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Unloading angular momentum for inertial actuators of a spacecraft in the pitch channel. (English. Russian original) Zbl 1272.93056

J. Comput. Syst. Sci. Int. 50, No. 3, 483-490 (2011); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upr. 2011, No. 3, 132-139 (2011).
Summary: The problem of gravitational unloading of the angular momentum of inertial actuators of a spacecraft in the pitch channel for circular and elliptic orbits is considered using the band theory of modal control. Control laws for gravitational unloading and stabilization of a given spacecraft position unambiguously determined by the object parameters and given coefficients of characteristic equation are obtained.

MSC:

93B51 Design techniques (robust design, computer-aided design, etc.)
70P05 Variable mass, rockets
93B40 Computational methods in systems theory (MSC2010)
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References:

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