Page
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Line
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Erratum
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Version
Template:Errata type
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52
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0
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In Figure 2.16, theta should be O
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2.10b
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87
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3
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In equation (3.27), the state used for the output should be c, not x
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2.10b
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97
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-11, -4
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Equation (4.4) is labeled incorrectly
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2.10b
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121
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5 to 6
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Global Lyapunov stability requires additional conditions
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2.10b
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152
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-5
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In the complex input u = exp(s t), s should be i omega, not i omega t
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2.10b
|
174
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-3
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In Example 6.3, z_2 should be x_1/omega instead of x_2/omega
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2.10b
|
179
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-3
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Reference to equation (6.17) should be to equation (6.15)
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2.10b
|
216
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-7 to -3
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F R_v F^T term dropped in proof of Theorem 7.4
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2.10b
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228
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13
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In Exercise 7.11, output to check is the feedforward signal
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2.10b
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228
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-12
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In Exercise 7.13, missing equals sign in covariance specification
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2.10b
|
234
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-12
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In displayed equation above equation (8.7), U should be u in the expression for the output
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2.10b
|
237
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4
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In Figure 8.3, the gain falls off at omega = a R1 k / R2
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2.10b
|
237
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5
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In Example 8.3, a = 10 rad/s
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2.10b
|
238
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8
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In Example 8.3, a = 10 rad/s
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2.10b
|
240
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-12
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After equation (8.17), "looses" should be "loses"
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2.10b
|
264
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16
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In Exercise 8.8, second transfer function should be G_yn instead of G_yd
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2.10b
|
278
|
2
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In proof of Theorem 9.3, "residues of the poles of is" should be "residue for the poles is"
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2.10b
|
351
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8
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Riemann sphere has radius (not diameter) 1
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2.10b
|
351
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10
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d(P_1, P_2) is the longest chordal distance, not shortest
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2.10b
|
363
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-18
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In Example 12.8, process zero is at s = -2
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2.10b
|
363
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-17
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In Example 12.8, controller zeros is at s = 3.5
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2.10b
|
364
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-10 to -4
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In Example 12.9, poles are at -a, -p1, -p2
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2.10b
|
367
|
-1
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Remove extra word "in"
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2.10b
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371
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-11
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After equation (12.23), generalized error is z, not w
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2.10b
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Page
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Line
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Erratum
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Version
