is called the 3dB bandwidth. (d)(6pts) The Dryden model MIL-F-8785C for simulating turbulence in relation to the short period mode is
|
|
- Valentine Atkins
- 5 years ago
- Views:
Transcription
1 Homeork 6 AERE355 Fall 7 Due /7 (M) SOLUTION PROBLEM (3pt The transfer function of a first order Lo Pass Filter (LPF) is frequency rane [, ] is called the filter 3dB bandidth () (a)(8pt The dc (ie very lo frequency) ain is ( i) computation to determine hy the interval [, ] H( ( s / H ives lo H( i) lo() db is called the 3dB bandidth here the ) Use the same / Solution: H ( i ) ives H( i ) Hence: lo H( i ) lo / lo() 3 db i The interval is the rane of frequencies such that the manitude of is ith 3dB of its static ain [, ] H ( i) (b)(6pt The bode(h) command as used to obtain the Frequency Response Function (FRF) shon at riht for rad/s For an input u( t) sin(t) use the information in Fiure (b) to estimate the values of M and expression for the output y ( t) M sin(t ) Solution: M () () db db M o ( ) 83 45rad (c)(pt The term lo pass filter is due to the fact that hen an input is supplied to H (, the output is a filtered version of the input Specifically, loer frequency (meanderin) components are alloed to pass freely, hile hiher frequency (rapidly jitterin) components are suppressed To visualize this, use the lsim command to complete the code at (c) in relation to a measured hite noise input, This is an array of numbers randomly u(t) sampled from a normal distribution havin mean and standard deviation Overlay plots of the input and output, and discuss ho they differ Solution: [See (c)] It is clear that the output is far less jittery than the input Fiure (b) FRF for H( ith Fiure (c) Plots of input and output (d)(6pt The Dryden model MIL-F-8785C for simulatin turbulence in relation to the short period mode is / 6 8 ( / 4b) H ( The input to this model is hite noise ith standard deviation Obtain the / 3 V L (4b / V ) s expression for the -3 db bandidth of this shapin filter Then describe hat the involved parameters are, and ho they control the bandidth Solution: V / b This is proportional to the plane speed V, and is inversely proportional to the in span b 4
2 PROBLEM (35pt The dynamics of the short period response to ind can be approximated by: q M Z M Z M M q Z q M M q q () Consider the Boein 747 (@ M=9) ith the folloin information: u=87; =37; Za=-34365; Ma=-68; Mad=-43; Mq=-396; Zde=86; Mde=-4; (a)(pt The dynamical system () is a -input/-output system Write a Matlab proram that uses the command sstf to obtain the to transfer functions of the system () associated ith only the input Solution: [See (a)] H ( ) 453 s 44 ( s 9335s 774 and (t) s 77 s 9335s 774 ( ) H q ( (b)(6pt Use the Matlab bode command to obtain plots the to FRF s associated ith the transfer functions in (a) Solution: [See (b)] Manitude (db) Phase (de) Phase (de) Manitude (db) SortPeriod FRF for a(t) in Response to (t) Frequency (rad/ Short Period FRF for q(t) in Response to (t) - Frequency (rad/ ( Fiure (b) Plot of the short period mode FRF s ) ( ) ( i) and H q ( i) H (c)(pt Give the system characteristic polynomial, and use it to obtain numerical values for (i) (iv) d, and (v) Solution: p ( s 9335s 774 s n n, (ii) n, (iii), ns Hence: (i) n 9335/ 4667 ; (ii) n r / s ; (iii) 4667/ ; (iv) 48 r s ; (v) / 43 sec d n / n (d)(9pt Use the Matlab command step to obtain a plots of the to step responses to a sharp ede ust Use the data cursor in relation to each response to estimate (i) d, and (ii) 4 [The data cursor information should be included in your plots] Finally, compare these numbers to those associated ith your ansers in (c) Solution: [See (d)]
3 3 Amplitude Amplitude 4 x -4 System: Ha Time (second: 8 Amplitude: 3 3 Short Period a(t) in Response to unit step (t) System: Ha Time (second: 97 Amplitude: 35 System: Ha Time (second: Amplitude: 84e-5 Time (second x Short Period q(t) in Response to unit step q (t) System: Hq Time (second: 54 Amplitude: -5 System: Hq Time (second: 498 Amplitude: -36 System: Hq Time (second: Amplitude: Time (second Fiure (d) Plots of the short period mode (t) and q(t) responses to a sharp ede (ie unit step) ust, (t) In relation to In relation to (t) Results from (c): : T (379 8) 5sec / T 5r s & 4 97sec T d d d / (498 54) 488sec / T 88r & 4 849sec q(t) : s d d d / 48 r s & sec d / Comment: The results from both plots compare favorably to the results in (c), iven that they ere obtained by eyeballin :)
