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14     Bu il d  Y o ur  O w n  Q u a d c o p t e r






















                             Figure 2.1  Wright 1903 Flyer shown with flight forces. (Courtesy of NASA)


                             center-of-gravity concept. CG can be thought of as an imaginary point within an aircraft
                             where it could be suspended in a perfectly balanced position. In the real world, a CG point
                             is used to determine if an aircraft is stable; if the entire payload including the airframe, fuel,
                             passengers, and cargo is within prescribed design limits; and consequently, if the aircraft is
                             safe to fly. A quadcopter CG may be thought of as the point within the copter where a string
                             could be attached to suspend it in a perfectly balanced state. Naturally, one would expect the
                             CG to be collocated with the physical center of the quadcopter. If the CG is located off center,
                             it would tend to make the quadcopter unstable, perhaps to the point of being uncontrollable
                             if it were located too far from the physical center. This is always something to consider when
                             attaching devices to the quadcopter. For instance, attaching a camera module close to the
                             outboard side of a motor boom, which might make sense for a better field of view, would
                             probably upset the CG to the detriment of the quadcopter flight stability.

                             Flight Axes
                             In order to fully understand airplane flight dynamics, it is necessary to discuss three physical
                             axes and the three rotations associated with those axes. Figure 2.2 shows a light general-
                             aviation (GA) airplane with its longitudinal axis running fore and aft through the fuselage.
                             The lateral axis is perpendicular and in the same plane as the longitudinal axis and runs
                             through the wing, intersecting with the longitudinal axis at the CG. The third axis, called the
                             vertical axis, is perpendicular to the other two and also goes through the CG. The three


                               Force     Description
                               Weight    The downward force acting upon the aircraft due to Earth’s gravity.
                               Lift      The upward force created by the rapid passage of air over and under the airfoil
                                         (wing).
                               Thrust    The forward force created by the rotating propeller pushing air backward.
                               Drag      The backward force created by wind resistance due to the fuselage shape and
                                         non-streamlined appendages.

                             Table 2.1  Four Aerodynamic Flight Forces
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