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Consider the UAV carrying out a sequence of longitudinal and turning coordinated flight maneuvers defined by a sequence of waypoints described below. The total time of
flight is sufficiently short that the weight of the UAV can be assumed to be a constant 45 lbs and the air density during the flight can be assumed to be constant. The
specified waypoints are defined with respect to a ground-fixed frame: the x and y axes are in a horizontal plane located at an altitude of 1,000 ft with the x-axis
pointing due east and the y-axis pointing due north; the z-axis defines the altitude above this horizontal plane.

The aircraft should be in steady climbing flight between waypoints 1 and 2; it should be in steady level turn between waypoints 2 and 3, and it should be in steady
descending flight between waypoints 3 and 4.
a) Select a flight plan for which the elapsed time from waypoint 1 to waypoint 4 is near minimum. Your flight plan should specify the constant airspeed, the constant
climb rate, and the bank angle for each of the three steady flight segments that satisfy the waypoint specifications.
(b) For each of the steady flight segments constructed in part (a), determine the elevator deflection and the throttle setting that guarantee the desired steady flight
conditions along that flight segment. Check that all flight constraints are satisfied for all steady flight segments.
(c) What is the elapsed flight time from waypoint 1 to waypoint 4(d) On the basis of your flight plan in part (a), give plot(s) that describe the 3D path of the
aircraft.

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