4 4 PROBLEM 3(35pt As a continuation of Problem, in this problem e consider the short period mode responses to von Karmon turbulence (t) From p8 of Nelson, the vertical ind turbulence spatial psd is iven by: 8 8 (339L ) (339 ) L L 3 L ( ) 3 / 6 (654*) (339L ) (339 L ) [*The rihtmost approximate equality is reasonable, and is needed to simplify the folloin parts] In vie of the fact that ( ) [see (655) on p9], the temporal psd is iven by: L 8 (339L 3 (339L ) a ) c ( b ) here e have, for convenience, defined a 339L ; b a 8/ 3 ; c L / (3) (a)(5pt Define the hite noise psd From (3) sho that the expression for Solution: i) ( ) i) Then (65) on p8 is: ( ) ( ) i) c[ b( i)] in relation to the rihtmost expression is iven by i) [ a( i)] c ( b ) c[ b( i)] c[ b( i)] c[ b( i)] i) i) Hence, i) a [ a( i)] [ a( i)] [ a( i)] c( bs ) 4 (b)(5pt From (a) the turbulence shapin filter is G ( For L ft and u 87fps use the bode ( as ) command to obtain a plot of this filter FRF Solution: [See 3(b)] Manitude (db) Vertical Von Karmon Turbulence Shapin Filter Phase (de) Frequency (rad/ Fiure 3(b) Shapin filter for the von Karmon vertical turbulence psd (c)(5pt The shapin filter (3) for the turbulence is a lo-pass filter From your plot in (b) find the ratio of the poer density at rad/sec divided by the enery at rad/sec Give your anser both as a difference in ddb, as ell as an actual ratio Solution: The psd at rad/sec is -db relative to the enery at rad/sec Since lo ( r), the ratio is r
5 5 4 (d)(7pt Use the Matlab command * normrnd(,,,) for /(L ) 57( 4 ), to simulate the hite noise that ill serve as the input to the shapin filter Then use the command lsim(sys,, tvec) to compute the filter output Your time array should be tvec should use the increment, and here 339L is the shapin filter time constant Plot both the input (hite noise) and output (turbulence) time series Solution: [See 3(d)] dt / Fiure 3(d) Plots of hite noise input and of simulated turbulence, (t) (e)(7pt Run your simulated turbulence in (d) throuh your -input / -output short period transfer function to obtain plots of the simulated and (t) Solution: [See 3(e)] q(t) responses Fiure 3(e) Short period mode (t) and q(t) responses to (t) H( (f)(6pt The block diaram related to the above is shon at the riht It reveals the (t) ( t) (t) poer of the Laplace transform Specifically, it shos that q( t) A( H( W ( Q( Hence, as an extension of the discussion in (b) e obtain the folloin expression for the psds S ( ) for (t) and q (t) : H( i) i) S ( ) Use the bode command in relation to the transfer funtion q H( in order to arrive at plots of these to psds Solution: [See 3(f)] Fiure 3(f) Plots of theoretical psd s for (t) and q (t)
6 Matlab Code %PROGRAM NAME: h6m %PROBLEM : %(b): =; s=tf('s'); H=/((s/) + ); fiure() bode(h) title('frf for H ith _B_W= r/s') % %(c): rn('shuffle') %This ill ensure that no to students have the same numbers n=; u=normrnd(,,n,); dt=; t=:n-; t=dt*t'; y=lsim(h,u,t); fiure() plot(t,[u,y]) title('plots of Input and Output') xlabel('time (sec)') %==================================================== %PROBLEM %Simulate Boein 747 response to von Karmon ind turbulence % Plane Information: u=87; =37; Za=-34365;Ma=-68;Mad=-43;Mq=-396;Zde=86;Mde=-4; % A, B, C & D Matrices: A=[Za/u, ; Ma+Mad*Za/u,Mad+Mq]; B=[-Za/u^,;-Ma/u^,-Mq]; C=eye(); D=zeros(,); %(a): % Creation of state space system & transfer functions related to : Hss=ss(A,B,C,D); [Hn,Hd]=sstf(A,B,C,D,); %Transfer functions re: ; Ha=tf(Hn(,:),Hd) Hq=tf(Hn(,:),Hd) %(b): fiure() vec=lospace(-,,); subplot(,,),bode(ha,vec) title('short Period Bode Plot for a(t) in Response to (t)') subplot(,,),bode(hq,vec) title('short Period Bode Plot for q(t) in Response to (t)') %(d): fiure() subplot(,,),step(ha) title('short Period a(t) in Response to unit step _(t)') subplot(,,),step(hq) title('short Period q(t) in Response to unit step q_(t)') %=========================================================== %PROBLEM 3 %(b): % Turbulence Information: L=^4; si=pi/(*l); s=(si**l)/pi; tau=339*l/u; =/tau; Hnum=s*[tau*(8/3)^5, ]; Hden=[tau^, *tau, ]; H=tf(Hnum, Hden); fiure(3) bode(h) title('vertical Von Karmon Turbulence Shapin Filter Bode Plot') %(d): %TURBULENCE SIMULATION: n=; n=sqrt(si)*randn(n,); A=-; B=; C=; D=; 6
7 dt=tau/; t=:n-; t=dt*t'; sysu=ss(a,b,c,d); =lsim(sysu,n,t); fiure(3) subplot(,,), plot(t,n) title('white noise input to the shapin filter') subplot(,,),plot(t,) title('von Karmon _(t) turbulence') %(e): %SIMULATION OF PHUGOID RESPONSE TO TURBULENCE: a=lsim(ha,,t); q=lsim(hq,,t); fiure(33) subplot(,,),plot(t,a) title('a(t) Response to _(t)') subplot(,,),plot(t,q) title('q(t) Response to _(t)') %(f): % Compute Theoretical psd's for a(t) and q(t): vec=lospace(-,,); HHa=sqrt(si)*H*Ha; [M,P]=bode(HHa,vec); psd_a = squeeze(m); psd_adb=*lo(psd_a); HHq=sqrt(si)*H*Hq; [M,P]=bode(HHq,vec); psd_q = squeeze(m); psd_qdb=*lo(psd_q); fiure(34) semilox(vec',[psd_adb, psd_qdb]) leend('psd for a(t)','psd for q(t)') xlabel('frequency (rad/sec)') ylabel('db') title('theoretical PSDs for a(t) and q(t)') 7
Homework 6 AERE355 Fall 2017 Due 11/27 (M) Name. is called the. 3dB bandwidth.