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19
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-11
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The Wright brothers made their first successful flight in 1903, not 1905
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2.9d
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25
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-1
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In Exercise 1.1, "loosing" should be "losing"
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2.9d
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32
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12
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In discussion on disturbance signals, "can" should be "cannot"
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2.9d
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62
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-6
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In Exercises 2.5 and 5.9, the (2,1) entry of the dynamics matrix should be ab-b
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2.9d
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63
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-8
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In Exercise 2.7, reference to inverted pendulum may be confusing
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2.9d
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80
|
5
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In Equation (3.19), the second term in the window dynamics should contain \rho c
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2.9d
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91
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-6
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In Exercise 3.2: use observable form, delta is the steering angle and "title" should be "tilt"
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2.9d
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92
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-9
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State space dynamics in Exercise 3.5 are not correct
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2.9d
|
106
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7
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Solution for x_2j in block diagonal form discussion has sign errors
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2.9d
|
107
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12-23
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Closed loop dynamics matrix is incorrect in Example 4.6
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2.9d
|
108
|
8
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Missing γ in equation (4.9)
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2.9d
|
110
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11, 13
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In Example 4.8, the linearized dynamics should contain 3 r_e, not 2 r_e
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2.9d
|
112
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-1
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In Example 4.9, V(x) should be V(z)
|
2.9d
|
117
|
3
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Typo in the caption for Figure 4.15
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2.9d
|
126
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-5
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In Exercise 4.1, x_0 should not be subtracted from time-shifted solution
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2.9d
|
126
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-5
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In Exercise 4.1, tau should be defined as t-t_0
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2.9d
|
127
|
5
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In Exercise 4.2, a_e should be a
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2.9d
|
127
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15
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Sign error in second Lyapunov function in Exercise 4.4
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2.9d
|
128
|
3
|
In Exercise 4.6, Pm/J should be taken as 1 and factor of 1/2 is misplaced
|
2.9d
|
129
|
-2
|
In Exercise 4.14c, the transformation T and its inverse are swapped
|
2.9d
|
131
|
-15
|
Extraneous text "!linear" in Section 5.1
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2.9d
|
135
|
12
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In equation (5.5), the upper limit of the integral should be t
|
2.9d
|
144
|
-7
|
Example 5.5 includes a damping term not shown in Figure 5.4
|
2.9d
|
144
|
-4
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In Example 5.5 and 5.6, m1 and m2 should be m
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2.10a
|
145
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5
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In Examples 5.5 and 5.6, dynamics in modal form should use z, not x
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2.9d
|
146
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-15
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Equation (5.15) is linear in the initial conditions and *input*
|
2.10a
|
147
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0
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The labels for v2 and v3 are misplaced in Figure 5.12
|
2.10a
|
148
|
-1
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In Example 5.5 and 5.6, m1 and m2 should be m
|
2.10a
|
149
|
8
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In Examples 5.5 and 5.6, dynamics in modal form should use z, not x
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2.9d
|
154
|
-10
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In Example 5.8, the third nodal equation should be deleted
|
2.10a
|
156
|
-10
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In AFM dynamics, c and k are missing subscript 2
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2.9d
|
157
