- The professor discusses plotting the phase plot for a transfer function containing multiple factors. He calculates the phase contributions of each factor at different frequencies and plots the individual phase plots.
- To plot the overall phase plot of the transfer function, he calculates the total phase at two corner frequencies and connects them with a smooth curve. This results in a phase plot that transitions from 90 degrees to -90 degrees over the different frequency ranges.
- He explains that the bode plot can be used to experimentally determine an unknown transfer function by measuring the input-output magnitude and phase responses at different frequencies.
This document is a transcript of a lecture on bode plots. The professor discusses drawing bode plots for second order transfer functions with different damping ratios. He draws the magnitude and phase plots, explaining how the resonant peak shifts left as damping increases. For undamped systems, he notes the magnitude would blow up to infinity at the natural frequency. He also discusses minimum phase and non-minimum phase systems, explaining how their phase plots differ at high frequencies. He leaves questions for students to think about generalizing these concepts to higher order systems and using bode plots to determine system properties.
1. The document discusses constructing the Bode plot of a transfer function step-by-step using an example transfer function of s/(s+1)*(s+10).
2. The transfer function is rewritten as a product of four factors: 0.1s, s, 1/(s+1), and 1/(0.1s+1). The Bode plots of the individual factors are constructed and then combined.
3. The Bode plot consists of a line with a slope of +20 dB/decade from the s term, shifted down by -20 dB from the 0.1 term. Below the first corner frequency of 1 rad/s, this represents the combined low-frequency
1) The document discusses transfer functions of linear time-invariant (LTI) systems. The governing equation for an nth order LTI system is presented.
2) Taking the Laplace transform of this equation yields the plant transfer function P(s) as a ratio of two polynomials, with the denominator polynomial d(s) of order n and the numerator polynomial n(s) of order m.
3) For causal systems, n must be greater than or equal to m, yielding a proper transfer function. The zeros of the transfer function are the roots of the numerator polynomial n(s) and the poles are the roots of the denominator polynomial d(s).
4) As homework, the student is
The document discusses using the Laplace transform to solve the heat equation for transient conduction. It presents a problem of calculating the temperature over time within a semi-infinite slab where the initial temperature is suddenly changed at the boundary. By taking the Laplace transform, the PDE is converted to an ODE, making the solution easier to obtain. The solution is found in the transform domain and then inverted back to the time domain to give the temperature as a function of position and time within the slab. Transforming the time variable rather than the space variable is preferred because it avoids issues with evaluating boundary terms involving derivatives.
This document discusses the Laplace transform and some of its key properties. It begins by reviewing the definition of the unilateral Laplace transform. It then outlines several important properties, including: 1) The Laplace transform of derivatives, where taking the derivative in the time domain corresponds to multiplying by s in the complex domain. 2) The initial value theorem and final value theorem. 3) The complex differentiation theorem, where differentiating in the complex domain corresponds to multiplying by -1/s. It also provides an overview of how the Laplace transform can be used to solve initial value problems for systems described by ordinary differential equations.
This document provides an introduction to state space representation of dynamic systems. It begins by stating that state space representation is an alternative to transfer function representation that allows analysis in the time domain rather than complex domain. It then uses the example of a mass-spring-damper system to illustrate the key steps: 1) Select state variables (here displacement and velocity), 2) Write first-order differential equations for each state variable based on the system model, 3) Collect the equations into matrix form allowing analysis with linear algebra tools. The representation allows rewriting a higher-order differential equation as a set of first-order equations.
- The document discusses constructing the Nyquist plot for a transfer function of the form s plus 1 divided by s plus 10.
- It is shown that the Nyquist plot for this transfer function is a semicircle in the first quadrant of the complex plane, with a center of 0.55 and radius of 0.45.
- The maximum phase angle of the transfer function occurs at the point where a tangent can be drawn to the semicircle, which is calculated to be 54.9 degrees using trigonometric relationships between the radius and tangent length.
The document discusses an upcoming lecture on Nyquist plots. It begins by reviewing frequency response and bode plots. It then introduces Nyquist plots, explaining that they visualize the sinusoidal transfer function G(j) by plotting its real and imaginary parts in the complex plane, known as the G(s) plane, as varies from 0 to infinity. Examples are given of plotting common transfer functions like 1/s, s, and 1/(Ts+1) on the Nyquist plane. Critical points like 0, =1/T, and are identified. The lecturer indicates they will demonstrate how to construct Nyquist plots and identify differences from bode plots.
- The document discusses bode plots and how to construct them for different transfer functions.
- It provides an example of constructing the bode plot for a transfer function G(s) = 1/s, showing that the magnitude plot is a straight line with a slope of -20 dB/decade and the phase plot is a horizontal line at -90 degrees.
- It then constructs the bode plot for a transfer function G(s) = s, finding that the magnitude plot has a slope of +20 dB/decade and the phase plot is a horizontal line at +90 degrees.
1) The document discusses Nyquist plots for various transfer functions, including time delay and second order systems.
2) A time delay transfer function results in a unit circle Nyquist plot, where the phase shifts from 0 to -Td as goes from 0 to infinity.
3) For a second order system, the Nyquist plot takes the shape of an arc that starts at 1 and ends at 1 as goes from 0 to infinity, cutting the imaginary axis when equals the natural frequency n.
- The document discusses the bode plot of a second-order transfer function.
