QB3c. A satellite is moving with the constant angular velocity (see sketch below) and its displacement projected onto the vertical line PN is S. Write down an expression for the displacement S as function of time t if the starting point of the motion is at W, the radius of the satellite's orbit is R and its rotational frequency is f. Please use appropriate algebraic symbols for multiplication (* for a × b), division (/ for a/b), exponents (a^b for a³), square root (sqrt(a*b/c) for √ax b/c) etc. For Greek letters use their names e.g. "theta", "alpha", "pi", "mu" (without the quotes) and for trigonometric functions use "cos", "tan", "sin" (without the quotes). Thus for Acoso use A*cos theta. Please use the "Display response" button to check you entered the answer you expect. S N A P Satellite R W

QB3c. A satellite is moving with the constant angular velocity (see sketch below) and its displacement projected onto the vertical line PN is S. Write down an expression for the displacement S as function of time t if the starting point of the motion is at W, the radius of the satellite's orbit is R and its rotational frequency is f. Please use appropriate algebraic symbols for multiplication (* for a × b), division (/ for a/b), exponents (a^b for a³), square root (sqrt(ab/c) for √ax b/c) etc. For Greek letters use their names e.g. "theta", "alpha", "pi", "mu" (without the quotes) and for trigonometric functions use "cos", "tan", "sin" (without the quotes). Thus for Acoso use Acos theta. Please use the "Display response" button to check you entered the answer you expect. S N A P Satellite R W

Classical Dynamics of Particles and Systems

5th Edition

ISBN:9780534408961

Author:Stephen T. Thornton, Jerry B. Marion

Publisher:Stephen T. Thornton, Jerry B. Marion

Chapter10: Motion In A Noninertial Reference Frame

Section: Chapter Questions

Problem 10.20P: Calculate the effective gravitational field vector g at Earths surface at the poles and the equator....

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