The Colombian company Advector is developing a UAS (Unmanned Aircraft System) for surveillance and control tasks. The distribution of components and systems within the aircraft structure is essential to ensure that the center of gravity is within the limits defined in the stability and control analysis. Decide:

Determine the weight of the aircraft with all systems installed and the position of the center of gravity for the preliminary distribution shown in Table 1. (0.5 points).

If the center of gravity is outside the limits, how far and in what direction must you move the batteries and the TX + Antenna video so that the center of gravity is within range? Consider the maximum distances that these two components can move. (1.0 points)

Center of gravity limits: 36.0 - 36.8 cm

Battery travel limits: 4 cm forward, 1 cm back.

Video TX + Antenna Scroll Limits: 12cm forward, 5cm back.

Table 1. Preliminary list of components and systems position

item Structure AP + Accesories Modem + Antenna Video TX + Antenna GPS Arm (cm) Weight (grf) Moment 47.2 2047 38.7 158 62 67 82 137 50 36 52 92 FLIR Gimbal Batt 440 10.2 30 TOTAL 1740