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• W2141674752 abstract "A nonlinear-optimal control strategy is devised using Hamilton-Jacobi formulation for tracking attitude maneuvers of rigid- asymmetric spacecraft. The exact motion model employs kinematical representation by the modified Rodrigues parameters (MRP) for large principal rotations. For tracking a constant attitude trajectory, an infinite-horizon optimal control problem is posed, wherein nonlinear feedforward and feedback control torques minimize a performance index with a quadratic control cost and a fourth-order attitude and angular-velocity error cost. Closed-form solution is obtained employing a Lyapunov function of the same form as the error cost, and by solving the Hamilton-Jacobi equation. Numerical results are presented for a practical tracking case with arbitrarily large initial conditions and desired state." @default.
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• W2141674752 date "2004-09-01" @default.
• W2141674752 modified "2023-10-17" @default.
• W2141674752 title "Optimal Nonlinear Tracking of Spacecraft Attitude Maneuvers" @default.
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• W2141674752 doi "https://doi.org/10.1109/tcst.2004.825060" @default.
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