The initial (3-2-1) Euler angles yaw, pitch and roll of a vehicle are (1), 0, 0) = (40, 30, 80) degrees. Assume the body angular velocity vector of the craft is given through the B frame components as Bw= sin(0.1t)] 0.01 20deg/s. Write a program to numerically integrate the yaw, pitch and roll angles over [cos(0.1t). a simulation time of 1 minute. Enter the Euler angle norm √№2 +0² + 02 at the simulation time step 42s. Express angles in radians. Let the initial angles integrate, don't wrap them to any particular quadrants.

The initial (3-2-1) Euler angles yaw, pitch and roll of a vehicle are (1), 0, 0) = (40, 30, 80) degrees. Assume the body angular velocity vector of the craft is given through the B frame components as Bw= sin(0.1t)] 0.01 20deg/s. Write a program to numerically integrate the yaw, pitch and roll angles over [cos(0.1t). a simulation time of 1 minute. Enter the Euler angle norm √№2 +0² + 02 at the simulation time step 42s. Express angles in radians. Let the initial angles integrate, don't wrap them to any particular quadrants.