Make a reorientation maneuver to a stable attitude. The spacecraft has the inertia J:6400 -76.4 -25.6]J-76.4 4730 -40 kg-m²-25.6 -40 8160(2)The initial quaterion is w(to) = √√2/2[10017], the initial angular velocity is. The desiredquaternion is the unit quaternion. The initial wheel momentum is w(to) = [0.01 0.01 0.017]rad/s. The gains are set to kp = 10 and k₁ = 150.(a) compare two different suitable control laws. Justify your choices.(b) compare two different wheel configurations, compare the pseudo-inverse with theminimax law in terms of wheel momenta and wheel speeds (state your assumptions).

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Answered: Make a reorientation maneuver to a…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

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