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Equation Sheet for Systems Dynamics and Control | ME 430, Study notes of Mechanical Engineering

Material Type: Notes; Class: SYSTEMS DYNAMICS AND CONTROL; Subject: Mechanical Engineering; University: Oregon State University; Term: Winter 2008;

Typology: Study notes

Pre 2010

Uploaded on 08/30/2009

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ME 430/ECE 451 Equation Sheet
First Order systems:
T(s) = a
s+a
Rise Time:
Tr=2.2
a
Settling Time:
Ts=4.6
a(1%)
Ts=4
a(2%)
Second Order systems:
T(s) = ω2
n
s2+ 2ζωns+ω2
n
Settling Time:
Ts=4.6
ζωn
(1%)
Ts=4.0
ζωn
(2%)
Ts=3.0
ζωn
(5%)
Percent Overshoot:
%OS = 100 e(πζ /1ζ2)
ζ=ln(%OS/100)
pπ2+ln2(%OS/100)
Rise Time:
Tr=1.64
ωn
(ζ=.5)
Tr=1.86
ωn
(ζ=.6)
Tr=2.13
ωn
(ζ=.7)
Peak Time:
Tp=π
ωnp1ζ2
Root Locus Refinement:
Breakaway and break-in points: For G=
NG
DGfind ssuch that: N0
GDGD0
GNG= 0
jw-axis crossing: Form Routh Table (for
closed loop transfer function) and find gain
for obtaining a row of zeros. Form aux.
equation using that gain and solve for s.
Arrival and Departure Angles:
Use : Pθzeros Pθpoles =±180
Steady State Error:
For closed loop transfer function T(s):
E(s) = X(s)Y(s)
=X(s)[1 T(s)]
Useful Numbers:
5% overshoot leads to ζ'0.7
16% overshoot leads to ζ'0.5
α= tan1(ζ
1ζ2)
ζ= 0.7 leads to α'45
ζ= 0.5 leads to α'30
182= 324 18 '4.2
222= 484 22 '4.7
262= 676 26 '5.1
4×26 = 104
9×26 = 234
12 ×26 = 312
12
2'1.73 12
6'0.58
220
6'2.47

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ME 430/ECE 451 Equation Sheet

First Order systems:

T (s) =

a s + a Rise Time:

Tr =

a

Settling Time:

Ts =

a

Ts =

a

Second Order systems:

T (s) =

ω n^2 s^2 + 2ζωns + ω^2 n Settling Time:

Ts =

ζωn

Ts =

ζωn

Ts =

ζωn

Percent Overshoot:

%OS = 100 e−(πζ/

1 −ζ^2 )

ζ =

−ln(%OS/100) √ π^2 + ln^2 (%OS/100)

Rise Time:

Tr =

ωn

(ζ = .5)

Tr =

ωn

(ζ = .6)

Tr =

ωn

(ζ = .7)

Peak Time:

Tp =

π ωn

√ 1 − ζ^2

Root Locus Refinement:

  • Breakaway and break-in points: For G = NG DG find^ s^ such that:^ N^

′ GDG^ −^ D

′ GNG^ = 0

  • jw-axis crossing: Form Routh Table (for closed loop transfer function) and find gain for obtaining a row of zeros. Form aux. equation using that gain and solve for s.
  • Arrival and Departure Angles: Use :

∑ θzeros −^

∑ θpoles =^ ±^180

Steady State Error:

For closed loop transfer function T(s): E(s) = X(s) − Y (s) = X(s)[1 − T (s)]

Useful Numbers:

5% overshoot leads to ζ ' 0. 7 16% overshoot leads to ζ ' 0. 5

α = tan−^1 ( √ 1 ζ−ζ 2 ) ζ = 0.7 leads to α ' 45 ◦ ζ = 0.5 leads to α ' 30 ◦

4 × 26 = 104

9 × 26 = 234

12 × 26 = 312

√ 12 2 '^1.^73

√ 12 6 '^0.^58 √ 220 6 '^2.^47