1 Homeork 6 AERE355 Fall 17 Due 11/7 (M) Name PROBLEM 1(3pt The transfer function of a first order Lo Pass Filter (LPF) is frequency rane [, BW ] is called the filter 3dB bandidth (BW) (a)(8pt The dc (ie
More informationIntroduction To Resonant. Circuits. Resonance in series & parallel RLC circuits
Introduction To esonant Circuits esonance in series & parallel C circuits Basic Electrical Engineering (EE-0) esonance In Electric Circuits Any passive electric circuit ill resonate if it has an inductor
More informationbe a deterministic function that satisfies x( t) dt. Then its Fourier
Lecture Fourier ransforms and Applications Definition Let ( t) ; t (, ) be a deterministic function that satisfies ( t) dt hen its Fourier it ransform is defined as X ( ) ( t) e dt ( )( ) heorem he inverse
More informationHomework 1 AERE355 Fall 2017 Due 9/1(F) NOTE: If your solution does not adhere to the format described in the syllabus, it will be grade as zero.
1 Hmerk 1 AERE355 Fall 217 Due 9/1(F) Name NOE: If yur slutin des nt adhere t the frmat described in the syllabus, it ill be grade as zer. Prblem 1(25pts) In the altitude regin h 1km, e have the flling
More informationEE Experiment 11 The Laplace Transform and Control System Characteristics
EE216:11 1 EE 216 - Experiment 11 The Laplace Transform and Control System Characteristics Objectives: To illustrate computer usage in determining inverse Laplace transforms. Also to determine useful signal
More informationChapter 14 - Fluids. Pressure is defined as the perpendicular force on a surface per unit surface area.
Chapter 4 - Fluids This chapter deals ith fluids, hich means a liquid or a as. It covers both fluid statics (fluids at rest) and fluid dynamics (fluids in motion). Pressure in a fluid Pressure is defined
More information1the 1it is said to be overdamped. When 1, the roots of
Homework 3 AERE573 Fall 08 Due 0/8(M) ame PROBLEM (40pts) Cosider a D order uderdamped system trasfer fuctio H( s) s ratio 0 The deomiator is the system characteristic polyomial P( s) s s (a)(5pts) Use
More informationEntering Matrices
MATLAB Basic Entering Matrices Transpose Subscripts The Colon Operator Operators Generating Matrices Element-by-element operation Creating a Plot Multiple Data Sets in One Graph Line Styles and Colors
More informationEE 4343/ Control System Design Project LECTURE 10
Copyright S. Ikenaga 998 All rights reserved EE 4343/5329 - Control System Design Project LECTURE EE 4343/5329 Homepage EE 4343/5329 Course Outline Design of Phase-lead and Phase-lag compensators using
More information1 Effects of Regularization For this problem, you are required to implement everything by yourself and submit code.
This set is due pm, January 9 th, via Moodle. You are free to collaborate on all of the problems, subject to the collaboration policy stated in the syllabus. Please include any code ith your submission.
More informationAn Investigation of the use of Spatial Derivatives in Active Structural Acoustic Control
An Investigation of the use of Spatial Derivatives in Active Structural Acoustic Control Brigham Young University Abstract-- A ne parameter as recently developed by Jeffery M. Fisher (M.S.) for use in
More informationHomework 2 Fall 2018 STAT 305B Due 9/13 (R) NOTE: All work associated with a given problem part MUST be placed DIRECTLY beneath that part.
