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