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4. A solution-concentration mixer control system consists of three subsystems that are flow control...
3. A sinusoid eơt s or can be expressed as a sum of exponentials e" and e" with complex ncies s-o...
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3. A sinusoid eơt s or can be expressed as a sum of exponentials e" and e" with complex ncies s-o +yoo and s* -ju, Locate in the complex plane the complex frequencies of (10 points) the following signals: (a) e cos2t (e) 2 ut) -2t (b) e 3 (c) cos3t (d) e Complex numbers: - R034 1 n even (reje)" rkejke Trignometric Identities sin 2x=2sinxcosx sin2 x+cos2 x = 1 in 1-cos 2 cos2x=1 + cos2x sin(x±y)-sinxcosy±cos x...
3. (l’+2° +1²=4') Topic: Laplace transform, CT system described by differential equations, LTI system properties. Consider...
3. (l’+2° +1²=4') Topic: Laplace transform, CT system described by differential equations, LTI system properties. Consider a differential equation system for which the input x(t) and output y(t) are related by the differential equation d’y(t) dy(t) -6y(t) = 5x(t). dt dt Assume that the system is initially at rest. a) Determine the transfer function. b) Specify the ROC of H(s) and justify it. c) Determine the system impulse response h(t).
5. Consider a CT system with transfer function This system is called an integrutor because t by h...
the subject is in digital signal processing
5. Consider a CT system with transfer function This system is called an integrutor because t by he d to the ingent t y)-x(r)dr. Discretize the above system using the bilinear transform. (a) What is the transfer function H'(:) of the resulting DT system b) If xin] is the input and yin] is the output of the resulting DT system, write the (c) Obtain an expression for the frequency response H'(o) of the...
In this chapter, we introduced a number of general properties of systems. In particular, a system...
In this chapter, we introduced a number of general properties of
systems. In particular,
a system may or may not be
(1) Memoryless
(2) Time invariant
(3) Linear
(4) Causal
(S) Stable
Determine which of these properties hold and which do not hold for
each of the
following continuous-time systems. Justify your answers. In each
example, y(t) denotes
the system output and x(t) is the system input.
(b) y(t) [cos(31)]x(1) (c) y() = 13, x(T)dT x(t) + x(t - 2...
This is control system question. please answer all and show a clear step. Thank you! Question...
This is control system question. please answer all and
show a clear step. Thank you!
Question 3 Given the translational system shown in Figure 2, an input force, f(t) is applied to the mass, M, causing the dashpot which has a viscosity B and the spring, a stiffness coefficient of k, to compress with output displacement X(t). Input force, f(t) M O F Fixed point Displacement, X(t) Figure 2: A translational system (a) Derive the system's equation in terms of...
problem 7 Problem-4 [10 Points] Find the Laplace transforms of the functions in Figure. 2 Figure....
problem 7
Problem-4 [10 Points] Find the Laplace transforms of the functions in Figure. 2 Figure. 2: Triangular Function Problem-5 [10 Pointsl A system has the transfer function h(s) = (s1)(s +2) a) Find the impulse response of the system b) Determine the output y(t), given that the input is x(t) u(t) Problem-6 [10 Pointsl Use the Laplace transform to solve the differential equation +22+10v(t) 3 cos(2t) dt2 dt subject to v(0)-1, dv(O) Problem-7 [10 Points] Solve the integrodifferential equation...
The state space model of an interconnected three tank water storage system is given by the following equation -3 1 o 1[hi] dt The heights of water in the tanks are, respectively, hi, h2, hz. Each tan...
The state space model of an interconnected three tank water storage system is given by the following equation -3 1 o 1[hi] dt The heights of water in the tanks are, respectively, hi, h2, hz. Each tank has an independent input flow; the volume flow rates of input water into the three tanks are, respectively, qii,qi2, Oi3. Each tank also has a water discharge outlet and the volume flow rates of water coming out of the tanks are, respectively, qo1,...
The state space model of an interconnected three tank water storage system is given by the following equation: -3 1 0 1rh dt os lo 0 3] 10 1-3 The heights of water in the tanks are, respectively,...
The state space model of an interconnected three tank water storage system is given by the following equation: -3 1 0 1rh dt os lo 0 3] 10 1-3 The heights of water in the tanks are, respectively, h,h2,h3. Each tank has an independent input flow; the volume flow rates of input water into the three tanks are, respectively, qǐ1,W2,4a. Each tank also has a water discharge outlet and the volume flow rates of water coming out of the tanks...
2.7.5 The impulse response of a continuous-time LTI system is given by h(t) = f(t) -...
2.7.5 The impulse response of a continuous-time LTI system is given by h(t) = f(t) - et u(t). (a) What is the frequency response H (w) of this system? (b) Find and sketch H(w). (c) Is this a lowpass, bandpass, or highpass filter, or none of those? 2.7.6 The impulse response of a continuous-time LTI system is given by h(t) = S(t – 2). (This is a delay of 2.) (a) What is the frequency response H (w) of this...