- It shows that the high frequency asymptote has a slope of -40 dB/decade and intersects the low frequency asymptote at the natural frequency n, which is also the corner frequency.
- The magnitude of the transfer function reaches its maximum value at a frequency where the derivative of the denominator term is zero, which occurs at = n/(1-2龍^2).
1. The document discusses analyzing the root locus of a mass-spring system modeled as a second order plant with a transfer function of 1/(s^2 + 1).
2. A PD controller is designed with Kp/Kd = 10 to stabilize the closed loop system. The open loop transfer function is derived as Ks + 10/(s^2 + 1).
3. Steps are outlined to plot the root locus for K > 0, including determining open loop poles and zeros, locating parts of the real axis on the locus, calculating the asymptote, and finding breakaway/break-in points.
1) The professor derives that for a stable linear time-invariant system with a sinusoidal input, the steady state output will be a sinusoid of the same frequency as the input.
2) The steady state output magnitude is scaled by the magnitude of the system's transfer function evaluated at j, and the phase is shifted by the phase of the transfer function evaluated at j.
3) This property allows the experimental determination of a system's transfer function by analyzing the steady state response to various sinusoidal inputs.
This document discusses the magnitude and phase plots of first-order transfer functions. It begins by deriving the phase plot of 1/(Ts+1), showing that the phase approaches 0 degrees at low frequencies, -45 degrees at the corner frequency 1/T, and -90 degrees at high frequencies. It then derives the corresponding magnitude plot, showing it has the characteristics of a low-pass filter with a cutoff frequency of 1/T. Finally, it briefly discusses the magnitude and phase plots of the reciprocal transfer function T(s+1), showing the magnitude plot has a high-frequency asymptote of 20log(T) rather than -20log(T) as with 1/(Ts+1).
The document discusses Bode plots, which are used to visualize the frequency response of linear time-invariant systems. It begins by reviewing frequency response and how it characterizes the steady-state output of a system to a sinusoidal input.
It then introduces Bode plots, which have two components - a magnitude plot and a phase plot. The magnitude plot uses logarithmic scales for both frequency and magnitude in decibels. The phase plot uses a logarithmic scale for frequency and a linear scale for phase in degrees. Using logarithmic scales allows visualization of a wide range of frequencies and magnitudes on the same plot.
The document outlines common building blocks that comprise transfer functions, such as constants, integrals, derivatives, and
The document discusses the effect of zeros on a control system's step response. Specifically:
- The example system has poles at -1 and -10, and a zero at 2, in the right half of the complex plane.
- The step response will start in one direction, then reverse and go in the opposite direction before settling to the final value of -2/10.
- A zero in the right half plane leads to a non-minimum phase response where the output changes signs during the step response.
The document discusses Bode plots and frequency response analysis. It introduces the first-order transfer function 1/(Ts+1) as a new factor to analyze. The magnitude and phase expressions for this factor are derived. It is explained that the magnitude plot has low and high frequency asymptotes. The low frequency asymptote is 0 dB as the magnitude tends to 1 at low frequencies compared to 1/T. The high frequency asymptote is -20log(T) dB as the magnitude tends to 1/T at high frequencies. It is noted that the asymptotes intersect at the corner/break frequency of 1/T, where the responses change behavior.
This document is a lecture on modeling and control system design. The professor discusses modeling a mechanical system involving two shafts connected by gears as a second order system. He derives the transfer function of the system and shows it has two poles at the origin, making it unstable. The professor then poses two tasks: 1) derive the transfer function and 2) design a stable, negative feedback control system that meets settling time and overshoot requirements. Key points are that the open loop system is unstable, proportional control can stabilize it, and root locus can be used to meet performance goals.
- The document summarizes the process of designing a controller for a gear transmission system to satisfy stability and performance requirements.
- It describes deriving the plant transfer function, choosing an initial proportional controller, and analyzing the closed-loop stability and performance using root locus analysis.
- Key steps include determining the regions of the real axis on the root locus, identifying asymptotes, and finding a potential breakaway point at -5 where the controller gain is 12.5.
The document discusses performance specifications and steady state errors in control systems.
It begins by explaining that performance can be specified by defining regions in the s-plane where the closed loop poles must lie. It then discusses analyzing steady state error by assuming the closed loop system is stable and rewriting the open loop transfer function G(s)H(s) in a generic form based on the number of open loop poles at the origin. This determines if it is a type 0, 1, 2 etc. system, which impacts the steady state error calculation.
- The document discusses frequency response analysis of control systems.
- It begins by reviewing state space representation and relating transfer functions to state matrices. Two homework problems are assigned involving checking these relationships for a mass-spring-damper system.
- The lecture then introduces frequency response, which analyzes the response of a system to a sinusoidal input. It considers providing a sinusoidal input u(t) to a stable linear time-invariant system and derives the output y(t). This lays the foundation for discussing how frequency response can be used for control design.
1) The document discusses the Nyquist stability criteria, which uses the Nyquist plot of the open loop transfer function G(s)H(s) to determine the stability of the closed loop system.
2) The poles of the closed loop characteristic equation 1 + G(s)H(s) are called the open loop poles. The zeros are called the closed loop poles.
3) The key question is whether the Nyquist plot of the open loop transfer function G(s)H(s) can be used to comment on the stability of the closed loop system. The answer is yes, based on the mapping theorem.
