Problem 3: A cube-shaped spacecraft is in a circular Earth orbit. Let N (n,) be inertialand the spacecraft is denoted S (ŝ₁). The spacecraft is described such that¯½º = J ŝ₁ŝ₁ + J ŝ₂§₂ + J §¸Ŝ3Location of the spacecraft in the orbit is determined by the orbit-fixed unit vectors ê, thatare oriented by the angle (Qt), where is a constant angular rate.52€33>2t55ΛИзAt the instant when Qt = 90°, the spacecraft S is oriented relative to the orbit such that8₁ = 0°Space-three 1-2-3 angles 0₂ = 60°andES = $₂ rad/s0₁ = 135°(a) At this instant, determine the direction cosine matrix that describes the orientation ofthe spacecraft with respect to the inertial frame N.

Step 1: The problem provides us with the Space-three 1-2-3 angles, which are the angles between the…

Answered: Problem 3: A cube-shaped spacecraft is…

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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