Roll-attitude control of a missile having a strong aerodynamic non-linearity
作者:
P. A. T. CHRISTOPHER,
期刊:
International Journal of Control
(Taylor Available online 1980)
卷期:
Volume 31,
issue 2
页码: 209-218
ISSN:0020-7179
年代: 1980
DOI:10.1080/00207178008961038
出版商: Taylor & Francis Group
数据来源: Taylor
摘要:
The suppression of non-linear behaviour by enclosing a system within a closed-loop having high loop gain is a well-known principle. An example of this type, arising in the roll-attitude control of guided missiles, is presented, and it is shown that a quasi-linear design technique is likely to be adequate, provided that a suitable test is made of the global asymptotic stability.
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