Homework 2 Fall 208 STAT 305B Due 9/3 (R) Name NOTE: All work associated with a given problem part MUST be placed DIRECTLY beneath that part PROBLEM (20pts) In a recent survey [ http://wwwpewinternetorg/206/0/04/the-politics-of-climate/
More informationProblem Weight Score Total 100
EE 350 EXAM IV 15 December 2010 Last Name (Print): First Name (Print): ID number (Last 4 digits): Section: DO NOT TURN THIS PAGE UNTIL YOU ARE TOLD TO DO SO Problem Weight Score 1 25 2 25 3 25 4 25 Total
More informationMEASUREMENTS OF TIME-SPACE DISTRIBUTION OF CONVECTIVE HEAT TRANSFER TO AIR USING A THIN CONDUCTIVE-FILM
MEASUREMENTS OF TIME-SPACE DISTRIBUTION OF CONVECTIVE HEAT TRANSFER TO AIR USING A THIN CONDUCTIVE-FILM Hajime Nakamura Department of Mechanical Engineering, National Defense Academy 1-10-0 Hashirimizu,
More informationLinear System Theory
Linear System Theory - Laplace Transform Prof. Robert X. Gao Department of Mechanical Engineering University of Connecticut Storrs, CT 06269 Outline What we ve learned so far: Setting up Modeling Equations
More informationA ROBUST BEAMFORMER BASED ON WEIGHTED SPARSE CONSTRAINT
Progress In Electromagnetics Research Letters, Vol. 16, 53 60, 2010 A ROBUST BEAMFORMER BASED ON WEIGHTED SPARSE CONSTRAINT Y. P. Liu and Q. Wan School of Electronic Engineering University of Electronic
More informationV DD. M 1 M 2 V i2. V o2 R 1 R 2 C C
UNVERSTY OF CALFORNA Collee of Enineerin Department of Electrical Enineerin and Computer Sciences E. Alon Homework #3 Solutions EECS 40 P. Nuzzo Use the EECS40 90nm CMOS process in all home works and projects
More informationAccurate and Estimation Methods for Frequency Response Calculations of Hydroelectric Power Plant
Accurate and Estimation Methods for Frequency Response Calculations of Hydroelectric Poer Plant SHAHRAM JAI, ABOLFAZL SALAMI epartment of Electrical Engineering Iran University of Science and Technology
More informationFrequency Response part 2 (I&N Chap 12)
Frequency Response part 2 (I&N Chap 12) Introduction & TFs Decibel Scale & Bode Plots Resonance Scaling Filter Networks Applications/Design Frequency response; based on slides by J. Yan Slide 3.1 Example
More information3 - Vector Spaces Definition vector space linear space u, v,
3 - Vector Spaces Vectors in R and R 3 are essentially matrices. They can be vieed either as column vectors (matrices of size and 3, respectively) or ro vectors ( and 3 matrices). The addition and scalar
More information18.12 FORCED-DAMPED VIBRATIONS
8. ORCED-DAMPED VIBRATIONS Vibrations A mass m is attached to a helical spring and is suspended from a fixed support as before. Damping is also provided in the system ith a dashpot (ig. 8.). Before the
More informationHomework Set 2 Solutions
MATH 667-010 Introduction to Mathematical Finance Prof. D. A. Edards Due: Feb. 28, 2018 Homeork Set 2 Solutions 1. Consider the ruin problem. Suppose that a gambler starts ith ealth, and plays a game here
More informationCorrelation, discrete Fourier transforms and the power spectral density
Correlation, discrete Fourier transforms and the power spectral density visuals to accompany lectures, notes and m-files by Tak Igusa tigusa@jhu.edu Department of Civil Engineering Johns Hopkins University
More information(1) Sensitivity = 10 0 g x. (2) m Size = Frequency = s (4) Slenderness = 10w (5)
1 ME 26 Jan. May 2010, Homeork #1 Solution; G.K. Ananthasuresh, IISc, Bangalore Figure 1 shos the top-vie of the accelerometer. We need to determine the values of, l, and s such that the specified requirements
More informationAPPLICATIONS FOR ROBOTICS
Version: 1 CONTROL APPLICATIONS FOR ROBOTICS TEX d: Feb. 17, 214 PREVIEW We show that the transfer function and conditions of stability for linear systems can be studied using Laplace transforms. Table
More informationIntermediate 2 Revision Unit 3. (c) (g) w w. (c) u. (g) 4. (a) Express y = 4x + c in terms of x. (b) Express P = 3(2a 4d) in terms of a.
Intermediate Revision Unit. Simplif 9 ac c ( ) u v u ( ) 9. Epress as a single fraction a c c u u a a (h) a a. Epress, as a single fraction in its simplest form Epress 0 as a single fraction in its simplest
More informationUC Berkeley Department of Electrical Engineering and Computer Sciences. EECS 126: Probability and Random Processes
UC Berkeley Department of Electrical Engineering and Computer Sciences EECS 26: Probability and Random Processes Problem Set Spring 209 Self-Graded Scores Due:.59 PM, Monday, February 4, 209 Submit your
More informationECE 3793 Matlab Project 3 Solution
ECE 3793 Matlab Project 3 Solution Spring 27 Dr. Havlicek. (a) In text problem 9.22(d), we are given X(s) = s + 2 s 2 + 7s + 2 4 < Re {s} < 3. The following Matlab statements determine the partial fraction
More informationDefinition of a new Parameter for use in Active Structural Acoustic Control
Definition of a ne Parameter for use in Active Structural Acoustic Control Brigham Young University Abstract-- A ne parameter as recently developed by Jeffery M. Fisher (M.S.) for use in Active Structural
More informationChap 4. State-Space Solutions and
Chap 4. State-Space Solutions and Realizations Outlines 1. Introduction 2. Solution of LTI State Equation 3. Equivalent State Equations 4. Realizations 5. Solution of Linear Time-Varying (LTV) Equations
