Vector Analysis
1. An aircraft with mass 5000 kg is moving with a velocity vector [2t i +
50j + 30t2 k ] m/sec) about its own axis. The roll (P), pitch (Q) and yaw (R)
rates are 2, 0.5 and 0.1 rad/s respectively. Find the forces and acceleration
acting on the aircraft in the Earth's inertial axis. (Hint w(angular acceleration)= Pi + Qj + Rk is
the angular velocity which also affects the linear momentum
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