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Mathematical Problems in Engineering
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Special Issues
Mathematical Problems in Engineering
/
2015
/
Article
/
Tab 1
/
Research Article
Trajectory Optimization for a Cruising Unmanned Aerial Vehicle Attacking a Target at Back Slope While Subjected to a Wind Gradient
Table 1
Other parameters of loiter munition and environmental parameters.
Parameters
Values
(kg)
1.8
(m
2
)
0.1
(kg/m
3
)
1.23
0.08258
ā0.176
0.312
(m)
2000