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Conceptual Design Requirements of a Newly Developed UAV as a ...

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electronics avails higher performance and lower weights sensors, camer<strong>as</strong> and processors.<br />

As shown in Figure 2, compared to conventional <strong>UAV</strong>'s, the payload-to-gross weight ratio<br />

% Payload/gross Weight<br />

70<br />

60<br />

50<br />

40<br />

30<br />

20<br />

10<br />

PAYLOAD vs Endurance<br />

0<br />

3 4 5 6 7 8 9 10<br />

Endurance (h)<br />

Figure 2: Payload vs Endurance <strong>of</strong> available Known Conventional<br />

<strong>UAV</strong>’s ( 4)<br />

Ceiling (feet)<br />

80,000<br />

70,000<br />

60,000<br />

50,000<br />

40,000<br />

30,000<br />

20,000<br />

10,000<br />

Present <strong>UAV</strong><br />

Service ceiling <strong>of</strong> <strong>UAV</strong>'s<br />

0<br />

0 10 20 30 40 50 60<br />

Endurance (h)<br />

Present <strong>UAV</strong><br />

Figure 3: Ceiling vs. Endurance <strong>of</strong> available Known Conventional<br />

<strong>UAV</strong>’s 4<br />

is average, however the endurance places the present <strong>UAV</strong> among the top <strong>of</strong> the group 4 .<br />

The ceiling is among the majority <strong>of</strong> <strong>UAV</strong>’s <strong>of</strong> its endurance category, Figure 3.<br />

4<br />

SSAS <strong>UAV</strong> Scientific Meeting & Exhibition, Jeddah, Saudi Arabia (June 6, 2006)<br />

Paper No. SSAS-2006-051

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