annas425
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Homework Statement
I am given the following dynamic system. I want to find the transfer function, θ1(s)/T(s).
The main body of the satellite, J1, acts like a large mass flying through space; space is essentially without friction and therefore no damping is imparted on the main body. The solar collector array acts like a second order underdamped system attached to the satellite, adding second order underdamped modes to the system. The satellite has thrusters that can impart a torque T(t) on the satellite main body; attitude θ1(t) can be measured; gravity from nearby planets is negligible about the axis of rotation; the structure attaching the main body to the solar collector acts as a torsional spring k and torsional damper b.
T(s) is the plant input, and θ1(s) is the plant output.
Homework Equations
Newton's 2nd Law (F=ma)
Laplace Transform?
The Attempt at a Solution
I came up with the following two equations (which I believe describe each body in the above dynamic system):
J1*θ1''(t) = -b*[θ1'(t) - θ2'(t)] - k*[θ1(t) - θ2(t)] + T(t)
J2*θ2''(t) = -b*[θ2'(t) - θ1'(t)] - k*[θ2(t) - θ1(t)]
As you can see, these are in the time domain (where θ''(t) = a(t), the second derivative of position; θ'(t) = v(t), the first derivative of position). I am unsure how to now get the transfer function from these equations (and in turn get these into the frequency domain). The transfer function is θ1(s)/T(s).
Should I take the Laplace Transform of the two equations? I am sure there is something else I am missing. Any light shed on this is GREATLY appreciated! Have a nice day :)