- The document discusses root locus analysis for systems with positive and negative feedback, as well as for systems where the controller gain (K) is positive or negative.
- For positive feedback systems, one branch of the root locus always lies in the right half plane, making the system unstable for any positive K.
- For negative K, the analysis involves defining a new positive parameter K-hat equal to -K, which allows applying the same steps as for positive K with pseudo positive or negative feedback.
- A grid is presented to identify which set of steps to use based on the sign of feedback and K: set 1 for negative feedback and positive K, set 2 for positive feedback and positive K, set 2
- The document discusses applying the Nyquist stability criterion using the mapping theorem to determine closed-loop stability.
- It establishes that for closed-loop stability, the contour mapped from the open-loop transfer function in the s-plane should encircle the origin P times in the counterclockwise direction in the closed-loop transfer function plane, where P is the number of open-loop poles within the contour.
- Subtracting 1 from the closed-loop transfer function shifts the corresponding contour in the open-loop transfer function plane, such that the number of encirclements of the origin in the closed-loop plane equals the number of encirclements of the point -1 in the open
The document discusses several examples of second-order systems and their step responses. For the system 耽(t) + y(t) = u(t), the step response is 1 - cos(t), which is bounded but BIBO stability is not determined. For the system 耽(t) + 畉(t) = u(t), the step response is -1 + t + e-t, which tends to infinity, indicating it is not BIBO stable. Finally, the system 耽(t) + 畉(t) - 2y(t) = u(t) has a step response containing e
t, which also tends to infinity.
- The document discusses the differences in constructing a root locus diagram when the feedback is positive instead of negative.
- With positive feedback, the closed loop characteristic equation is 1 minus G(s)H(s) equals 0 instead of 1 plus G(s)H(s) equals 0.
- This means that closed loop poles occur when the open loop transfer function is equal to 1, instead of minus 1 as with negative feedback. Therefore, the phase condition changes from an odd multiple of pi to an even multiple of pi.
This document summarizes a lecture on control system design using root locus analysis. The professor discusses plotting the root locus for a specific system and using it to determine the range of proportional gain (KP) that ensures both closed-loop stability and desired performance. By substituting values into the closed-loop characteristic equation, they determine that KP must be between 8 and 35.76 to satisfy both conditions. They also note that choosing KP between 12.5 and 35.76 would result in an underdamped second order system, as desired. As homework, students are asked to plot the root locus for negative values of KP to gain more experience with root locus analysis.
1) The document discusses the steps to construct a root locus plot, including locating open loop poles and zeros, determining parts of the locus on the real axis, finding asymptotes, breakaway/breakin points, and crossover points where the locus crosses the imaginary axis.
2) As an example, the instructor constructs the root locus for an open loop transfer function with poles at -4 and 1. Key points are identified, including a crossover at the origin when K=4 and a breakaway point at -1.5 when K=6.25.
3) The root locus plot shows the closed loop system is stable for all K > 4. Additionally, a settling time less than 4 seconds can be
This document discusses the Nyquist stability criterion and the mapping theorem.
[1] The mapping theorem states that a closed contour in the s-plane maps to a corresponding closed contour in the F(s)-plane, where F(s) is a ratio of polynomials. The number of clockwise encirclements of the origin in the F(s)-plane equals Z - P, where Z is the number of zeros and P is the number of poles of F(s) inside the s-plane contour.
[2] An example function F(s) with two zeros and two poles is analyzed. A closed contour in the s-plane maps to a closed contour in the F(s)-plane
The document discusses the state space representation of linear time-invariant (LTI) systems. It provides the following key points:
1. The state space representation of a single-input single-output (SISO) LTI system is given by x (t) = Ax(t) + bu(t) and y(t) = cx(t) + du(t), where x(t) is the state vector, u(t) is the input, y(t) is the output, and A, b, c, d are matrices that characterize the system.
2. For multiple-input multiple-output systems, u(t) and y(t) become
- The document discusses bode plots and how to construct them for different transfer functions.
- It provides an example of constructing the bode plot for a transfer function G(s) = 1/s, showing that the magnitude plot is a straight line with a slope of -20 dB/decade and the phase plot is a horizontal line at -90 degrees.
- It then constructs the bode plot for a transfer function G(s) = s, finding that the magnitude plot has a slope of +20 dB/decade and the phase plot is a horizontal line at +90 degrees.
1) The document discusses Nyquist plots for various transfer functions, including time delay and second order systems.
2) A time delay transfer function results in a unit circle Nyquist plot, where the phase shifts from 0 to -Td as goes from 0 to infinity.
3) For a second order system, the Nyquist plot takes the shape of an arc that starts at 1 and ends at 1 as goes from 0 to infinity, cutting the imaginary axis when equals the natural frequency n.
- The document discusses the bode plot of a second-order transfer function.
- It shows that the high frequency asymptote has a slope of -40 dB/decade and intersects the low frequency asymptote at the natural frequency n, which is also the corner frequency.
- The magnitude of the transfer function reaches its maximum value at a frequency where the derivative of the denominator term is zero, which occurs at = n/(1-2龍^2).
1. The document discusses analyzing the root locus of a mass-spring system modeled as a second order plant with a transfer function of 1/(s^2 + 1).
2. A PD controller is designed with Kp/Kd = 10 to stabilize the closed loop system. The open loop transfer function is derived as Ks + 10/(s^2 + 1).
