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).

Answered: Image /qna-images/answer/645f63c1-7354-493f-a5f1-403ec01f1b35.jpg

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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-10 10 40 a. Find the volume of the parallelepiped whose edges are represented by A = 2i - 3j + 4k, ii. B = 1+ 2) - k, C = 31 - 1 + 2k . b. The angular velocity of a rotating rigid body about an axis of rotation is given by ai = 4i +j - 2k. Find the linear velocity of a point P on the body whose position vector relative to a point on the axis of rotation is 2i-3j+k. ii. Find the moment of inertia tensor from the given picture. 300 mm P.T.O. iv. Given point P = (1, -2, 3) and vector A = yz i+x1- yx k , express this vector in cylindrical coordinate system. V. a. Show that the contraction of the outer product of the tensors AP and B, is an invariant. b. Show that every tensor can be expressed as the sum of two tensors, one of which is symmetric and the other skew-symmetric in a pair of covariant or contra variant indices. vi. The 4-oz top with radius of gyration about its spin axis of 0.62 in. is spinning at the rate p = 3600 rev/min in the sense shown, with its spin axis making an angle…
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