The following evaluation criteria were found:
- small size/weight (requirement of movable
structure)
- low material costs
- low energy consumption
-
easy assembly
- operational safety (especially no entanglement of
the string in the rotors of the drone)
Ranking
| |
low
weight |
low material
cost |
low energy
consum-ption |
easy assembly |
Opera
tional
safety |
"+"
Number |
Ranking |
low
weight |
0 |
- |
- |
+ |
- |
1 |
4 |
| low material
cost |
+ |
0 |
- |
+ |
- |
2 |
3 |
| low energy
consum-ption |
+ |
+ |
0 |
+ |
- |
3 |
2 |
| easy assembly |
- |
- |
- |
0 |
- |
0 |
5 |
Opera
tional safety |
+ |
+ |
+ |
+ |
0 |
4 |
1 |
"-"
Number |
1 |
2 |
3 |
0 |
4 |
|
|
Aufstellung der
Gewichte über die Anzahl der erreichten "+"- Punkte
The criteria weight is formed by
normalizing the "+" awarded to the "+" accounted for per criterion
(quotient
formation). Rounding to two decimal places (percent).
Evaluation criterion
|
"+" Number
|
Weight
|
| low weight |
1 |
0,2 |
| low material
cost |
2 |
0,3 |
|
low energy consumption |
3 |
|
| easy assembly |
0 |
0,1 |
|
operational safety |
4 |
0,3 |
Result
|
|
1 |
|