3. Steps are outlined to plot the root locus for K > 0, including determining open loop poles and zeros, locating parts of the real axis on the locus, calculating the asymptote, and finding breakaway/break-in points.
1) The professor derives that for a stable linear time-invariant system with a sinusoidal input, the steady state output will be a sinusoid of the same frequency as the input.
2) The steady state output magnitude is scaled by the magnitude of the system's transfer function evaluated at j, and the phase is shifted by the phase of the transfer function evaluated at j.
3) This property allows the experimental determination of a system's transfer function by analyzing the steady state response to various sinusoidal inputs.
This document discusses the magnitude and phase plots of first-order transfer functions. It begins by deriving the phase plot of 1/(Ts+1), showing that the phase approaches 0 degrees at low frequencies, -45 degrees at the corner frequency 1/T, and -90 degrees at high frequencies. It then derives the corresponding magnitude plot, showing it has the characteristics of a low-pass filter with a cutoff frequency of 1/T. Finally, it briefly discusses the magnitude and phase plots of the reciprocal transfer function T(s+1), showing the magnitude plot has a high-frequency asymptote of 20log(T) rather than -20log(T) as with 1/(Ts+1).
The document discusses Bode plots, which are used to visualize the frequency response of linear time-invariant systems. It begins by reviewing frequency response and how it characterizes the steady-state output of a system to a sinusoidal input.
It then introduces Bode plots, which have two components - a magnitude plot and a phase plot. The magnitude plot uses logarithmic scales for both frequency and magnitude in decibels. The phase plot uses a logarithmic scale for frequency and a linear scale for phase in degrees. Using logarithmic scales allows visualization of a wide range of frequencies and magnitudes on the same plot.
The document outlines common building blocks that comprise transfer functions, such as constants, integrals, derivatives, and
The document discusses the effect of zeros on a control system's step response. Specifically:
- The example system has poles at -1 and -10, and a zero at 2, in the right half of the complex plane.
- The step response will start in one direction, then reverse and go in the opposite direction before settling to the final value of -2/10.
- A zero in the right half plane leads to a non-minimum phase response where the output changes signs during the step response.
The document discusses Bode plots and frequency response analysis. It introduces the first-order transfer function 1/(Ts+1) as a new factor to analyze. The magnitude and phase expressions for this factor are derived. It is explained that the magnitude plot has low and high frequency asymptotes. The low frequency asymptote is 0 dB as the magnitude tends to 1 at low frequencies compared to 1/T. The high frequency asymptote is -20log(T) dB as the magnitude tends to 1/T at high frequencies. It is noted that the asymptotes intersect at the corner/break frequency of 1/T, where the responses change behavior.
This document is a lecture on modeling and control system design. The professor discusses modeling a mechanical system involving two shafts connected by gears as a second order system. He derives the transfer function of the system and shows it has two poles at the origin, making it unstable. The professor then poses two tasks: 1) derive the transfer function and 2) design a stable, negative feedback control system that meets settling time and overshoot requirements. Key points are that the open loop system is unstable, proportional control can stabilize it, and root locus can be used to meet performance goals.
- The document summarizes the process of designing a controller for a gear transmission system to satisfy stability and performance requirements.
- It describes deriving the plant transfer function, choosing an initial proportional controller, and analyzing the closed-loop stability and performance using root locus analysis.
- Key steps include determining the regions of the real axis on the root locus, identifying asymptotes, and finding a potential breakaway point at -5 where the controller gain is 12.5.
The document discusses performance specifications and steady state errors in control systems.
It begins by explaining that performance can be specified by defining regions in the s-plane where the closed loop poles must lie. It then discusses analyzing steady state error by assuming the closed loop system is stable and rewriting the open loop transfer function G(s)H(s) in a generic form based on the number of open loop poles at the origin. This determines if it is a type 0, 1, 2 etc. system, which impacts the steady state error calculation.
- The document discusses frequency response analysis of control systems.
- It begins by reviewing state space representation and relating transfer functions to state matrices. Two homework problems are assigned involving checking these relationships for a mass-spring-damper system.
- The lecture then introduces frequency response, which analyzes the response of a system to a sinusoidal input. It considers providing a sinusoidal input u(t) to a stable linear time-invariant system and derives the output y(t). This lays the foundation for discussing how frequency response can be used for control design.
1) The document discusses the Nyquist stability criteria, which uses the Nyquist plot of the open loop transfer function G(s)H(s) to determine the stability of the closed loop system.
2) The poles of the closed loop characteristic equation 1 + G(s)H(s) are called the open loop poles. The zeros are called the closed loop poles.
3) The key question is whether the Nyquist plot of the open loop transfer function G(s)H(s) can be used to comment on the stability of the closed loop system. The answer is yes, based on the mapping theorem.
- The document discusses root locus analysis for systems with positive and negative feedback, as well as for systems where the controller gain (K) is positive or negative.
- For positive feedback systems, one branch of the root locus always lies in the right half plane, making the system unstable for any positive K.
- For negative K, the analysis involves defining a new positive parameter K-hat equal to -K, which allows applying the same steps as for positive K with pseudo positive or negative feedback.
- A grid is presented to identify which set of steps to use based on the sign of feedback and K: set 1 for negative feedback and positive K, set 2 for positive feedback and positive K, set 2
- The document discusses applying the Nyquist stability criterion using the mapping theorem to determine closed-loop stability.
