A satellite's positioning system is often modelled as the transfer function of its angular position over the input torque due to its thruster, G (s) = . Which of the following statements is not correct? O Without a controller, the satellite position demonstrates a parabolic trajectory if a constant input torque is applied. O The system has two poles at the origin, s%3D0. O With a unity feedback configuration, the satellite position demonstrates a parabolic trajectory if a constant input torque is applied. O The system is marginally stable.

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A satellite's positioning system is often modelled as the transfer function of its angular position over
the input torque due to its thruster, G (s) = . Which of the following statements is not correct?
O Without a controller, the satellite position demonstrates a parabolic trajectory if a constant input torque is
applied.
O The system has two poles at the origin, s%3D0.
O With a unity feedback configuration, the satellite position demonstrates a parabolic trajectory if a constant
input torque is applied.
O The system is marginally stable.
Transcribed Image Text:A satellite's positioning system is often modelled as the transfer function of its angular position over the input torque due to its thruster, G (s) = . Which of the following statements is not correct? O Without a controller, the satellite position demonstrates a parabolic trajectory if a constant input torque is applied. O The system has two poles at the origin, s%3D0. O With a unity feedback configuration, the satellite position demonstrates a parabolic trajectory if a constant input torque is applied. O The system is marginally stable.
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