Consider a rigid aircraft observed by optical sensors giving the inertial velocities of the mass center and right wing tip points Vem and Vrwt indicated below. Position of the right wing tip relative to the mass center Frwt/cm is also known and indicated below. Vem Vwt = 74î – 21ĵ + 68k ft/s = 100î – 10ĵ + 10k ft/s %3D řrwt/cm = -2î + 10ĵ + 1k ft Compute aircraft angular velocity vector (in units of rad/s) when the angular velocity vector
Consider a rigid aircraft observed by optical sensors giving the inertial velocities of the mass center and right wing tip points Vem and Vrwt indicated below. Position of the right wing tip relative to the mass center Frwt/cm is also known and indicated below. Vem Vwt = 74î – 21ĵ + 68k ft/s = 100î – 10ĵ + 10k ft/s %3D řrwt/cm = -2î + 10ĵ + 1k ft Compute aircraft angular velocity vector (in units of rad/s) when the angular velocity vector
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