Project 1: A device for simulating conditions in space allows rotations abou; thre orthogonal axes as illustrated in the figure. At this instant, the astronaut is moving as shown with a velocity v= 5.0 fVsec and an acceleration a= 32.0 fisec?, both relative to the capsule. Use the method of multiple- rotating-coordinase systems, with at least two rotating coordinate systems, to determine for the instant pictured: (a) the inertial velocity of the astronaut's head; (b) the inertial acceleration of the astronaut's hoad: given the data in the figures. v, - 5.0 ft/sec a = 32.0 t/sec ca = 3.0 rad/sec a, = 0.0 rad/sec i, = 2.0 rad/sec @, 4.0 rad /sec a, = 5.0 rad/sec a = 6.0 rad/sec

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: O l 1
Project 1:
A device for simulating conditions in space allows rotations abou; three orthogonal axes as
ilustrated in the figure.
At this instant, the astronäut is moving as shown with a velocity v, = 5.0 f/sec and
an accelerntion ar= 32.0 /sec?, bodh relative to the cupsule. Use thie method of multiple-
rotating-coordinare systems, with at least two rotating coordinate systems, to determine
for the instant picturod:
(a) the inertial velocity of the astronaut's head;
(b) the inertial acceleration of the astronaut's hoead:
given the data in the figures.
a, = 32.0 ft/sec
ca = 3.0 rad/sec
ci, = 0.0 rad/sec
cà, - 2.0 rad/sec
v, = 5.0 t/sec
0, = 4.0 rad/sec
a, = 5.0 rad /sec
a, = 6.0 rad/sec
10 f-
2 fi
Assume that the astronaut is canstant relative to Capsule
Plot the components of his acceleratien in body frame xyz
in terms of wi Wg"
Transcribed Image Text:: O l 1 Project 1: A device for simulating conditions in space allows rotations abou; three orthogonal axes as ilustrated in the figure. At this instant, the astronäut is moving as shown with a velocity v, = 5.0 f/sec and an accelerntion ar= 32.0 /sec?, bodh relative to the cupsule. Use thie method of multiple- rotating-coordinare systems, with at least two rotating coordinate systems, to determine for the instant picturod: (a) the inertial velocity of the astronaut's head; (b) the inertial acceleration of the astronaut's hoead: given the data in the figures. a, = 32.0 ft/sec ca = 3.0 rad/sec ci, = 0.0 rad/sec cà, - 2.0 rad/sec v, = 5.0 t/sec 0, = 4.0 rad/sec a, = 5.0 rad /sec a, = 6.0 rad/sec 10 f- 2 fi Assume that the astronaut is canstant relative to Capsule Plot the components of his acceleratien in body frame xyz in terms of wi Wg"
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