2012, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2012, No. 3, pp. 69–72.

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Pogorelov, V.A., Chub, E.G. & Yakovlev, K.Y. Modeling the motion of an uncompensated gyrostabilized platform in the Rodrigues-Hamilton parameters. Russ. Aeronaut. 55, 315–319 (2012). https://doi.org/10.3103/S1068799812030154

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  • DOI: https://doi.org/10.3103/S1068799812030154

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