L _ r rolling moment resulting from sideslip induced yaw rate.
2.
However, the usual hazard is associated with induced rolling moments.
3.
If the contents of one tank is significantly different to the other you have a rolling moment.
4.
Dihedral effect of an aircraft is a rolling moment resulting from the vehicle having a non-zero angle of sideslip.
5.
These opposing rolling moment effects have to be overcome by the aileron input in order to sustain the roll rate.
6.
When the torpedo tilted, the anti-rolling controller steers roll-rudders ( or ailerons ) in twisting ailerons manner to produce counter-rolling moment.
7.
Due to the circulation control effect of vectored thrust, a substantial rolling moment can be produced with very little control input.
8.
These other effects are called " rolling moment due to yaw rate " and " rolling moment due to sideslip rate " respectively.
9.
These other effects are called " rolling moment due to yaw rate " and " rolling moment due to sideslip rate " respectively.
10.
Yaw increases the speed of the outboard wing whilst reducing speed of the inboard one, causing a rolling moment to the inboard side.
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