�The space shuttle�consists of multiple�subsystems. Can you identify those that are control systems, or parts of control systems?
© NASA-Houston.
�Components of a block diagram for�a linear, �time-invariant�system
�a. Cascaded�subsystems;�b. equivalent transfer�function
�Loading in cascaded�systems
�a. Parallel�subsystems;�b. equivalent�transfer�function
�a. Feedback control�system;�b. simplified model;�c. equivalent transfer�function
�Block diagram�algebra for summing�junctions—�equivalent forms for moving a block�a. to the left past a�summing junction;�b. to the right past a�summing junction
�Block diagram algebra for pickoff points—�equivalent forms for moving a block�a. to the left past a pickoff point;�b. to the right past a pickoff point
�Block diagram�
�Steps in solving�Example 5.1:�a. collapse summing�junctions;�b. form equivalent�cascaded system�in the forward path�and equivalent�parallel system in the�feedback path;�c. form equivalent�feedback system and�multiply by cascaded�G1(s)�
�Block diagram
�Steps in the �block diagram �reduction
�Steps in the �block diagram �reduction
�Steps in the �block diagram �reduction
�Steps in the �block diagram �reduction
�Steps in the �block diagram �reduction
�Steps in the �block diagram �reduction
�Block diagram for�Skill-Assessment�Exercise
�Second-order�feedback control�system
�Feedback system
�Feedback system for�
�Signal-flow graph components:�a. system;�b. signal;�c. interconnection of systems and signals
�Building signal-flow�graphs:�a. cascaded system�nodes (from Figure 5.3(a));�b. cascaded system�signal-flow graph;�c. parallel system�nodes (from Figure 5.5(a));�d. parallel system�signal-flow graph;�e. feedback system�nodes (from Figure�5.6(b));�f. feedback system�signal-flow graph
�Signal-flow graph�development:�a. signal nodes;�b. signal-flow graph;�c. simplified signal-flow graph
�Signal-flow graph�for demonstrating�Mason’s rule
Loop Gain:-
Forward Path gain
Non-Touching loop gain
Mason Gain Formulae
�Forward Path gain���Loop Gains
�Non-Touching loops taking two at a time
�Non-Touching loops taking three at a time
�Stages of�development of a�signal-flow graph�for the system of�Eqs. 5.36:�a. place nodes;�b. interconnect�state variables and�derivatives;�c. form dx1/dt ;�d. form dx2/dt�(figure continues)
�(continued)�e. form dx3 /dt;�f. form output
�Representation of�Figure as�cascaded first-order�systems
�a. First-order subsystem;�b. signal-flow graph for Figure 5.23 system
�Signal-flow�representation
�Signal-flow�representation�
Figure 5.27�Signal-flow graphs for obtaining forms for�G(s) = C(s)/R(s) = (s2 + 7s + 2)/(s3 + 9s2 + 26s + 24):�a. phase-variable form;�b. controller canonical form
Control Systems Engineering, Fourth Edition by Norman S. Nise
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Figure 5.28�Signal-flow graph for observer canonical�form variables:�a. planning;�b. implementation
Control Systems Engineering, Fourth Edition by Norman S. Nise
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Figure 5.29�Feedback�control system�for Example 5.8
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Figure 5.30�Creating a signal-flow�graph for the�Figure 5.29 system:�a. forward transfer�function;�b. complete system
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Figure 5.31�State-space forms for�C(s)/R(s) =�(s+ 3)/[(s+ 4)�(s+ 6)].�Note: y = c(t)
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Figure 5.32�State-space�transformations
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Figure 5.33�To be an eigenvector,�the transformation Ax�must be collinear with�x; thus in (a), x is not�an eigenvector; in (b),�it is.
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Figure 5.34�Alvin, a manned�submersible,�explored the �wreckage of theTitanic with a tethered robot, Jason Junior.
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© Rob Catanach, Woods Hole Oceanographic Institution.
Figure 5.35�Block diagram�reduction for the�antenna azimuth�position control�system:�a. original;�b. pushing input�potentiometer to�the right past the�summing junction;�c. showing equivalent�forward transfer�function;�d. final closed-loop transfer function
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Figure 5.36�Signal-flow graph for�the antenna azimuth�position control�system
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Figure 5.37�Block diagram of�the UFSS vehicle’s�elevator and vehicle�dynamics, from which�a signal-flow graph�can be drawn
Control Systems Engineering, Fourth Edition by Norman S. Nise
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Figure 5.38�Signal-flow graph�representation of the�UFSS vehicle’s pitch-�control system:�a. without position and�rate feedback;�b. with position and�rate feedback�(Note: Explicitly�required variables are:�x1 = θ, x2 = dθ/dt,�and x4 =δe)
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Figure 5.39�Block diagram of the heading�control system for the UFSS�vehicle
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Figure P5.1�
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Figure P5-2 (p. 301)
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Figure P5.3�
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Figure P5.4�
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Figure P5.5�
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Figure P5.6�
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Figure P5-7 (p. 303)
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Figure P5.8�
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Figure P5.9�
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Figure P5.10�
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Figure P5.11�
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Figure P5.12�
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Figure P5.13�
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Figure P5.14�
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Figure P5.15�
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Figure P5.16�
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Figure P5.17�
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Figure P5.18�
Control Systems Engineering, Fourth Edition by Norman S. Nise
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Figure P5.19�
Control Systems Engineering, Fourth Edition by Norman S. Nise
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Figure P5.20
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Figure P5-21 (p. 307)
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Figure P5.22�
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Figure P5.23�
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Figure P5-24a (p. 309)
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Figure P5-24b (p. 310)
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Figure P5.25�
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Figure P5.26�
Control Systems Engineering, Fourth Edition by Norman S. Nise
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Figure P5.27�
Control Systems Engineering, Fourth Edition by Norman S. Nise
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Figure P5.28�
Control Systems Engineering, Fourth Edition by Norman S. Nise
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Figure P5.29�
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Figure P5.30�
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Figure P5.31�
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Figure P5.32�Space shuttle pitch�control system�(simplified)
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© 1988, Rockwell International.
Figure P5.33�AM modulator
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Figure P5.34�Feedback control system representing human eye movement
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Figure P5.35�a. HelpMate robot�used for in-hospital�deliveries;�b. simplified block�diagram for bearing�angle control
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Courtesy of Hank Morgan/Rainbow/PNI.
Figure P5.36�a. Load tester�(© 1992 IEEE);�b. approximate�block diagram
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Figure P5.37�Solenoid coil circuit
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Figure P5.38�a. Position control:�motor and load;�b. block �diagram
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Figure P5.39�a. Position control;�b. position control�with tachometer
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Figure P5.40�Position control
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Figure P5.41�a. Motor and load;�b. Motor and load in�feedback system
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