Problem 4 (25%) Consider the attitude control system of a rigid satellite shown in Figure 1.1....
Problem 4 (25%) Consider the attitude control system of a rigid satellite shown in Figure 1.1. Fig. 1.1 Satellite tracking control system In this problem we will only consider the control of the angle e (angle of elevation). The dynamic model of the rigid satellite, rotating about an axis perpendicular to the page, can be approximately written as: JÖ = tm - ty - bė where ) is the satellite's moment of inertia, b is the damping coefficient, tm is...
Formuals:
3. A sinusoid eơt s or can be expressed as a sum of exponentials e" and e" with complex ncies s-o +yoo and s* -ju, Locate in the complex plane the complex frequencies of (10 points) the following signals: (a) e cos2t (e) 2 ut) -2t (b) e 3 (c) cos3t (d) e Complex numbers: - R034 1 n even (reje)" rkejke Trignometric Identities sin 2x=2sinxcosx sin2 x+cos2 x = 1 in 1-cos 2 cos2x=1 + cos2x sin(x±y)-sinxcosy±cos x...
3. (l’+2° +1²=4') Topic: Laplace transform, CT system described by differential equations, LTI system properties. Consider a differential equation system for which the input x(t) and output y(t) are related by the differential equation d’y(t) dy(t) -6y(t) = 5x(t). dt dt Assume that the system is initially at rest. a) Determine the transfer function. b) Specify the ROC of H(s) and justify it. c) Determine the system impulse response h(t).
the subject is in digital signal processing
5. Consider a CT system with transfer function This system is called an integrutor because t by he d to the ingent t y)-x(r)dr. Discretize the above system using the bilinear transform. (a) What is the transfer function H'(:) of the resulting DT system b) If xin] is the input and yin] is the output of the resulting DT system, write the (c) Obtain an expression for the frequency response H'(o) of the...
In this chapter, we introduced a number of general properties of
systems. In particular,
a system may or may not be
(1) Memoryless
(2) Time invariant
(3) Linear
(4) Causal
(S) Stable
Determine which of these properties hold and which do not hold for
each of the
following continuous-time systems. Justify your answers. In each
example, y(t) denotes
the system output and x(t) is the system input.
(b) y(t) [cos(31)]x(1) (c) y() = 13, x(T)dT x(t) + x(t - 2...
This is control system question. please answer all and
show a clear step. Thank you!
Question 3 Given the translational system shown in Figure 2, an input force, f(t) is applied to the mass, M, causing the dashpot which has a viscosity B and the spring, a stiffness coefficient of k, to compress with output displacement X(t). Input force, f(t) M O F Fixed point Displacement, X(t) Figure 2: A translational system (a) Derive the system's equation in terms of...
problem 7
Problem-4 [10 Points] Find the Laplace transforms of the functions in Figure. 2 Figure. 2: Triangular Function Problem-5 [10 Pointsl A system has the transfer function h(s) = (s1)(s +2) a) Find the impulse response of the system b) Determine the output y(t), given that the input is x(t) u(t) Problem-6 [10 Pointsl Use the Laplace transform to solve the differential equation +22+10v(t) 3 cos(2t) dt2 dt subject to v(0)-1, dv(O) Problem-7 [10 Points] Solve the integrodifferential equation...
The state space model of an interconnected three tank water storage system is given by the following equation -3 1 o 1[hi] dt The heights of water in the tanks are, respectively, hi, h2, hz. Each tank has an independent input flow; the volume flow rates of input water into the three tanks are, respectively, qii,qi2, Oi3. Each tank also has a water discharge outlet and the volume flow rates of water coming out of the tanks are, respectively, qo1,...
The state space model of an interconnected three tank water storage system is given by the following equation: -3 1 0 1rh dt os lo 0 3] 10 1-3 The heights of water in the tanks are, respectively, h,h2,h3. Each tank has an independent input flow; the volume flow rates of input water into the three tanks are, respectively, qǐ1,W2,4a. Each tank also has a water discharge outlet and the volume flow rates of water coming out of the tanks...
2.7.5 The impulse response of a continuous-time LTI system is given by h(t) = f(t) - et u(t). (a) What is the frequency response H (w) of this system? (b) Find and sketch H(w). (c) Is this a lowpass, bandpass, or highpass filter, or none of those? 2.7.6 The impulse response of a continuous-time LTI system is given by h(t) = S(t – 2). (This is a delay of 2.) (a) What is the frequency response H (w) of this...
Problem 4 (25%) Consider the attitude control system of a rigid satellite shown in Figure 1.1. Fig. 1.1 Satellite tracking control system In this problem we will only consider the control of the angle e (angle of elevation). The dynamic model of the rigid satellite, rotating about an axis perpendicular to the page, can be approximately written as: JÖ = tm - ty - bė where ) is the satellite's moment of inertia, b is the damping coefficient, tm is...
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