- It establishes that for closed-loop stability, the contour mapped from the open-loop transfer function in the s-plane should encircle the origin P times in the counterclockwise direction in the closed-loop transfer function plane, where P is the number of open-loop poles within the contour.
- Subtracting 1 from the closed-loop transfer function shifts the corresponding contour in the open-loop transfer function plane, such that the number of encirclements of the origin in the closed-loop plane equals the number of encirclements of the point -1 in the open
The document discusses several examples of second-order systems and their step responses. For the system 耽(t) + y(t) = u(t), the step response is 1 - cos(t), which is bounded but BIBO stability is not determined. For the system 耽(t) + 畉(t) = u(t), the step response is -1 + t + e-t, which tends to infinity, indicating it is not BIBO stable. Finally, the system 耽(t) + 畉(t) - 2y(t) = u(t) has a step response containing e
t, which also tends to infinity.
- The document discusses the differences in constructing a root locus diagram when the feedback is positive instead of negative.
- With positive feedback, the closed loop characteristic equation is 1 minus G(s)H(s) equals 0 instead of 1 plus G(s)H(s) equals 0.
- This means that closed loop poles occur when the open loop transfer function is equal to 1, instead of minus 1 as with negative feedback. Therefore, the phase condition changes from an odd multiple of pi to an even multiple of pi.
This document summarizes a lecture on control system design using root locus analysis. The professor discusses plotting the root locus for a specific system and using it to determine the range of proportional gain (KP) that ensures both closed-loop stability and desired performance. By substituting values into the closed-loop characteristic equation, they determine that KP must be between 8 and 35.76 to satisfy both conditions. They also note that choosing KP between 12.5 and 35.76 would result in an underdamped second order system, as desired. As homework, students are asked to plot the root locus for negative values of KP to gain more experience with root locus analysis.
1) The document discusses the steps to construct a root locus plot, including locating open loop poles and zeros, determining parts of the locus on the real axis, finding asymptotes, breakaway/breakin points, and crossover points where the locus crosses the imaginary axis.
2) As an example, the instructor constructs the root locus for an open loop transfer function with poles at -4 and 1. Key points are identified, including a crossover at the origin when K=4 and a breakaway point at -1.5 when K=6.25.
3) The root locus plot shows the closed loop system is stable for all K > 4. Additionally, a settling time less than 4 seconds can be
This document discusses the Nyquist stability criterion and the mapping theorem.
[1] The mapping theorem states that a closed contour in the s-plane maps to a corresponding closed contour in the F(s)-plane, where F(s) is a ratio of polynomials. The number of clockwise encirclements of the origin in the F(s)-plane equals Z - P, where Z is the number of zeros and P is the number of poles of F(s) inside the s-plane contour.
[2] An example function F(s) with two zeros and two poles is analyzed. A closed contour in the s-plane maps to a closed contour in the F(s)-plane
The document discusses the state space representation of linear time-invariant (LTI) systems. It provides the following key points:
1. The state space representation of a single-input single-output (SISO) LTI system is given by x (t) = Ax(t) + bu(t) and y(t) = cx(t) + du(t), where x(t) is the state vector, u(t) is the input, y(t) is the output, and A, b, c, d are matrices that characterize the system.
2. For multiple-input multiple-output systems, u(t) and y(t) become
1) The document describes deriving the governing equations of motion for a gear transmission system consisting of an input shaft connected to an output shaft via gears.
2) Equations are written for the torques acting on the input and output shafts based on free body diagrams. Gear ratios are then used to relate the angular displacements and eliminate variables, resulting in a single equation relating the input torque, output angular displacement, and load torque.
3) The derivation results in a consolidated differential equation that models the gear transmission system and relates the input torque to the output angular displacement, achieving the goal of obtaining a linear model for control system design.
The professor discusses how to convert performance specifications into desired regions for closed loop pole locations to ensure stability and meet specifications. He uses an example where the dominant closed loop dynamics are required to have a settling time below 4 seconds and a peak overshoot below 10%. By analyzing these specifications, he derives a region in the complex plane shaped like an open trapezoid. As long as the closed loop poles lie within this region, both the settling time and overshoot specifications will be met while also maintaining stability. Root locus analysis can then be used to determine controller parameters that place the closed loop poles within this desired region.
- The document discusses a special case of Routh's stability criterion where an entire row of the Routh's array is zero.
- When this occurs, it implies the polynomial will have radially opposite roots. An auxiliary polynomial is constructed from the row above to determine these roots.
- An example is worked through where the auxiliary polynomial is found to have four radially opposite roots of -1賊j and +1賊j. This implies two roots are in the right half plane, with the remaining five roots in the left half plane.
The document discusses special cases that may occur when constructing the Routh's array to analyze the stability of a control system. The first case is when the first element of a row in the array is zero, with other elements non-zero. In this case, the zero should be replaced with a small positive number epsilon. If there is no sign change from the element above epsilon to below, there is a pair of roots on the imaginary axis. If there is a sign change, roots exist in the right half plane. An example is worked out demonstrating no sign change, indicating roots on the imaginary axis. A second example shows a sign change, meaning roots in the right half plane.
