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The Scientific World Journal
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2015
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Article
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Tab 1
/
Research Article
Helicopter Control Energy Reduction Using Moving Horizontal Tail
Table 1
Flight dynamics modes comparison.
Mode (rad/s)
= 40 kts
= 80 kts
Padfield
Our model
Padfield
Our model
Padfield
Our model
1st
2nd
3rd
4th
5th
(Padfieldresults are taken from [
43
]).