More informationStability of CL System
Stability of CL System Consider an open loop stable system that becomes unstable with large gain: At the point of instability, K( j) G( j) = 1 0dB K( j) G( j) K( j) G( j) K( j) G( j) =± 180 o 180 o Closed
More informationOSCILLATIONS
OSCIAIONS Important Points:. Simple Harmonic Motion: a) he acceleration is directly proportional to the displacement of the body from the fixed point and it is always directed towards the fixed point in
More informationMAE 143B - Homework 7
MAE 143B - Homework 7 6.7 Multiplying the first ODE by m u and subtracting the product of the second ODE with m s, we get m s m u (ẍ s ẍ i ) + m u b s (ẋ s ẋ u ) + m u k s (x s x u ) + m s b s (ẋ s ẋ u
More informationLab Experiment 2: Performance of First order and second order systems
Lab Experiment 2: Performance of First order and second order systems Objective: The objective of this exercise will be to study the performance characteristics of first and second order systems using
More informationColor Reproduction Stabilization with Time-Sequential Sampling
Color Reproduction Stabilization ith Time-Sequential Sampling Teck-Ping Sim, and Perry Y. Li Department of Mechanical Engineering, University of Minnesota Church Street S.E., MN 55455, USA Abstract Color
More informationLogic Effort Revisited
Logic Effort Revisited Mark This note ill take another look at logical effort, first revieing the asic idea ehind logical effort, and then looking at some of the more sutle issues in sizing transistors..0
More informationMMSE Equalizer Design
MMSE Equalizer Design Phil Schniter March 6, 2008 [k] a[m] P a [k] g[k] m[k] h[k] + ṽ[k] q[k] y [k] P y[m] For a trivial channel (i.e., h[k] = δ[k]), e kno that the use of square-root raisedcosine (SRRC)
More informationSignals & Systems - Chapter 6
Signals & Systems - Chapter 6 S. A real-valued signal x( is knon to be uniquely determined by its samples hen the sampling frequeny is s = 0,000π. For hat values of is (j) guaranteed to be zero? From the
More informationAirspeed Calibration Using GPS Three-Vector Method ( Cloverleaf Method)
Airspeed Calibration Usin GPS Three-ector Method ( Cloverleaf Method) An Informal Memo by Wayne Olson Updated: 1/10/2005 An Informal Memo by Wayne Olson...1 Déjà vu I ve seen this before:...1 Introduction...2
More informationLecture 17 Errors in Matlab s Turbulence PSD and Shaping Filter Expressions
Lectre 7 Errors in Matlab s Trblence PSD and Shaping Filter Expressions b Peter J Sherman /7/7 [prepared for AERE 355 class] In this brief note we will show that the trblence power spectral densities (psds)
More informationDynamics 4600:203 Homework 03 Due: February 08, 2008 Name:
Dynamics 4600:03 Homework 03 Due: ebruary 08, 008 Name: Please denote your answers clearly, i.e., bo in, star, etc., and write neatly. There are no points for small, messy, unreadable work... please use
More informationWhy do Golf Balls have Dimples on Their Surfaces?
Name: Partner(s): 1101 Section: Desk # Date: Why do Golf Balls have Dimples on Their Surfaces? Purpose: To study the drag force on objects ith different surfaces, ith the help of a ind tunnel. Overvie
More informationCALCULATION OF STEAM AND WATER RELATIVE PERMEABILITIES USING FIELD PRODUCTION DATA, WITH LABORATORY VERIFICATION
CALCULATION OF STEAM AND WATER RELATIVE PERMEABILITIES USING FIELD PRODUCTION DATA, WITH LABORATORY VERIFICATION Jericho L. P. Reyes, Chih-Ying Chen, Keen Li and Roland N. Horne Stanford Geothermal Program,
More informationSimulation, Transfer Function
Max Force (lb) Displacement (in) 1 ME313 Homework #12 Simulation, Transfer Function Last Updated November 17, 214. Repeat the car-crash problem from HW#6. Use the Matlab function lsim with ABCD format
More information2.161 Signal Processing: Continuous and Discrete
MI OpenCourseWare http://ocw.mit.edu.6 Signal Processing: Continuous and Discrete Fall 8 For information about citing these materials or our erms of Use, visit: http://ocw.mit.edu/terms. MASSACHUSES INSIUE
More informationTowards a Theory of Societal Co-Evolution: Individualism versus Collectivism
Toards a Theory of Societal Co-Evolution: Individualism versus Collectivism Kartik Ahuja, Simpson Zhang and Mihaela van der Schaar Department of Electrical Engineering, Department of Economics, UCLA Theorem
More informationSAMPLE SOLUTION TO EXAM in MAS501 Control Systems 2 Autumn 2015
FACULTY OF ENGINEERING AND SCIENCE SAMPLE SOLUTION TO EXAM in MAS501 Control Systems 2 Autumn 2015 Lecturer: Michael Ruderman Problem 1: Frequency-domain analysis and control design (15 pt) Given is a
More informationLinear Regression Linear Regression with Shrinkage
Linear Regression Linear Regression ith Shrinkage Introduction Regression means predicting a continuous (usually scalar) output y from a vector of continuous inputs (features) x. Example: Predicting vehicle
More informationh = 0 km for your table in (a)], and for T0 = 316 K. Then obtain a Homework 1 AERE355 Fall 2017 Due 9/1(F)
1 Herk 1 AERE355 Fall 17 Due 9/1(F) SOLUION NOE: If yur slutin des nt adhere t the frat described in the syllabus, it ill be grade as zer Prble 1(5pts) In the altitude regin < h < 1k, e have the flling
More informationAuthor(s) NAKAGAWA, Ichiro; NODA, Hiromu; HAT.
