Synthesis of Attitude Control for a Gyroscopic Stabilizer of the Navigation System of a Descent Vehicle

Details Synthesis of Attitude Control for a Gyroscopic Stabilizer of the Navigation System of a Descent Vehicle Synthesis of Attitude Control for a Gyroscopic Stabilizer of the Navigation System of a Descent Vehicle

Sep 2001

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2001cosre..39..498s&link_type=abstract

Cosmic Research, v. 39, Issue 5, p. 498-503 (2001).

Computer Science

Scientific paper

The possibility to synthesize the attitude control for a gyrostabilized platform is investigated under the most general assumptions on its drifts, using the principle of maximum. The analytical form of the control vector, explicitly depending on all components of the state vector of a navigation system of a descent vehicle, is a specific feature of the found solution.

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