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The input to the satellite system of Figure 1 is a step function θc(t) = 5u(t) in degrees. As a result, the satellite angle θ(t) varies sinusoidally at a frequency of 10 cycles per Minute. Find the ratio of the amplifier gain K and the moment of inertia J for the system, assuming that the units of time in the system Differential equation are seconds.
Figure: Satellite control system
example
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#question ...THE APPLICATION AND OPERATION OF ZENER DIODES
Explain in detail the operation of 8255 in mode1 taking suitable example. In mode1, Ports A and B are programmed as input or output ports and Port C is used for handshaking.
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