Title FREE OSCLLATONS OF THE EARTH OBSE GALTZN SESMOGRAPH AT ABUYAMA, JA Author(s) NAKAGAWA, chiro; NODA, Hiromu; HAT Citation Special Contributions of the Geophy University (1966), 6: 255-265 ssue Date
More informationToday (10/23/01) Today. Reading Assignment: 6.3. Gain/phase margin lead/lag compensator Ref. 6.4, 6.7, 6.10
Today Today (10/23/01) Gain/phase margin lead/lag compensator Ref. 6.4, 6.7, 6.10 Reading Assignment: 6.3 Last Time In the last lecture, we discussed control design through shaping of the loop gain GK:
More information16.333: Lecture # 14. Equations of Motion in a Nonuniform Atmosphere. Gusts and Winds
16.333: Lecture # 14 Equations of Motion in a Nonuniform Atmosphere Gusts and Winds 1 Fall 2004 16.333 12 2 Equations of Motion Analysis to date has assumed that the atmosphere is calm and fixed Rarely
More information'XNH8QLYHUVLW\ (GPXQG73UDWW-U6FKRRORI(QJLQHHULQJ. EGR 224 Spring Test II. Michael R. Gustafson II
'XNH8QLYHUVLW\ (GPXQG73UDWW-U6FKRRORI(QJLQHHULQJ EGR 224 Spring 2017 Test II Michael R. Gustafson II Name (please print) In keeping with the Community Standard, I have neither provided nor received any
More information6.1 Sketch the z-domain root locus and find the critical gain for the following systems K., the closed-loop characteristic equation is K + z 0.
6. Sketch the z-domain root locus and find the critical gain for the following systems K (i) Gz () z 4. (ii) Gz K () ( z+ 9. )( z 9. ) (iii) Gz () Kz ( z. )( z ) (iv) Gz () Kz ( + 9. ) ( z. )( z 8. ) (i)
More informationMAPLE for CIRCUITS and SYSTEMS
2520 MAPLE for CIRCUITS and SYSTEMS E. L. Gerber, Ph.D Drexel University ABSTRACT There are three popular software programs used to solve circuits problems: Maple, MATLAB, and Spice. Each one has a different
More informationCHARACTERIZATION OF ULTRASONIC IMMERSION TRANSDUCERS
CHARACTERIZATION OF ULTRASONIC IMMERSION TRANSDUCERS INTRODUCTION David D. Bennink, Center for NDE Anna L. Pate, Engineering Science and Mechanics Ioa State University Ames, Ioa 50011 In any ultrasonic
More informationExercise 1 (A Non-minimum Phase System)
Prof. Dr. E. Frazzoli 5-59- Control Systems I (HS 25) Solution Exercise Set Loop Shaping Noele Norris, 9th December 26 Exercise (A Non-minimum Phase System) To increase the rise time of the system, we
More informationBfh Ti Control F Ws 2008/2009 Lab Matlab-1
Bfh Ti Control F Ws 2008/2009 Lab Matlab-1 Theme: The very first steps with Matlab. Goals: After this laboratory you should be able to solve simple numerical engineering problems with Matlab. Furthermore,
More informationModule 5: Design of Sampled Data Control Systems Lecture Note 8
Module 5: Design of Sampled Data Control Systems Lecture Note 8 Lag-lead Compensator When a single lead or lag compensator cannot guarantee the specified design criteria, a laglead compensator is used.
More informationCHAPTER 12 TIME DOMAIN: MODAL STATE SPACE FORM
CHAPTER 1 TIME DOMAIN: MODAL STATE SPACE FORM 1.1 Introduction In Chapter 7 we derived the equations of motion in modal form for the system in Figure 1.1. In this chapter we will convert the modal form
More informationLesson 19: Process Characteristics- 1 st Order Lag & Dead-Time Processes
1 Lesson 19: Process Characteristics- 1 st Order Lag & Dead-Time Processes ET 438a Automatic Control Systems Technology 2 Learning Objectives After this series of presentations you will be able to: Describe
More informationSome tools and methods for determination of dynamics of hydraulic systems
Some tools and methods for determination of dynamics of hydraulic systems A warm welcome to the course in Hydraulic servo-techniques! The purpose of the exercises given in this material is to make you
More informationFrequency-Weighted Model Reduction with Applications to Structured Models
27 American Control Conference http://.cds.caltech.edu/~murray/papers/sm7-acc.html Frequency-Weighted Model Reduction ith Applications to Structured Models Henrik Sandberg and Richard M. Murray Abstract
More informationRadar Dish. Armature controlled dc motor. Inside. θ r input. Outside. θ D output. θ m. Gearbox. Control Transmitter. Control. θ D.
Radar Dish ME 304 CONTROL SYSTEMS Mechanical Engineering Department, Middle East Technical University Armature controlled dc motor Outside θ D output Inside θ r input r θ m Gearbox Control Transmitter
More informationStudio Exercise Time Response & Frequency Response 1 st -Order Dynamic System RC Low-Pass Filter
Studio Exercise Time Response & Frequency Response 1 st -Order Dynamic System RC Low-Pass Filter i i in R out Assignment: Perform a Complete e in C e Dynamic System Investigation out of the RC Low-Pass
More informationÜbersetzungshilfe / Translation aid (English) To be returned at the end of the exam!
