P 5.7 Astronaut Bruce McCandless II took the first untethered walk-in space on February 7, 1984, using the gas-jet propulsion device illustrated in Figure P5.7(a). The controller can be represented by a gain K2, as shown in Figure P5.7(b). The moment of inertia of the equipment and astronaut is I = 25 kg.m². (a) Determine the necessary gain K3 to maintain a steady-state error equal to 1 cm when the input is a unit ramp. (b) With this gain K3, determine the necessary gain K,K2 in order to restrict the percent overshoot to P.O.<10.

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Chapter1: Units, Trigonometry. And Vectors
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P5.7 Astronaut Bruce McCandless II took the first untethered walk-in space on February 7, 1984, using
the gas-jet propulsion device illustrated in Figure P5.7(a). The controller can be represented by a gain
K2, as shown in Figure P5.7(b). The moment of inertia of the equipment and astronaut is I= 25 kg.m?.
(a) Determine the necessary gain K3 to maintain a steady-state error equal to 1 cm when the input is a
unit ramp. (b) With this gain K3, determine the necessary gain KIK2 in order to restrict the percent
overshoot to P.O.310.
Transcribed Image Text:P5.7 Astronaut Bruce McCandless II took the first untethered walk-in space on February 7, 1984, using the gas-jet propulsion device illustrated in Figure P5.7(a). The controller can be represented by a gain K2, as shown in Figure P5.7(b). The moment of inertia of the equipment and astronaut is I= 25 kg.m?. (a) Determine the necessary gain K3 to maintain a steady-state error equal to 1 cm when the input is a unit ramp. (b) With this gain K3, determine the necessary gain KIK2 in order to restrict the percent overshoot to P.O.310.
Gas jet
Astronaut
controller
R(s)
Force 1 Velocity
Is
Position
Desired
K1
K2
(meters)
position
K3
Transcribed Image Text:Gas jet Astronaut controller R(s) Force 1 Velocity Is Position Desired K1 K2 (meters) position K3
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