1. The document discusses applying Routh's stability criterion to analyze the stability of control systems.
2. Routh's array is constructed for two example polynomials to determine the location of roots in the complex plane.
3. For the first polynomial, the Routh's array shows no sign changes, indicating all roots have negative real parts and the system is stable.
4. For the second polynomial, the Routh's array shows two sign changes, indicating two roots have positive real parts and the system is unstable.
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des Louis de belle accueillis sell puss p竪re peut olds sects it's all辿tells peutall asplait suite
Il -12 ) pas cause subit lequel euros le en as d辿taill辿 de till
PILONI balo -2
ispeulit Mais anglais appareils guilt gens ils en anglais glory pile le vous pr竪s
... still que y pais vida Los play qu辿tej坦n Less via Leal su abuelos l叩stimaall) isa las
des audit elleguilt disons s'il souhait sous sirs vous lucius atoutes pouvait lets pas
il taille glacis Lieu daily qui les jeutaille pas bill Luc jean 辿cumait il taille Lacis just-Zuf辰lligurl zu
peut 辿lus silly mais les mes ishaute quils le aurais sans Les 辿tablis qui
des Louis de belle accueillis sell puss p竪re peut olds sects it's all辿tells peutall asplait suite
Il -12 ) pas cause subit lequel euros le en as d辿taill辿 de till
PILONI balo -2
ispeulit Mais anglais appareils guilt gens ils en anglais glory pile le vous pr竪s
... still que y pais vida Los play qu辿tej坦n Less via Leal su abuelos l叩stimaall) isa las
des audit elleguilt disons s'il souhait sous sirs vous lucius atoutes pouvait lets pas
il taille glacis Lieu daily qui les jeutaille pas bill Luc jean 辿cumait il taille Lacis just -Zuf辰lligurl zu
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Biases, our brain and software developmentMatias Iacono
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Quick presentation about cognitive biases, classic psychological researches and quite new papers that displays how those biases might be impacting software developers.
This PPT covers the index and engineering properties of soil. It includes details on index properties, along with their methods of determination. Various important terms related to soil behavior are explained in detail. The presentation also outlines the experimental procedures for determining soil properties such as water content, specific gravity, plastic limit, and liquid limit, along with the necessary calculations and graph plotting. Additionally, it provides insights to understand the importance of these properties in geotechnical engineering applications.
Defining the Future of Biophilic Design in Crete.pdfARENCOS
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Mozambique, a country with vast natural resources and immense potential, nevertheless faces several economic challenges, including high unemployment, limited access to energy, and an unstable power supply. Underdeveloped infrastructure has slowed the growth of industry and hampered peoples entrepreneurial ambitions, leaving many regions in the darkliterally and figuratively.
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Algorithm design techniques include:
Brute Force
Greedy Algorithms
Divide-and-Conquer
Dynamic Programming
Reduction / Transform-and-Conquer
Backtracking and Branch-and-Bound
Randomization
Approximation
Recursive Approach
What is an algorithm?
An Algorithm is a procedure to solve a particular problem in a finite number of steps for a finite-sized input.
The algorithms can be classified in various ways. They are:
Implementation Method
Design Method
Design Approaches
Other Classifications
In this article, the different algorithms in each classification method are discussed.
The classification of algorithms is important for several reasons:
Organization: Algorithms can be very complex and by classifying them, it becomes easier to organize, understand, and compare different algorithms.
Problem Solving: Different problems require different algorithms, and by having a classification, it can help identify the best algorithm for a particular problem.
Performance Comparison: By classifying algorithms, it is possible to compare their performance in terms of time and space complexity, making it easier to choose the best algorithm for a particular use case.
Reusability: By classifying algorithms, it becomes easier to re-use existing algorithms for similar problems, thereby reducing development time and improving efficiency.
Research: Classifying algorithms is essential for research and development in computer science, as it helps to identify new algorithms and improve existing ones.
Overall, the classification of algorithms plays a crucial role in computer science and helps to improve the efficiency and effectiveness of solving problems.
Classification by Implementation Method: There are primarily three main categories into which an algorithm can be named in this type of classification. They are:
Recursion or Iteration: A recursive algorithm is an algorithm which calls itself again and again until a base condition is achieved whereas iterative algorithms use loops and/or data structures like stacks, queues to solve any problem. Every recursive solution can be implemented as an iterative solution and vice versa.
Example: The Tower of Hanoi is implemented in a recursive fashion while Stock Span problem is implemented iteratively.
Exact or Approximate: Algorithms that are capable of finding an optimal solution for any problem are known as the exact algorithm. For all those problems, where it is not possible to find the most optimized solution, an approximation algorithm is used. Approximate algorithms are the type of algorithms that find the result as an average outcome of sub outcomes to a problem.
Example: For NP-Hard Problems, approximation algorithms are used. Sorting algorithms are the exact algorithms.
Serial or Parallel or Distributed Algorithms: In serial algorithms, one instruction is executed at a time while parallel algorithms are those in which we divide the problem into subproblems and execute them on different processors.
1. Control Systems
Prof. C. S. Shankar Ram
Department of Engineering Design
Indian Institute of Technology, Madras
Lecture 56
Bode Plot 4
Part - 2
So now, having a plot at the magnitude plot; once again please note that I am only
plotting the asymptotes right. We are not plotting the actual curve assets right. So, now
let us go ahead and plot the phase plot.