Prüfung Regelungstechnik I (Control Systems I) Prof. Dr. Lino Guzzella 3.. 24 Übersetzungshilfe / Translation aid (English) To be returned at the end of the exam! Do not mark up this translation aid -
More informationFunctional and Structural Implications of Non-Separability of Spectral and Temporal Responses in AI
Functional and Structural Implications of Non-Separability of Spectral and Temporal Responses in AI Jonathan Z. Simon David J. Klein Didier A. Depireux Shihab A. Shamma and Dept. of Electrical & Computer
More informationProblem Weight Total 100
EE 350 Problem Set 3 Cover Sheet Fall 2016 Last Name (Print): First Name (Print): ID number (Last 4 digits): Section: Submission deadlines: Turn in the written solutions by 4:00 pm on Tuesday September
More informationELECTRONICS & COMMUNICATIONS DEP. 3rd YEAR, 2010/2011 CONTROL ENGINEERING SHEET 5 Lead-Lag Compensation Techniques
CAIRO UNIVERSITY FACULTY OF ENGINEERING ELECTRONICS & COMMUNICATIONS DEP. 3rd YEAR, 00/0 CONTROL ENGINEERING SHEET 5 Lead-Lag Compensation Techniques [] For the following system, Design a compensator such
More informationEE nd Order Time and Frequency Response (Using MatLab)
EE 2302 2 nd Order Time and Frequency Response (Using MatLab) Objective: The student should become acquainted with time and frequency domain analysis of linear systems using Matlab. In addition, the student
More informationCENG 5210 Advanced Separation Processes. Reverse osmosis
Reverse osmosis CENG 510 Advanced Separation Processes In osmosis, solvent transports from a dilute solute or salt solution to a concentrated solute or salt solution across a semipermeable membrane hich
More information3. The vertices of a right angled triangle are on a circle of radius R and the sides of the triangle are tangent to another circle of radius r. If the
The Canadian Mathematical Society in collaboration ith The CENTRE for EDUCTION in MTHEMTICS and COMPUTING First Canadian Open Mathematics Challenge (1996) Solutions c Canadian Mathematical Society 1996
More informationFORCE NATIONAL STANDARDS COMPARISON BETWEEN CENAM/MEXICO AND NIM/CHINA
FORCE NATIONAL STANDARDS COMPARISON BETWEEN CENAM/MEXICO AND NIM/CHINA Qingzhong Li *, Jorge C. Torres G.**, Daniel A. Ramírez A.** *National Institute of Metrology (NIM) Beijing, 100013, China Tel/fax:
More informationAn Analog Analogue of a Digital Quantum Computation
An Analog Analogue of a Digital Quantum Computation arxiv:quant-ph/9612026v1 6 Dec 1996 Edard Farhi Center for Theoretical Physics Massachusetts Institute of Technology Cambridge, MA 02139 Sam Gutmann
More informationProfessor Fearing EE C128 / ME C134 Problem Set 7 Solution Fall 2010 Jansen Sheng and Wenjie Chen, UC Berkeley
Professor Fearing EE C8 / ME C34 Problem Set 7 Solution Fall Jansen Sheng and Wenjie Chen, UC Berkeley. 35 pts Lag compensation. For open loop plant Gs ss+5s+8 a Find compensator gain Ds k such that the
More informationSchool of Mechanical Engineering Purdue University
Case Study ME375 Frequency Response - 1 Case Study SUPPORT POWER WIRE DROPPERS Electric train derives power through a pantograph, which contacts the power wire, which is suspended from a catenary. During
More informationSIMPLE HARMONIC MOTION PREVIOUS EAMCET QUESTIONS ENGINEERING. the mass of the particle is 2 gms, the kinetic energy of the particle when t =
SIMPLE HRMONIC MOION PREVIOUS EMCE QUESIONS ENGINEERING. he displacement of a particle executin SHM is iven by :y = 5 sin 4t +. If is the time period and 3 the mass of the particle is ms, the kinetic enery
More informationSUPPORTING INFORMATION. Line Roughness. in Lamellae-Forming Block Copolymer Films
SUPPORTING INFORMATION. Line Roughness in Lamellae-Forming Bloc Copolymer Films Ricardo Ruiz *, Lei Wan, Rene Lopez, Thomas R. Albrecht HGST, a Western Digital Company, San Jose, CA 9535, United States
More informationMASSACHUSETTS INSTITUTE OF TECHNOLOGY Department of Mechanical Engineering Dynamics and Control II Fall 2007
MASSACHUSETTS INSTITUTE OF TECHNOLOGY Department of Mechanical Engineering.4 Dynamics and Control II Fall 7 Problem Set #9 Solution Posted: Sunday, Dec., 7. The.4 Tower system. The system parameters are
More informationCHAPTER 6 STATE SPACE: FREQUENCY RESPONSE, TIME DOMAIN
CHAPTER 6 STATE SPACE: FREQUENCY RESPONSE, TIME DOMAIN 6. Introduction Frequency Response This chapter will begin with the state space form of the equations of motion. We will use Laplace transforms to
More informationCDS 101/110: Lecture 3.1 Linear Systems
CDS /: Lecture 3. Linear Systems Goals for Today: Revist and motivate linear time-invariant system models: Summarize properties, examples, and tools Convolution equation describing solution in response
More informationLinear Regression Linear Regression with Shrinkage
Linear Regression Linear Regression ith Shrinkage Introduction Regression means predicting a continuous (usually scalar) output y from a vector of continuous inputs (features) x. Example: Predicting vehicle
More informationA Computer Controlled Microwave Spectrometer for Dielectric Relaxation Studies of Polar Molecules
384 A Computer Controlled Microave Spectrometer for Dielectric Relaation Studies of Polar Molecules Jai N. Dahiya*, Santaneel Ghosh and J. A. Roberts+ Department of Physics and Engineering Physics, Southeast
More informationDeveloping a Multisemester Interwoven Dynamic Systems Project to Foster Learning and Retention of STEM Material
100 10 1 ζ=0.1% ζ=1% ζ=2% ζ=5% ζ=10% ζ=20% 0-90 -180 ζ=20% ζ=10% ζ=5% ζ=2% ζ=1% ζ=0.1% Proceedings of 2004 IMECE: November 13-19, 2004, Anaheim, CA 2004 ASME International Mechanical Engineering Congress
More informationIntroduction to Feedback Control
Introduction to Feedback Control Control System Design Why Control? Open-Loop vs Closed-Loop (Feedback) Why Use Feedback Control? Closed-Loop Control System Structure Elements of a Feedback Control System
More informationCDS 101: Lecture 4.1 Linear Systems
CDS : Lecture 4. Linear Systems Richard M. Murray 8 October 4 Goals: Describe linear system models: properties, eamples, and tools Characterize stability and performance of linear systems in terms of eigenvalues
More informationThe peculiarities of the model: - it is allowed to use by attacker only noisy version of SG C w (n), - CO can be known exactly for attacker.
