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411 समाचार
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411 REFERENCE · Wikibooks

LMIs in Control/Click here to continue/Applications of Linear systems/Mixed H2/Hinf LMI Satellite Attitude Control

Reference material by Wikibooks contributors. This retains its source identity and is not 411 news reporting.

The System Using the same formulation of the problem as in the H2 and Hinf feedback applications (linked below) the system is of the form: This formulation comes from the process described in Duan, page 371-373, steps 12.1 to 12.8. Tc and Td are the flywheel torque and the disturbance torque respectively. Ix, Iy, and Iz are the diagonalized inertias from the inertia matrix Ib. ω0 = 7.292115 x 10-5 rad/s is the rotational angular velocity of the Earth, and θ, Φ, and ψ are the three Euler angles. The LMI below utilizes the state space representation of the above system, which is described on the H2 and Hinf pages as well: Iab = Ia - Ib, Iabc = Ia - Ib - Ic , x = [q q']T , M = diag(Ix, Iy, Iz), zinf = 10-3 M q''', z2 = q These formulations are found in Duan, page 374-375, steps 12.10 to 12.15. The Data Data required for this problem include the moment of inertias and angular velocities of the system. Knowledge of expected disturbances d would be beneficial. The Optimization Problem There are two requirements of this problem: Closed-loop poles are restricted to a desired LMI region Where , L and M are matrices of correct dimensions and L is symmetric Minimize the effect of disturbance d on output vectors z2 and zinf. Design a state feedback control law u = Kx such that The closed-loop eigenvalues are located in , λ(A+BK) That the H2 and Hinf performance conditions below are satisfied with a small and : The LMI: Mixed H2/Hinf Feedback Control min s.t. trace(Z) < AX + B1W + (AX + B1W)T + BBT < 0 Gives a set of solutions to , and W, Z and X > 0, where is equal to . Conclusion Once the solutions are calculated, the state feedback gain matrix can be constructed as K = WX-1, and = Implementation This LMI can be translated into MATLAB code that uses YALMIP and an LMI solver of choice such as MOSEK or CPLEX. Related LMIs H2 LMI for Satellite Attitude Control Hinf LMI for Satellite Attitude Control External Links LMI Methods in Optimal and Robust Control - A course on LMIs in Control by Matthew Peet. - LMIs in Control Systems: Analysis, Design, and Applications - Duan and Yu