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Application of Cayley-Klein parameters in the problem of strapdown navigation system stochastic state vector synthesis for a self-contained space vehicle

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Abstract

The state vector and observer equations are obtained for a strapdown (gimballess) navigation system with three accelerometers, three angular rate sensors, and a barometric altimeter. These equations are based on the nonlinear filtration methods that ensure required estimation accuracy under arbitrary space maneuver of a vehicle.

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Authors and Affiliations

  1. Rostov Military Institute of Rocket Forces, Rostov, Russia

    V. A. Pogorelov

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  1. V. A. Pogorelov
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Original Russian Text © V.A. Pogorelov, 2008, published in Avtomatika i Telemekhanika, 2008, No. 8, pp. 48–55.

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Pogorelov, V.A. Application of Cayley-Klein parameters in the problem of strapdown navigation system stochastic state vector synthesis for a self-contained space vehicle. Autom Remote Control 69, 1311–1318 (2008). https://doi.org/10.1134/S0005117908080043

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  • DOI: https://doi.org/10.1134/S0005117908080043

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