| http://www.w3.org/ns/prov#value | - These forces and moments can be deduced from measurements performed by measurement means such as accelerometers or strain gauges fixed on the structure, with the deformations thereof being measured; it implements an approximation by assuming that the fuselage of the helicopter is a rigid body presenting six degrees of freedom (whereas, in fact, the helicopter is a deformable body which is subjecte
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