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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Consider a rigid aircraft observed by optical sensors giving the inertial velocities of the mass
center and right wing tip points Vem and Vwt indicated below. Position of the right wing tip
relative to the mass center frwt/cm is also known and indicated below.
"TA
Viwt = 74î – 21j + 68k ft/s
Vem =
100î – 10j + 1ok ft/s
Frwt/cm = -2î + 10ĵ + 1k ft
Compute aircraft angular velocity vector (in units of rad/s) when the angular velocity vector
magnitude equals 502 rad/s.
Transcribed Image Text:Consider a rigid aircraft observed by optical sensors giving the inertial velocities of the mass center and right wing tip points Vem and Vwt indicated below. Position of the right wing tip relative to the mass center frwt/cm is also known and indicated below. "TA Viwt = 74î – 21j + 68k ft/s Vem = 100î – 10j + 1ok ft/s Frwt/cm = -2î + 10ĵ + 1k ft Compute aircraft angular velocity vector (in units of rad/s) when the angular velocity vector magnitude equals 502 rad/s.
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VIcm=100i^-10j^+10k^ ft/sVIrwt =74i^-21j^+68k^ ft/sVrwt/cm=-2i^+10j^+1k^ ft/swe know from kinematics relation that Vrwt=Vcm+Vrel+Vcm/wrt×ωω=xi^+yj^+zk^ rad/secVrel=0 (Rigid body kinematics)Vrwt=Vcm+0+Vcm/wrt×ωVrwt-Vcm=Vcm/wrt×ω      .......(i)74i^-21j^+68k^ -100i^-10j^+10k^ ft/s=y-10zi^-x+2zj^+2y+10xk^= -26i^-11j^+58k^ =y-10zi^-x+2zj^+2y+10xk^Therefore, y-10z=-26x+2z=112y+10x=58from equation (i) we have,-26i^-11j^+58k^=r×ω     , r=rcm/rwtω=262+112+58222+102+122x2+y2+z2=138735on solving equations y-10z=-26x+2z=112y+10x=58and x2+y2+z2=138735we get,x=19735y=67z=9435ω=19735i^+67j^+9435k^ rad/secω=19735i^+67j^+9435k^ ×180πdeg/sec=322.49 i^+49.11 j^+153.88 k^ deg/sec

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