(Refer 際際滷 Time: 00:38)
So, let us do the phase plot. So, let me draw the phase plot. So, the phase of G of j omega
I am plotting in degrees. So, let us say I start with 0, and then let us say so this is ok, let
us say this is minus 90, let us say this is plus 90, fine.
So, once again we have 0.1, 1, 10 say 100 so as the four regions. Now, let us just plot the
phase plot. So, what is going to happen let us do it for each one factor at a time right that
is what we are going to do. So, let me use the same colour code.
So, what happens to the see ultimately what are we plotting for G of s is going to be let
me rewrite the transfer function here. So, 0.1 s divided by s plus 1 times 0.1 s plus 1
right, so that is what we are doing ok. So, now what is going to be the phase contribution
2. of 0.1, the phase contribution of 0.1 is going to be 0 degrees right. So, I draw a horizontal
line at 0 degrees. So, this is going to be the contribution from 0.1.
What is going to be the contribution from s plus 90 right? So that is going to be the same
throughout the frequency range. So, this is the phase contribution of s. What about the
phase contribution of 1 by s plus 1? So, if you recall what happens with 1 by s plus 1 is
at the low frequency value is 0, it has a phase of minus 45 degrees at the corner
frequency is 1 and then it tends to 90 degree minus 90 degrees as omega tends to infinity
right that is the phase plot of 1 by s plus 1 right. So, that is what I am going to plot. So, at
the corner frequency of 1, we are going to have a what to say phase of minus of 45.
So, what is going to happen is the following. So, 1 by s plus 1 will have a phase plot like
this ok. This is going to be the phase plot of 1 by x plus 1 in green. Now, what is going to
happen with 1 by 0.1 s plus 1 at the corner frequency of 10, we are going to have a phase
of minus 45. So, what is going to happen is the following. So, we are going to have a
phase diagram of 1 by 0.1 s plus 1 coming like this ok. So, this is the phase diagram of 1
by 0.1 s plus 1.
So, now what we need to do is that if I want a phase diagram of the complete transfer
function, I just need to add the four curves right. But this is a little bit complex because
these are not straight lines right. So, it is ok, but the thing is that like at low frequencies
you will start from plus 90 degrees that is obvious right because at very low frequencies
the only phase contribution will come from s, because 0.1 anyway will give you of case
contribution of 0 degrees throughout, 1 by s plus 1 and 1 by 0.1 s plus 1 will give you a
phase contribution of close to 0 degrees at low frequencies.
So, at low frequencies, anyway I will start from the value of 90 degrees. So, if you in a
sense look at the phase of G of j omega, the essentially the formula for this is going to be
90 degrees, because that is what s will give me minus tan inverse omega that is what the
will be the phase of 1 by j omega plus 1 and tan inverse of minus tan inverse of 0.1
omega because that is going to be the phase contribution of 1 divided by 0.1 j omega
plus 1, right.
So, I think this is something which we have discussed before right you have a transfer
function as essentially products of the you just add the individual take the algebraic sum
of the individual phase contributions right so that is what we have.
3. So, what we do is that like in order to plot the net phase plot, we just take the we just
calculate the a phase at the corner frequency, so that we can mark them and draw a
smooth curve through those frequencies right. So, the two corner frequencies are at are at
omega equals 1 and omega equals 10. So, at omega equals 1, what is going to happen to
this what to say value, we are going to have 90 degrees minus tan inverse 1 minus tan
inverse of 0.1 all right so that is what we are going to have.
So, what is the value, can you calculate and tell me? Of course, tan inverse of 1 is 45.
What is tan inverse of 0.1? So, if I calculate tan inverse 0.1 that is around 5.71 degrees
right, so 5.71 plus 45 that is going to be the 1. So, I subtract it from 90 I get 39.29, so
that is what I have. So, I get 39.29 degrees as a value at omega equals are 1.
So, at omega equals 1, the phase is going to be approximately let us say something like
39 oops 39.29 ok. So, this value is something like 39.29 ok, so that is that is the value.
Now, at omega equals 10, what do we get, the phase of G of j omega is going to be equal
to 90 degrees minus tan inverse of 10 minus tan inverse of 1 all right that is what we will
have. So, tan inverse of one the third term now is 45 degrees. What is tan inverse of 10,
let us calculate.
So, let us calculate tan inverse of 10, and then we will see what happens tan inverse of 10
is this, then I add 45 then I take the negative of this and then I add 90. So, I am going to
get essentially the negative of the same number, I am going to get minus 39.29 degrees
that is what I am going to get alright. So, at 10, I am going to have something like this.
So, this is going to be minus 39.29.
So, what I need to draw is that I need to draw a phase curve which essentially starts from
90, and then like passes through these through do two points. And then ultimately goes to
minus 90 as omega tends to infinity ok, so that is what will happen. Why minus 90,
because tan inverse omega will contribute a 90 degrees tan inverse of 0.1 omega will
contribute a 90 degrees. So, immediately you see that as omega tends to infinity, the
phase of G of j omega will tend to minus 90 degrees all right. I hope it is clear, right.
And as omega tends to 0, the phase of G of j omega you can immediately see that it tends
to 0 degrees right that is pretty obvious so that is why sorry not 0, 90 degrees I am sorry
about that plus 90 because the tan inverse 2 tan inverse terms will contribute 0, you have
already have a 90 degree term. So, we have 90 degrees. So, you see that the phase curve
4. goes from 90 plus 90 to minus 90 in this manner ok. So, this is the phase curve of this net
transfer function. So, the red one is a phase of G of j omega ok, so that is the phase plot
for this particular transfer function.
