Problem 1: Accelerometers' measurements obtained from an IMU unit strapped on an aircraft are[105 3] m/s2. The Euler angles are o = 15°, 0 = 30°, = 10°. Considering the fact that theaccelerometers measurements include components of the gravitational acceleration, find theacceleration of the aircraft.

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Description: Problem 1: Accelerometers' measurements obtained from an IMU unit strapped on an aircraft are[105 3] m/s2. The Euler angles are o = 15°, 0 = 30°, = 10°. Considering the fact that theaccelerometers measurements include components of the gravitational

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Problem 1: Accelerometers' measurements obtained from an IMU unit strapped on an aircraft are [105 3] m/s². The Euler angles are $ = 15°,0 = 30°, p = 10°. Considering the fact that the accelerometers measurements include components of the gravitational acceleration, find the acceleration of the aircraft.

Problem 1: Accelerometers' measurements obtained from an IMU unit strapped on an aircraft are [105 3] m/s². The Euler angles are $ = 15°,0 = 30°, p = 10°. Considering the fact that the accelerometers measurements include components of the gravitational acceleration, find the acceleration of the aircraft.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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