Aimed at the inherent blemish existed currently in airplane cockpit temperature regulating system, a digital temperature auto-regulating design scheme of the system is put forward, namely, the temperature controller of digital PID is designed firstly, and then applied in airplane cockpit temperature regulating system by adopting the way of cascade control. Experiment result indicates that the design scheme is reasonable.
REFERENCES
1.
2.
F. R.
Lei
and X. L.
Zhou
, Design Search Manual of Chip 51 Module in Common Use
. (Tsinghua University Press
, Beijing
, 2010
), pp. 23
–34
.3.
M.
Xing
and A. L.
Cheng
, Microcontrollers Principle and Application
(Posts & Telecom Press
, Beijing
, 2012
), pp. 13
–21
.4.
Z. W.
Chen
and Z. R.
Chen
, Systems Design and Practice of 51 Series Chip
(Publishing House of Electronics industry
, Beijing
, 2009
), pp. 213
–221
.5.
J.
Wang
and S. H.
Cui
, Sensor Practical Technique
. (China Machine Press
, Beijing
, 2012
), pp. 102
–110
.6.
7.
H. C.
Sun
and D. Z.
Li
, Process Control Engineering Design
(Chemical Industry Press
, Beijing
, 2009
), pp. 322
–327
.8.
Y. N.
Guo
and J. L.
Chang
, Process Control Systems
(China Machine Press
, Beijing
, 2009
), pp. 171
–178
.9.
D. X.
Huang
and J. C.
Wang
, Process Control Systems
(Tsinghua University Press
, Beijing
, 2010
), pp. 336
–342
.10.
X. H.
Qi
and J. Q.
Huang
, Modern Control Theory and Apply
(National Defense Industry Press
, Beijing
, 2007
), pp. 163
–174
.11.
Z. L.
Wang
and Y. K.
Guo
. Process Control and Simulink Application
(Publishing House of Electronics Industry
, Beijing
, 2006
), pp. 167
–185
.
This content is only available via PDF.
© 2019 Author(s).
2019
Author(s)
You do not currently have access to this content.