|
7
|
Missing factor of A in second term of equation (5.26)
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2.10a
|
164
|
-11
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Parameter values are missing in Exercise 5.3
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2.9d
|
164
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-3
|
Remove part (a) in Exercise 5.6
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2.9d
|
165
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11
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In Exercise 5.7, the 5% settling time should be 3 tau instead of 2 tau
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2.9d
|
165
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16
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In Exercise 5.8, the initial condition is x_0
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2.9d
|
166
|
3
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In Exercises 2.5 and 5.9, the (2,1) entry of the dynamics matrix should be ab-b
|
2.9d
|
168
|
12
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The control matrix in the equilibrium set should be 'B' instead of 'b'
|
2.10a
|
169
|
-12
|
In heuristic derivation of reachability test, α is missing subscript
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2.9d
|
180
|
-2
|
Formula for k_r in equation (6.21) of Theorem 6.3 is incorrect
|
2.9d
|
181
|
9
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Missing 's' in expression for characteristic polynomial in discussion of eigenvalue assignment
|
2.9d
|
183
|
-7
|
In equation (6.22), k omega^2 should be k omega_0^2
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2.9d
|
184
|
-10
|
In equation (6.24), the sign of the sin(omega t) term is incorrect for zeta less than one
|
2.9d
|
185
|
4
|
Values of zeta in the caption for Figure 6.8 don't match the figure
|
2.9d
|
188
|
-2
|
Dynamics matrix in Example 6.7 has errors in (3,4) and (4,4) entries
|
2.9d
|
189
|
22
|
Numerical gains for Example 6.7 are incorrect
|
2.9d
|
197
|
3
|
In Figure 6.15, reference velocity is v_r = 20 m/s
|
2.10a
|
198
|
14
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In Exercise 6.4, need to assume A is invertible and C A^-1 B is nonzero
|
2.9d
|
199
|
-1, -2
|
In AFM dynamics, c and k are missing subscript 2
|
2.9d
|
200
|
9
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In Exercise 6.13, R should be removed and rho should be rho_1
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2.9d
|
206
|
10,11
|
In the last paragraph of Section 7.1, "reachable" should be replaced by "observable"
|
2.9d
|
209
|
2
|
In Example 7.2, the observer gain is given by equation (7.11)
|
2.9d
|
214
|
-13
|
In Example 7.4, hats are missing in displayed equation for u
|
2.10a
|
220
|
12
|
In computation of error dynamics, u_ff argument is missing
|
2.9d
|
220
|
-13
|
Minus sign is missing in gain scheduled feedback
|
2.9d
|
224
|
-7
|
References to first and second equations are switched in computer implementation discussion
|
2.9d
|
240
|
-16, -13
|
Sign error in equation (8.17) - (sI - A) should be (A - sI)
|
2.9d
|
240
|
-11
|
Explanation of the lack of zeros when B or C is full rank is confusing
|
2.9d
|
241
|
-4, -6
|
In Example 8.5, q should be replaced by theta
|
2.9d
|
247
|
-1
|
In section on pole/zero cancellations, pole and zero are at s = -a
|
2.10a
|
248
|
1
|
In section on pole/zero cancellations, pole and zero are at s = -a
|
2.10a
|
249
|
3
|
Location of the process pole is missing a zero in figure caption for cruise control example
|
2.9d
|
250
|
-16
|
Missing parenthesis in exponential for output signal
|
2.10a
|
253
|
-1
|
In description of Bode plot for second order transfer function, 'a' should be omega_0
|
2.10a
|
254
|
12
|
In description of Bode plot for second order transfer function, 'a' should be omega_0
|
2.10a
|
254-5
|
-10 to 9
|
In Example 8.8, explanation of effects of poles and zeros is incorrect and confusing
|
2.10a
|
256
|
1
|
Caption for Figure 8.15b is missing an s in the numerator
|
2.9d
|
257
|
5
|
In Example 8.9, the expression for sigma is not correct
|
2.10a
|
272
|
8
|
Before Example 9.3, range of theta should be -pi/2 to pi/2
|
2.10a
|
277
|
13
|
In Theorem 9.3, N should be Z
|
2.9d
|
278
|
3
|
Missing factor of 2 pi in residue formula for proof of Theorem 9.3
|
2.10a
|
288
|
-3
|
Exponential signal is incorrect on the left-hand side of harmonic expansion equation
|
2.9d
|
292
|
18
|
In Exercise 9.9, 10/a should be 1/tau
|
2.9d
|
307
|
-9
|
Toward end of Section 10.4, k_i should be k_t
|
2.9d
|
308
|
0
|
Figure 10.11 is missing filter on derivative term
|
2.9d
|
310
|
-4
|
In Figure 10.13, the indices on the resistors and capacitors are incorrect
|
2.9d
|
311
|
-3
|
Missing ydot after equation (10.16)
|
2.9d
|
313
|
8,9
|
In Exercise 10.1, the second term in the denominator should be kp not kd
|
2.9d
|
314
|
-5
|
In Exercise 10.11, the dynamics for x_2 should test for e less than e_0, not e less than 1
|
2.9d
|
315
|
-8
|
Extraneous 'LDH' and comment in the text
|
2.9d
|
319
|
0
|
Arrow labeled u_fd in Figure 11.3 is in the wrong direction
|
2.9d
|
319
|
4, -2
|
The signal u_ff should be u_fr in the caption for Figure 11.3 and associated text
|
2.9d
|
319
|
-7
|
Extraneous text "!design" in Chapter 12
|
2.9d
|
323
|
-9
|
Maximum sensitivity occurs at frequency omega_ms not omega_sc
|
2.9d
|
325
|
-9
|
Proportional gain in Example 11.4 transfer function should be kp
|
2.9d
|
330
|
5
|
Denominator of vectored thrust process model should be Js^2
|
2.9d
|
336
|
-8
|
Extraneous text "!design" in Chapter 12
|
2.9d
|
345
|
12
|
Exercise 11.4 should be Example 11.4 in Exercise 11.9
|
2.9d
|
345
|
14
|
T_d should be T_f in Exercise 11.9
|
2.9d
|
345
|
-5
|
Numerator and denominator are switched in Exercise 11.11
|
2.9d
|
351
|
2,3
|
Caption for Figure 12.4 doesn't quite match figure
|
2.9d
|
356
|
6, 12
|
In Example 12.6, n = -1 should be n = 1
|
2.9d
|
363
|
-11
|
"Assigning a closed loop zero" should be "assigning a closed loop pole"
|
2.9d
|
369
|
-1
|
Extraneous text "!design" in Chapter 12
|
2.9d
|
378
|
15,16
|
Bennett's books on the history of control were published in 1979 and 1993
|
2.10a
|