1. A spacecraft has two attitude sensors, sensing two unit vectors (directions), v, with i = 1, 2. We know the first sensor (2=1) is more accurate than the second sensor. At an instant in time, the two vectors measured by the 0.8273 -0.8285 sensors have the body frame components: 50 = 0.5541 0.5522 0.0920 -0.0955 At the same time, the four vectors are determined to have inertial frame components: -0.1517 -0.8393 NV1 -0.9669 0.4494 0.2050 0.3044 Use the Triad Method to determine the estimated attitude [B/V]. Be sure to normalize all the provided unit vectors. Enter a response with at least 5 significant digits. # adjust the return matrix values as needed def result( ): don = [0, 6, 0. 0, 0, 0, 0, 6, 0] return dom Run Reset