And you immediately see that because this has a 0 at 0, it does not have a 0 on the right
half plane, it essentially follows the points that we discussed at the beginning of this
class right. What did we discuss, you give me a transfer function right, and I plot the
bode diagram, you immediately see that the magnitude plot is going to tend to a slope of
minus 20 times n minus m decibels per decade. What was the n minus m in this
problem? What is n? 2 m 1 in this particular problem right, because this is a transfer
function we started off with is not it ok. So, you see that n minus m is 1 in this case.
(Refer 際際滷 Time: 11:21)
So, what did the magnitude plot slope tend to at high frequencies minus 20 decibels per
decade one could see that right, so that was the general concept that we learned. And
since this is a minimum phase system, what did the phase tend to minus 90 degrees times
n minus m. You see that it tends to minus 90 degrees.
So, this is the procedure for calculating the bode plot right. So, given the particular
transfer function, we should be also familiar with the inverse process. Let us say I give
you this bode plot. Can you figure out the transfer function that plays a very important
role like as far as experimental determination of transfer function is concerned. And
towards the end of the course, we will do a case study in that regard ok. So, I will give
5. you, the reason I am letting you do all the experiments I want to see you know like how
much you gain out of those experiments.
So, I want you to independently think and then like what I will do is that I will give you
actual data from one of those experiments and then ask you to get the transfer function
ok. Some techniques you may be already reading what to say learning in some of the
experience so, but then like let us see towards the end like. So, how the theory and
practice come together see right now we are looking at many mathematical what to say
formulations and ideas and so on right.
So, using frequency response, towards the end you will see how everything comes
together for practical applications so that is something which we look at in that maybe
the last two weeks of the course right. So, we will do a few case studies. So, that is that is
something which we will keep for the end ok.
So, this is the bode plot and it becomes very important because what happens is that like
many times if you want to experimentally determine the transfer function of the system
right, let us say what we have been doing in this course, we have been using physics to
derive, mathematical equations in the form of linear ODEs, then take Laplace transform
then get the transfer function right. Suppose, you know like we want to do the same
process empirically that is I do not want to derive equations of motion or I am not in a
position to derive equations of motion because my system which is given to me is like a
black box, I do not know what components are there. So, I cannot I am in a position not
to apply physics to model the system
Then what I do is a I can use frequency response to my advantage right is not it I can use
experience to my advantage right. I can do sinusoids of various varying frequency, I look
at the steady state output. Of I also get sinusoids of the same frequency, then I know that
in the frequency range of interest, I can model the system as an LTA system right that is
point number one.
And then what you do is that then you record the input sinusoid, output sinusoid you
know what is a scaling ok. You know the input amplitude output amplitude you will get
the amply magnitude at particular frequencies you can also measure the phase shift all
right then you get the phase plot then you plot the magnitude plot, plot the phase plot you
get the bode plot right. And you do the inverse problem that is given the bode plot, how
6. do you get the transfer function that is something which you can figure out right, so that
is that is an important practical application of what we are learning as far as the bode
diagram is concerned right.
So, anyway I will give you a few more bode diagrams to plot as homework ok. So but
now, I know like what I am going to leave you with is a bunch of question is a set of
questions right.
(Refer 際際滷 Time: 15:15)
So, I am going to ask you a question ok, please think about it and try to figure out the
answer. Using the bode plot bode plot, how can one calculate the values of K p e, K v e,
and K a e ok. I think I am using;I hope I am using the same symbols right.
So, K p e was a static position error constant; K v e was a static velocity error constant;
K e was a static acceleration error constant. You remember when we did steady state
error analysis. Please refer to those notes right. I am hoping that using the same symbols
ok.
So, the question is are like I am going to leave you with is it like how do we calculate
these constants right when we have the bode plot that is why I give you the bode plot,
can you use a bode plot to graphically figure out these constants. And what is the
advantage of this, because using the bode plot you can tell me what is going to be the
7. steady state error right when you have certain types of inputs right, so that is something
which I want you to figure out ok.
So, I am just going to stop here like. So, with this we complete our discussion of bode
plots. So, in the big picture perspective what we are doing, we are doing frequency
response right essentially what happens when we go sinusoidal inputs to stable LTA
systems we saw that the steady state output is also going to be a sinusoid of the same
frequency, but scaled in magnitude and shifted in phase right. And the term which is
important is what is called a sinusoidal transfer function right so which we get by
substituting s equals g omega in the system transfer function.
Now, the question is how do we visualize the sinusoidal transfer function, so that we can
do frequency response analysis. One of the main tools which you will use in multiple
domains including automotive and biomedical which is which is the which are the
groups of interest for our department, we one of the main tools we use is what is called
the bode plot that is why I go ahead spend a quite a bit of time in explaining the bode
plots.
So, next week what I am going to do is that like I am going to briefly discuss what is
called as a Nyquist plot and the Nyquist stability criteria. I am not going to spend so
much time on that ok, but I want you to know what they are right. And then like we will
go to what to say essentially controller design using frequency response methods ok. We
did control design using time response methods. Now we are going to use these
frequency response methods to design controllers. And then we look at both ok, so that is
what our action plan is fine.