Application of information criteria to control the structurally uncertain navigation system of a reusable spacecraft

Details Application of information criteria to control the structurally uncertain navigation system of a reusable spacecraft Application of information criteria to control the structurally uncertain navigation system of a reusable spacecraft

Feb 2009

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2009cosre..47...44p&link_type=abstract

Cosmic Research, Volume 47, Issue 1, pp.44-52

Physics

95.10.Eg

Scientific paper

The problem of attitude control of a gyro-stabilized platform with the structurally uncertain drift model is solved. The solution is realized in two stages. At the first stage, on the basis of the obtained stochastic model of the reusable spacecraft navigation system, the drift model of gyro-stabilized platform is identified. At the second stage, the control of its spatial orientation is synthesized with regard to the found drift model. The results of numerical simulation are presented in conclusion.

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