Lecture 6. SG based on noisy channels [4]. CO Detection of SG The peculiarities of the model: - it is alloed to use by attacker only noisy version of SG C (n), - CO can be knon exactly for attacker. Practical
More informationUSE OF FILTERED SMITH PREDICTOR IN DMC
Proceedins of the th Mediterranean Conference on Control and Automation - MED22 Lisbon, Portual, July 9-2, 22. USE OF FILTERED SMITH PREDICTOR IN DMC C. Ramos, M. Martínez, X. Blasco, J.M. Herrero Predictive
More informationCourse Background. Loosely speaking, control is the process of getting something to do what you want it to do (or not do, as the case may be).
ECE4520/5520: Multivariable Control Systems I. 1 1 Course Background 1.1: From time to frequency domain Loosely speaking, control is the process of getting something to do what you want it to do (or not
More informationCore Concepts Review. Orthogonality of Complex Sinusoids Consider two (possibly non-harmonic) complex sinusoids
Overview of Continuous-Time Fourier Transform Topics Definition Compare & contrast with Laplace transform Conditions for existence Relationship to LTI systems Examples Ideal lowpass filters Relationship
More information7.2 Controller tuning from specified characteristic polynomial
192 Finn Haugen: PID Control 7.2 Controller tuning from specified characteristic polynomial 7.2.1 Introduction The subsequent sections explain controller tuning based on specifications of the characteristic
More informationLab 3: Poles, Zeros, and Time/Frequency Domain Response
ECEN 33 Linear Systems Spring 2 2-- P. Mathys Lab 3: Poles, Zeros, and Time/Frequency Domain Response of CT Systems Introduction Systems that are used for signal processing are very often characterized
More informationE2.5 Signals & Linear Systems. Tutorial Sheet 1 Introduction to Signals & Systems (Lectures 1 & 2)
E.5 Signals & Linear Systems Tutorial Sheet 1 Introduction to Signals & Systems (Lectures 1 & ) 1. Sketch each of the following continuous-time signals, specify if the signal is periodic/non-periodic,
More informationPositioning Servo Design Example
Positioning Servo Design Example 1 Goal. The goal in this design example is to design a control system that will be used in a pick-and-place robot to move the link of a robot between two positions. Usually
More informationRaktim Bhattacharya. . AERO 632: Design of Advance Flight Control System. Preliminaries
. AERO 632: of Advance Flight Control System. Preliminaries Raktim Bhattacharya Laboratory For Uncertainty Quantification Aerospace Engineering, Texas A&M University. Preliminaries Signals & Systems Laplace
More information3-D FINITE ELEMENT MODELING OF THE REMOTE FIELD EDDY CURRENT EFFECT
3-D FINITE ELEMENT MODELING OF THE REMOTE FIELD EDDY CURRENT EFFECT Y. Sun and H. Lin Department of Automatic Control Nanjing Aeronautical Institute Nanjing 2116 People's Republic of China Y. K. Shin,
More informationOccurrence Frequency of Aurora Derived from ASCAPLOT. J unji NAKAMURA* 1tU:.tJ:v' : 0):r''-5'v=:0v,-cv:t K"Etf"A
o. 16. 1962] (1361) Occurrence Frequency of Aurora Derived fro ASCAPLOT J unji AKAMURA* 1959 : 1cf 196 : ) Ascaplot r::5rt L r tj:*1ett2: t -C BiffP t-fur::t3vt t :Yt;O) Fsi Fsil J t:1:1:ej}j;jt)jt 2:
More informationIT6502 DIGITAL SIGNAL PROCESSING Unit I - SIGNALS AND SYSTEMS Basic elements of DSP concepts of frequency in Analo and Diital Sinals samplin theorem Discrete time sinals, systems Analysis of discrete time
More informationAnalysis of planar welds
Dr Andrei Lozzi Design II, MECH 3.400 Analysis of planar elds School of Aerospace, Mechanical and Mechatronic Engineering University of Sydney, NSW 2006 Australia lecture eld ne b References: Blodget,
More informationCh 14: Feedback Control systems
Ch 4: Feedback Control systems Part IV A is concerned with sinle loop control The followin topics are covered in chapter 4: The concept of feedback control Block diaram development Classical feedback controllers
More information