发明名称 |
Method for shaping wing velocity profiles for control of flapping wing micro air vehicles |
摘要 |
A method of controlling wing position and velocity for a flapping wing air vehicle provides six-degrees-of-freedom movement for the aircraft through a split-cycle constant-period frequency modulation with wing bias method that generates time-varying upstroke and downstroke wing position commands for wing planforms to produce nonharmonic wing flapping trajectories that generate non-zero, cycle averaged wing drag and alter the location of the cycle-averaged center of pressure of the wings relative to the center of gravity of the aircraft to cause horizontal translation forces, rolling moments and pitching moments of the aircraft. |
申请公布号 |
US8700233(B1) |
申请公布日期 |
2014.04.15 |
申请号 |
US20100883317 |
申请日期 |
2010.09.16 |
申请人 |
DOMAN DAVID B.;OPPENHEIMER MICHAEL W.;THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE |
发明人 |
DOMAN DAVID B.;OPPENHEIMER MICHAEL W. |
分类号 |
B64C33/00 |
主分类号 |
B64C33/00 |
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