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Problems for Chapter I Problem 1.1 Consider the Conservation of Linear Momentum Equations (CLMEs) with respect to the body axes X Y Z , , :             X X Y Y Z Z X A T Y A T Z A T m U QW RV m g F F m V UR PW m g F F m W PV QU m g F F  ï€ ï€½    ï€ ï€½    ï€ ï€½   Rewrite the above equations under the following conditions: - constant pitching maneuver (loop in the XZ plane); - constant rolling around the X axis; - steady-turning at constant altitude (with ailerons and rudder maneuver). Solution of Problem 1.1 Constant Pitching Maneuver Figure P1.1 shows a constant pitching maneuver.
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