Unloading angular momentum for inertial actuators of a spacecraft in the pitch channel

DOI10.1134/S1064230711030075zbMath1272.93056OpenAlexW2007421990MaRDI QIDQ357805

N. E. Zubov, A. V. Bogachev, S. N. Timakov, E. A. Mikrin, V. N. Ryabchenko, E. A. Vorob'eva, M. Sh. Misrikhanov

Publication date: 13 August 2013

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230711030075

Mathematics Subject Classification ID

Design techniques (robust design, computer-aided design, etc.) (93B51) Variable mass, rockets (70P05)

Related Items (7)

Synthesis of spacecraft covariance controls ⋮ Reduction of large-scale dynamical systems by the Krylov subspaces method: analysis of approaches ⋮ Methods for suppressing nonlinear oscillations in astatic auto-piloted aircraft control systems ⋮ Terminal synthesis of orbital orientation for a spacecraft ⋮ Synthesis of decoupling laws for attitude stabilization of a spacecraft ⋮ Algorithms for the synthesis of observers for nonlinear dynamic systems ⋮ Schemes of momentum/reaction wheels unloading by mechanical restructuring and gearbox for spacecraft

Cites Work

• Stabilization of a wheels carrying communication satellite without angle and angular velocity sensors
• Momentum unloading excessive reaction-wheel system of a spacecraft
• The band formula for A.N. Krylov's problem

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