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Unformatted text preview: gravity vector in body-fixed coordinates. Problem 3 Find the quaternions that result in the following B2L transformation matrix. T B2L = [ 0.66 0.49 0.56 0.66 0.73 0.14 0.34 0.47 0.81 ] Problem 4 Estimate and plot the Euler angle time histories using the rate gyro data provided on the class website. Numerically integrate the angular rate differential equations using both the Euler and quaternion formulations. Assume the Euler angles are initially set to zero. 1...
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This note was uploaded on 01/18/2012 for the course MAE 142 taught by Professor Aliseda,a during the Spring '08 term at UCSD.
- Spring '08