曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
Taking the inverse Laplace transform,
' b
y(t) = b + ( . b)e_ur
a
(5.54)
We note that y(0) = 1 and y(oo) = b/a.
The first term on the right-hand side represents forced response and the sec-
ond term represents the natural response. The forced response is also known as
steady-state response, and the natural response is also known as transient response.
Observe that the pole at s = 0 corresponding to the input unit-step function gen-
erates the forced response. The transient response is generated by the system pole
at s - -a and is of the form e-"r. Thus, the farther to the left the pole is located
on the negative real axis, the faster the transient response will decay to zero. On
the other hand, if this pole is located on the positive real axis, then the response
will be of diverging nature because the out,put will increase steadily with time.
The zeros of the system and the inpue function influence the amplitude of both
the steady-state and the transient response. In this case, we have only one system
zero at s - -b, and there is no zero because of the input function. The effect of
this system zero on the amplitude of the response can be seen in Eq. (5.54).
The quantity l/a is called the time constant of the given first-order system.
The time constant is a measure of the speed with which a system responds to an
external input. The lower the value of the time constant (or l:igher the value of a),
the faster will be the system response. Sometimes, a is also called the exponential
decay frequency. For t = lla, y(t) = 0.63 times its final rise above the initial
value. In other words, at time equal to one tim.e constant. the output rises to 63%
ofits steady-state value above the initial value.
The rise time Tr is the time for the output to increase from 0.1 to 0.9 times its
final or steady-state value. However, it may be noted that some authors define it as
the time for the output to rise from 0.1 to l00o/o of the final value. However, this
alternative definition is not used in this text.
For a first-order system,
2.2
Tr - N
a
(5.55)
The settling time Tx is defined as the time required for the output to reach, for
the first occurrence, within 2% ofits final or steady-state value. For the first-order
system, this value is approximately given by
4
Ts - -
a
5-4-2 Response of Second-Order Systems
Now let us consider a second-order system given by
b
G(s) = -
= s~+ as +b
The response to a unit-step input is
),(s) = G(s)r (s)
b
(5.56)
(5.57)
(5.5 8)
(5.59)
,j
j
"4;
Jv
Nl
ei
lit
~
N
N
s
:~
r'
7j\
' J.
y(s) = G(s)r (s)
= ( ::b)(l)
PERFORMANCE, STABILITY, DYNAMICS, AND CONTROL
A second-order system has two poles.ln general, the response of a second-order
system can be any one of the four types of responses as shown in Fig. 5.3. Suppose
the system poles, which depend on the values ofa and b, are both real and negative
as shown in Fig. 5.3a; then the corresponding response is a steady rise, without
any overshoot, to the final value. This type of response is called an "overdamped"
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
动力机械和机身手册2(157)
